EFTA00277580

• e Form Approved OMB No. 2120-0020 For FAA Use Only US Department Of Transportation MAJOR REPAIR AND ALTERATION Office Identification Federal (Airframe, Powerplant, Propeller, or Appliance) Aviation Administration So- r5DO- 1 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions a d disposition of this form. This report is required bylaw (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for ea such violation (Section 901 Federal Aviation Act of 1958). Make Model 1. Aircraft Boeing 727-100 _ Serial No. Nationality and Registration Mark 20115 USA N908JE 2. Owner Name (As shown on registration certificate) = N om J.E.G.E, Inc. 3. For FAA Use Only .. ..• . • pties with applicable Tor, data identified here' for the above atoverthInes reqiiFements is approved described aircraft, subject ntorrnity I by a person ,uthedram 43, se 43.7. 5 (-1 --f5V 0 — i T OCT Sign of Inspector Date 4. Unit Identificati 5. Type Alteration Unit Make Model Serial No. Repair AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE U.S. Certificated Mechanic •VI NICS DIVISION Foreign Certificated Mechanic Radio Class 1,2,3 0 Certificated Repair Station Limited Airframe Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized lndi .d4,31) ( 9/W_ . :,7 fr/ g_. <71, 0C)Z C?-7---46 '& /- ,/ eeZ Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given personsRecified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is APPROVED O REJECTED FAA Flt. Standards Manufacturer inspectfon Authorization Other (Specify) BY Inspector FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group -b, Date of Approval or Rejection Certificate or Signatur thorized I idu d Designation No. ____ ..______ Der-0,57 _,,ao6 SD4R514M 0: Steve Ouellette l FAA Form 337 (12-88) EFTA00277580 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the work performect 1•1908JE under Banyan Air Service; Avionics Division work order #71301 completed on a2s/a6 A. Installed ari AirCell Iridium ST-3100 P/N 400-10680-001 and removed a previously installed AirCell AGT.01 P/N 900001-2. Minor wiring changes were made at the mating connector IAW installation manual P/N 800-10680 Rev. B dated June 2005. B. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapterg,'Options,3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 2, paragraphs 24 & 25 and the aircraft's maintenance manual. . 111W: C A functional test of the .ab6e/Aniprrient has been performed FAR25.1309 and FAR25 .1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. The weight change is negligible. the equipment list was updated to reflect this change. E. Instructions for continued airworthiness is attached.. END ❑ Additional Sheets are Attached EFTA00277581 Instruction for Continued Airworthiness for AirCell ST 3100 Aircraft Subscriber Equipment System Installed on Boeing 727-100 N908JE S/N 20115 Revision O. Dated: 9/17/2006 EFTA00277582 •• e EFTA00277583 • APPLICATION REVISIONS . DESC. NEXT ASSY USED ON REV DESCRIPTION DATE APPROVED ST 3100 ASE SYSTEM BARON 95-B55 A BASELINE RELEASE 2002-10-16 K. FRANTZ B SEE DCN 00179 2002-10-25 K. FRANTZ • ._,.... S a • • ALL SHEETS CARRY THE SAME REVISION LETTER a UNLESS OTHERWISE SPECIFIED e a DIMENSIONING & TOLERANCING bkW ASME Y14.5M-1994 DIMENSIONS ARE IN INCHES STANDARD TOLERANCES: x = ±. .1 )(X= ± .02 )(XX= ± .010 no d ..._.7 . AirCell, Inc. 1172 Century Drive Suite 280, Building B S Louisville, CO 80027 S APPROVED DATE PREPARED BY YEAR-M O-DA K. FRANTZ 2002-10-16 MECH DESIGN YEAR-MO-DA INSTRUCTIONS FOR CONTINUED Z. HOH 2002-10-16 AIRWORTHINESS ELEC DESIGN YEAR-M O-DA B. SOUKUP 2002-10-16 TECH SUPPORT B. NIELSON YEAR-MO-DA ST 3100 ASE SYSTEM 2002-10-16 --\ SYSTEMS YEAR-MO-DA K. FRANTZ 2002-10-16 ENGINEERING YEAR-MO-DA SIZE - CAGE CODE DRAWING NUMBER REV J. POLSON 2002-10-16 A 1NO67 . 820-10680-001 B FILE FORMAT: Microsoft Word 2000 SCALE: NONE WEIGHT: NA SH 1 of 8 FILENAME: 820-10680-001-B.doc 699-10077: A-SIZE SPEC TEMPLATE.DOC EFTA00277584 • •• EFTA00277585 p. p p TABLE OF CONTENTS p 1 GENERAL INFORMATION p 3 1.1 SCOPE OF THIS DOCUMENT p 3 1.2 TECHNICAL SUPPORT CONTACT INFORMATION 3 p 1.3 • GENERAL. NOTES 3 1.4 ADVISORIES 4 2 SYSTEM DESCRIPTION 4 9 2.1 TOP LEVEL SYSTEM CONFIGURATION 1 "4 2.2 OPERATION OF THE SYSTEM p 6 OPERATIONAL TIME LIMITS AND SCHEDULED MA p INTENANCE 7 4 UNSCHEDULED MAINTENANCE p 4.1 7 TROUBLESHOOTING PROCEDURE p 7 5 AIRWORTHINESS LIMITATIONS p 7 FIGURES AND TABLES Table 2.1-1 System Component Definition 5 Figure 2.1-1 Block Diagram of ST 3100 ASE System 6 ) ) • AirCell, Inc. SIZE CAGE CODE DRAWING NUMBER REV 1172 Century Drive e A 1NQ67 820-10680-001 B Suite 280, Building B FILE FORMAT: Microsoft Word 2000 SH 2 of 8 Louisville, CO 80027 FILE NAME: 820.10680-001-B.doc 699.10077: A-SIZE SPEC TEMPLATE.DOC EFTA00277586 'I EFTA00277587 GENERAL INFORMATION 1.1 SCOPE OF THIS DOCUMENT This manual defines the instructions for continued airworthiness (ICAW Subscriber Equipment (ASE) system. Th ) for an AirCell_ 3000 Series Aircraft e manual is written to demonstra and 25.1529. Specifically, this manual te compliance with FARs 23.1529 defines the instructions for the System (ST 3100). Model 3100 Satellite Telephone This manual is subdivided into sections to support the general operation, ST 3100 system. Section 1 defines gene inspection and maintenance of the ral information for the maintenan system. Section 2 provides general ce and airworthiness of the ASE information on the configuration an Section 3 presents a discussion of d operation of AirCell ASE systems the scheduled maintenance an op . Section 4 and Appendix A provide d era tio na l tim e limits for the system. instructions for system operationa maintenance and component replac l checks, troubleshooting, unscheduled ement. Section 5 provides a brief limitations for the ST 3100 system. statement addressing airworthiness 1.2 TECHNICAL SUPPORT CONTACT INFORMATION Technical support for AirCell products is available from 08:00 to 17:00 Unite Zone GMT —7 hours) Monday through d States Mountain Time (Time Friday. The contact information for Air follows: Cell Technical Support is as From a landline: Phone (in the US): 1.888.286.9876 (toll free) Phone (outside the US): 001.303.379.0278 (toll call) From an AirCell phone: From an Air Mode/AMPS phone (in the US): 611 (toll free) From a SAT Mode (Iridium) phone (w orldwide): 2471 (toll free) Email: customerservice@aircell.com Note: The toll free numbers for AirCe ll phones will only work for AirCell pro vided phones and services. 1.3 GENERAL NOTES • All pages in this document carry the sa me revision level. Revision status is on each page of this manual. indicated by a letter printed • The material in this manual is subje ct to change. Before planning or maintenance operation, check with performing any installation or AirCell Technical Support to verify that has the latest revision. this manual is complete and • AirCell, Inc. welcomes your comm ents, suggestions, and corrections include in your correspondence the concerning this manual. Please publication number, equipment part nu and a brief description of any problem or mber, page or figure number, consideration you noted. Please se nd your comments to: AirCell, Inc. Corporate Publication Coordinato r 1172 Century Drive Suite 280, Build ing B Louisville, Colorado 80027 cpc@aircell.com AirCell, Inc. SIZE CAGE CODE DRAWING NUMBER elf 1172 Century Drive Suite 280, Building B A 1NC)67 820-10680-001 REV B FILE FORMAT: Microsoft Word 20 Louisville, CO 80027 00 I SH 3 of 8 FILE NAME: 820-10680-001-B.doc 699-10077: A-SIZE SPEC TEMPLATE. DOC EFTA00277588 i EFTA00277589 1.4 ADVISORIES WARNING Statements in this section contain critical safety info rmation. Read these statements carefully before installing this unit. WARNING Observe standard safety precautions and wear safety glasses to prevent personal injury while performing maintenance on this unit in the aircraft . WARNING Shut off power before connecting or disconnecting the ST 3100 system, as voltage transients may damage the unit or the interface wiring. WARNING Components or subassemblies found in this unit may con tain materials such as beryllium oxide, acids, lithium, radioactive material, mercury, etc. that can be hazardous to your health. If the component enclosure gal is broken , precautions must be taken against personal contact or inhalation in accordance with OSHA requirements 29CFR 1910.1000 or superseding documents. AirCell strongly discourage s the opening or disassembly of sealed components. WARRANTY AND CERTIFICATIONS Any alteration of this product voids the FAA or FCC certific ation and the AirCell warranty. 2 SYSTEM DESCRIPTION The ST 3100 ASE system provides access to a range of two way communication options from an aircraft, including voice and data applications. With the ST 3100 system these services are available when the aircraft is in the air or on the ground. The AirCell satellite mode communications link is provided using the 1600 MHz Iridium LEO (Low Earth Orbit-485 miles altit ude) satellite network, which provides coverage from the ground up over the entire surface of the earth. 2.1 TOP LEVEL SYSTEM CONFIGURATION The ST 3100 system consists of a number of primary sys tem components. The heart of the system is the ST 3100 ASE Transceiver, which includes internal elec tronics to support operation in the Iridium satellite network. Other system components include the externa lly mounted antenna, a low loss coaxial cable, and various user interfaces including multiple ASE handsets (up to 9), an RS -232 data port, and an audio panel interface. AirCell' AirCell, Inc. SIZE CAGE CODE DRAWING NUMBER REV 1172 Century Drive A 1NO67 820-10680-001 B Suite 280, Building B FILE FORMAT: Microsoft Word 2000 SH 4 of 8 Louisville, CO 80027 FILE NAME: 820-10680-001-B.doc 699-10077: A-SIZE SPEC TEMPLATE.DOC EFTA00277590 .. I EFTA00277591 AAt4r4fAco ed The primary components of an ASE system include Line Replaceable Units (LRUs) and AirCell specifi assemblies (such as coaxial cables or wiring harnesses) that are manufactured or purchased by the system installer. A list of the LRUs and specified assemblies is provided in Table 2.1-1, and a representative block diagram is provided in Figure 2.1-1 to demonstrate the interconnection of a typical ST 3100 system. For detailed information on the system components, please refer to ST 3100 ASE System installation manual (AirCell document 800-10680), or contact AirCell Technical Support for assistance. Table 2.1-1 System Component Definition System Designatio Description AirCell PN. Approved AirCell PN Component n Alternate(s) of Alternate System LRU ST 3100 Transceiver ASE Transceiver 400-10680-001 none Transceiver LRU 3/8 ATR Width 3000 Series :Mounting Tray Mounting Tray 800007-1 Mounting Rails 151-10689-001 System Wiring Specified 26 wire System NA Harness Assembly Harness ASE Handset LRU Flush Mount Standard ASE 400-10001-10X* Handset 400-10035-00X* ASE Handset Portable Coilcord ASE Handset 400-10015-00X* Custom Retractable ASE Handset 400-10019-00X* Satellite LRU 1600 MHz Satellite 1600 MHz Satellite 015-10683-001 ASE Antenna, 015-10306-001 ASE Antenna, ASE Antenna Patch Style Blade Style Satellite Channel Specified Low Loss Coaxial NA Coaxial Cable Assembly. Cable (vendor item)" "X" designates the color of the ASE handsets. ** The system coaxial cable is a required item that is not provided by AirCell. The system installer will need to purchase this item from an approved vendor as defined later in this document. AirCell, Inc. SIZE CAGE CODE DRAWING NUMBER REV (MICA: 1172 Century Drive Suite 280, Building B A 1NQ67 FILE FORMAT: Microsoft Word 2000 820-10680-001 B I SH 5 of 8 Louisville, CO 80027 FILE NAME: 820-10680-001-B.doc 699-1C077:A-SIZE SPEC TEMPLATE.DOC EFTA00277592 • . . . .. : I EFTA00277593 ASE SATELLITE \/ ANTENNA I ASE SYS HS CNCTR .44111 .\_ AIRCRAFT ASE HANDSET CHANNEL FUSELAGE ASE SYS HS CNCTR 1=1--M120 ASE HANDSET CHANNEL 0 ASE SYSTEM XCVR ASE 5Y5 HS CNCTR p Mffal ASE HANDSET CHANNEL SAT ANTENNA ID D TO AUDIO PANEL AUX CNCTR NO CONNECTION ASE SYS RS232 CNCTR I TO RS232 DATA TERMINAL SYS CNCTR TO AIRCRAFT POWER (2.8 Vdc) I I AIRCRAFT FUSELAGE I I Figure 2.1-1 Block Diagram of ST 3100 ASE System I Note: Each 'Handset Channel' listed above is capable of supporting up to 3 ASE handsets, making it possible to integrate up to 9 handsets in the ST 3100 system. I 2.2 OPERATION OF THE SYSTEM The user interface and operation of the ST 3100 system is designed to be very similar to the operation of a I terrestrial cellular or PCS phone. Some key features of the ST 3100 system are as follows: • The system will power up when the avionics master switch for the aircraft is powered on. The AirCell system is always on when the avionics master is powered on. • ' The Satellite mode network provides coverage anywhere on (or above) the surface of the earth with a I clear view of the sky in all directions. • To place a call from the system handset, the user must verify that the system is 'in service'. SAT mode calls are typically dialed as international long distance calls (00 + country code + phone number). After dialing, the user must press the " SND " key on the handset, and the phone call will proceed as a typical cellular or PCS call. At the completion of a call, the user may press the " END " key to terminate the call. • The user may receive incoming (ground to air) phone calls depending on the in service condition. The user can answer these calls by pressing the " SND " key on the handset. • Data calls can be made from Air to Ground over the ST system by connecting a Data Terminal Equipment device (such as a PC) to the RS-232 port of the system. The ST system has a built in modem function, so some user setup of the DTE will be required. ) More detailed operating instructions are provided for this system in the ST 3100 User's manual (AirCell document 810-10680). ) AirCell, Inc. SIZE CAGE CODE DRAWING NUMBER REV 6N_j.ri•Celf 1172 Century Drive Suite 280, Building B A 1NQ67 FILE FORMAT: Microsoft Word 2000 820-10680-001 B SH 6 of 8 Louisville, CO 80027 FILE NAME: 820-10680-001-B.doc 699-10077: A-SIZE SPEC TEMPLATE.D GC I EFTA00277594 I EFTA00277595 uctict)ticccfoC INTENANCE 3 OPERATIONAL TIME LIMITS AND SCHEDULED MA sys tem is des igne d and man ufac ture d to be mai nten anc e free after installation. As a result of The ST 3100 des ign, ther e are no ope ratio nal time limi ts or per iodic maintenance checks or procedures that must be this sys tem . Insp ecti ons and /or sys tem veri fica tion che cks are only required in the event of a performed for the 4 of this document. system failure (On Condition), as defined in Section the sys tem ope rato r may per form a visu al insp ecti on of the various system components at the As an option, aircraft manufacturer. or oth er per iodi c mai nten anc e inte rval as defi ned by the aircraft annual inspection, 4 UNSCHEDULED MAINTENANCE is des igne d for "On Con ditio n" mai nten anc e only . In the event of a system failure, the The ST 3100 system use r/air craf t ope rato r is adv ised to follo w the trou bles hooting procedure defined in Appendix A of this system orm ing the bas ic pro ced ure , the use r will eith er hav e returned the system to normal manual. After perf additional guidance. operation, or should contact AirCell technical support for proc ess of per form ing the trou bles hoo ting pro ced ure , auth orized field service personnel are Note that, in the ing interfaces, or (with prior to wiri ng har nes ses , RF cab le ass emb lies , mo unt permitted to perform repairs ell Tec hnic al Sup por t) to rem ove and rep lace any of the primary system Line Replaceable approval from AirC or subassembly level , und er any circ ums tanc es, auth oriz e field rep air Units (LRUs). AirCell does not on any LRU . Sea led LRU s sho uld alw ays be retu rne d to the AirCell FAA Repair Station for maintenance evaluation and repair. 4.1 TROUBLESHOOTING PROCEDURE e to iden tify sim ple pro blem s that may be iden tifie d and/or resolved with simple Appendix A provides a guid on and test pro ces ses . It is adv ised tha t the pro ced ure in this appendix should be performed field inspecti ell Tec hnic al Sup por t for add ition al inst ruct ion. No spe cialized tools or equipment are before contacting AirC required to perform this procedure. a step in this pro ced ure is not clea r, or the resu lts of a procedure are not conclusive, the In the event that t for assistance. test operator should feel free to contact Technical Suppor 5 AIRWORTHINESS LIMITATIONS ST 310 0 ASE sys tem is a non -cri tica l com mun icat ions system. In accordance with FAR The AirCell end ix G) and FAR 25.1 529 (wit h Par t 25 App end ix H) this system has no 23.1529 (with Part 23 App aircraft. Airworthiness Limitations for either Part 23 or Part 25 s limi tatio ns sec tion is FAA app rove d and spe cifie s maintenance required under Sections The airworthines eral Avia tion Reg ulat ions unle ss an alte rna tive pro gra m has been approved. 43.16 and 91.403 of the Fed DRAWING NUMBER REV AirCell, Inc. SIZE CAGE CODE A7-fr C e lf 1172 Century Drive Suite 280, Building B A 1NQ67 FILE FORMAT: Microsoft Word 2000 820-10680-001 SH 7 of 8 B Louisville, CO 80027 FILE NAME: 820-10680-001-B.doc 699-10377: A-SIZE SPEC TEMPLATE.DOC EFTA00277596 'a . . % . . . I EFTA00277597 t.d S • 0 P 9 P Appendix A ST 3100 ASE System Troubleshooting Procedure p p a a a A tirr AirCell, Inc. SIZE CAGE CODE DRAWING NUMBER F. kj ell 1172 Century Drive Suite 280, Building B A 1NQ67 820-10680-001 B FILE FORMAT: Microsoft Word 2000 I SH 8 of 8 Louisville, CO 80027 FILE NAME: 820-10680-001-B.doc 68410077,S. SPEC TEMPLATE.DOC a EFTA00277598 • EFTA00277599 EFTA00277600 TrCell' Symptom Possible Cause Discussion Verification Step(s) The handset display should always O Verify that the aircraft power system (master avionics switch) is on. Symptom 1 Power is not available to ASE be illuminated when power is O Verify that the ASE system circuit breaker is closed. System Handset Display is applied to the ASE transceiver. O Visually inspect the displays of all installed handsets in the system. If all handsets not illuminated arc off, proceed to the next bullet in this list. If most handsets are illuminated, but Because the failure of a handset display is unlikely, a `dead' display one is not, then proceed to Symptom 2. (One or more suggests that there is a problem with O If all handset displays are dead, the problem is likely in the power system wiring handsets integrated in the input power to the ASE system. before the ASE transceiver. Visually check the system connections and the wiring . system, no handset In the event that the one or more harness leads between the transceiver and the aircraft power system. Repair or displays are handset display(s) are not reconnect any obvious problems. illuminated) illuminated, the user/operator should O If needed, ring out the power lines per the system wiring diagram. Repair any verify that aircraft power is on and broken wires or rework to match the system wiring diagram. . available to the ASE transceiver. O If this procedure does not resolve the problem, contact AirCell Technical Support - for additional guidance. In a system with multiple handsets, O Some ASE systems integrate multiple handsets. If more than one handset is Symptom 2 Bad connection or faulty wiring if some handsets are operating and installed on the system, check the display on all handsets. If only one of multiple Handset Display is between handset and some arc not, then it is likely that handsets is not illuminated, then the problem is either a bad handset or in the handset not illuminated transceiver. either the handset is bad or the connection/ wiring harness between that handset cradle and the transceiver. wiring between the handset and the O Perform a visual inspection to verify that ail connections are made in accordance (ASE System has or transceiver is faulty. with the system wiring diagram. Correct any obvious problems. multiple handsets, O If all system connections are correct, then switch the `dead' handset with a known Bad handset good handset and retest the system. If the handset is still dead in the new location, and the displays of most handsets are on, then the handset is bad. Contact AirCell Technical Support for repair/replacement but one handset is not instructions. illuminated.). O If the known good handset is now dead, then the problem is in the system wiring/connections between the handset and the transceiver. Ring out the lines per . the system wiring diagram. Specifically check for 9V power and ground leads on the HS power line from the transceiver system connector. Repair any broken wires or rework the system wiring harness to match the wiring diagram. O If this procedure does not resolve the problem, contact AirCell Technical Support • for additional guidance. A-1 ST 3100 ASE System Troubleshooting Procedure 820-10680-001, Rev B Ceti- IC tttik MiLttlettAdt s .0 EFTA00277601 WINO mi, wut:.‘soilmOlpf EFTA00277602 ‘4110 46P 4019 -.4m! VaY INV 10, INF 4mY 441,,w 400.4, wov011OtiOWWW 14104rOVINVOtiOVIOU Symptom Possible Cause • Discussion Verification St,9(s) Symptom 3 Possible Cause 3A' The ST 3100 transceiver operates in Verification Test 3A Handset Display is System antenna does not have Satellite (SAT) mode. When in O Verify that the system SAT antenna has a clear LOS to the sky in all directions. A illuminated and Line of Sight (LOS) view to coverage the ST system should clear LOS is defined to exist when there are no obstructions (such as buildings, display indicates no satellite. detect and register for SAT mode trees, vehicles etc) that are higher than 30 degrees above aircraft horizon in any signal for Satellite service. direction. This should never be a problem in flight. • (SAT) mode. If the system does not register, then O Use the handset to enter the SAT lock mode (FCN,.3, 3) keys on the handset. The it is likely that either the antenna handset will display the word "IRIDIUM" when the SAT mode is locked. does not have a LOS to a satellite O Once the LOS has been established the system should register on the SAT network (3A), or there is a problem with the within 60 seconds. The system is registered when the "NO SVC" indicator is not RF channel in the aircraft (3B). In visible on the handset display. this condition, it is unlikely that 0 If the "NO SVC" indicator extinguishes, then the SAT mode is engaged, and the there is a problem with the system problem is resolved. The user may choose to make a test call and verify the transceiver. operation the system. • 0 If the "NO SVC" indicator stays illuminated, then the system cannot register, and it is likely that there is an installation or equipment problem. Either contact AirCell Technical Support for additional guidance, or proceed to Verification Test 3B. No Satellite mode Possible Cause 3B Verification Test 3B signal There is a problem with the O While the aircraft is on the ground, perform a visual inspection of the ASE system Satellite RF channel. satellite antenna. Verify that the antenna is installed to the aircraft fuselage in accordance with the system antenna installation drawings. Verify the mechanical integrity of the antenna, and that the antenna is reasonably free of dirt, oil, ice and • • other undesired coatings. O Visually inspect the RF satellite channel, including the coaxial connections to the antenna and the system transceiver. Inspect the coaxial connectors to verify that they are connected in accordance with the system wiring diagram, and that they are not damaged. Look for breaks, kinks or other damage to the coaxial cable. 0 The user is authorized to correct installation errors (such as cabling errors), or to repair minor damage (such as broken coaxial connections, damaged coaxial cables, etc). The user is not authorized to open or modify sealed LRUs. O If these steps do not resolve the problem, contact AirCell Technical Support for additional guidance. Other conditions For all other conditions, contact AirCell Technical Support for guidance. • A-2 ST 3100 ASE System Troubleshooting Procedure 820-10680-001, Rev B • • • EFTA00277603 Form Approved --tt OMB No. 2120-0020 For FA Use Only IdentificatioA US Department MAJOR REPAIR AND ALTERATION Office 0f Transportation (Airframe, Powerplant, Propeller, or Appliance) (5 Federal Aviation Administration O-rspo- iq INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). _ Make Model 1. Aircraft Boeing 727-100 Serial No. Nationality and Registration Mark 20115 USA N908JE 2. Owner Name (As shown on registration certificate) Address (as shown on registration certificate) J.E.G.E, Inc. 103 Foulk Road STE 202 Wilmington, DE. 19803-3742 3. For FAA Use Only -,i-c:;;;;:.,:•• _ •*4-4 .:, 4. Unit identification 5. Type Alteration Unit Make Model Serial No. Repair AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE U.S. Certificated Mechanic SD4R514M AVIONICS DIVISION Foreign Certificated Mechanic Radio Class 1635 NW 51st Place El Certificated Repair Station Limited Airframe Ft. Lauderdale, FL 33309 Manufacturer D. I certify that the repair and/or alteration made to the unit(s) *dentified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Indivi October 10, 2006 c.- ---- Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given persons s• • cified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is e. APPROVED O REJECTED FAA Fit. Standards Manufacturer Inspection Authorization Other (Specify) BY Inspector FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of orized Ind* - I Designation No. October 10, 2006 SD4R514M Steve Ouellette FAA Form 337 (12-88) EFTA00277604 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) The purpose of this 337 is for the work performed on N908JE under BanYan Air Service; Avionics Division work order #71301 completed on October 4, 2006. A. Installed an AirCell Iridium Antenna P/N S67-1575-109 in accordance with DER Services drawing number 2006-173-1 approved per FAA form 8130-3 signed by Robert Belgau DERT designation number DERT-510024-CE. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapter 11, sections 3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 3, paragraphs 43 & 44 and the aircraft's maintenance manual. A log book entry and equipment list was generated to reflect the above installation. The weight change is negligible. the equipment list was updated to reflect this change. Instructions for Continued Airworthiness is "on condition only." END Additional Sheets are Attached EFTA00277605 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS October 07, 2006 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL TYPE (AirPlane. Radio, Helicopter, etc) NAME OF APPLICANT Boeing 727-31 Airplane Banyan Air Services LIST OF DATA IDENTIFICATION TITLE DER Services Effectivity: Drawing: S/N: 20115, T/N: N908JE • 2006-173-1 Iridium Antenna Installation STA 515 - BTWN S-2R & S-3R _ Rev. I/R -i.'-...*-::i:Dtd. 27-Sep-06 . END END END END END_ END_ END_ END_ END_ END_ ___END_END Note: This aircraft is effected by AD 98-11-03 RI. Certification to FAR 25.571, Damage - tolerance and fatigue evaluation of structure may be required. Per Advisory Circular 25.1529-1 Instructions for; Continued Airworthiness of Structural Repairs on Transport Category Airplanes, the damage tolerance and fatigue evaluation of the structure must be performed before 4/11/2003. Notes: . . 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering design data and is not installation approval. (Ref. 8110.45 8/30/02 for more info) 2) This approval is valid for the aircraft model and serial number listed below 3) This approval is based on FAA Approved structural analysis on file at DER Services office in Ft. Lauderdale, FL. or DER Services, Inc. office in Birmingham AL. Model No. 727.-31 Serial No. 20115 PURPOSE Approve data for low profile antenna installation (structural aspects only, Static Analysis) OF DATA APPLICABLE REQUIREMENTS (LIST SPECIFIC SECTIONS) CAR 4b.200, 4b.201, 4b.202, 4b.260, 4b301, 4b302, 4b303, 4b.306 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I (We) Therefore pi Approve these data SIGNATURES) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Robert J. Belgau DERT-510024-CE Structures — , FAA FORM 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. F2006-173 EFTA00277606 - a EFTA00277607 8 7 6 5 4 3 2 1 EFTA00277608 GENERAL NOTES: DESCRIPTION DATE APPROVED I/R INITIAL RELEASE 09-27-2006 1. FABRICATE PART(s) AS SHOWN. STA 515.00 FASTENER CODES ❑ LU 2. BEFORE INSTALLATION OF DOUBLER, ROLL TO ❑ MATCH AIRCRAFT MOLD LINE RADIUS. ITEM DESCRIPTION D D itj NASI097AD4 (TY'P 50 PLS) x 3. BREAK ALL SHARP EDGES .0201.030 R. 64510428AD 3 (TYP 8 PLS) x 4. TREAT ALL REWORKED AREAS USING ALODINE 1201S (PER MIL-C-5541, CLASS 1A) AND TVVO (2) COATS OF EPDXY POLYAMIDE PRIMER (PER MIL-P-233377, TYPE I). 5. FINISH ALUMINUM PARTS USING ALODINE S - 2R EXISTING FUSELAGE SKIN 1201S AND TWO (2) COATS OF EPDXY PRIMER. (REF) S - 3R 6. MAINTAIN MINIMUM 2D + 1/16" EDGE DISTANCE C FOR ALL FASTENERS ON DETAILS; MINIMUM 2D EDGE DISTANCE ON ASSEMBLY. STA 510 STA 520 C 7, ALL FASTENERS ARE TO BE INSTALLED IN TRANSITION-FIT HOLES. HOLE TOLERANCE PER NAS618. EXISTING BONDED -o 8. ALL FASTENER LENGTHS ARE TO BE VERIFIED STRAPS 4- FOR TOLERANCE PRIOR TO INSTALLATION. (REF) 9. INSTALL ALL PARTS AND THREADED FASTENERS WET USING PR1436G TYPE III SEALANT ON ALL FAYING SURFACES. B B 50 COUNTERSUNK RIVET NAS 1097AD4 - 2 OPL 10. RESTORE ORIGINAL FINISH PER B727 M.M. 51-21. 8 RIVET - NUTPLATE MS20426AD3- 2 QPL 11. PROTECT REWORKED AREA AGAINST 4 4 SCREW MS24694C55 OPL CORROSION PER B727 SRM, CHAPTER 51-10-2. 3 4 NUTPLATE NAS 1 473A3 QPL 2 1 DOUBLER - INTERNAL 0.050" 2024-T3 00 -A -250/5 QPL 12. REFERENCE 8727 S.R.M, CHAPTER 51-30 FOR 1 1 L1 CPS -IRIDIUM ANTENNA 567- 1575-109 QPL FASTENER REMOVAL AND INSTALLATION PROCEDURES. ITEM QTY NAME PART NUMBER MATERIAL MIL -SPEC VENDOR 13. REINSTALL ALL ADJACENT STRUCTURE Ports List REMOVED TO FACILITATE ANTENNA CRAVING CREATED FCN, INSTALLATION. BANYAN AIR SERVICE CRAVING SIZE, B lJ DER SERVICES 2100 kV 6.311 STREET, Suitt C-I09, FT. LAITIRDAI.E rl. =9. (9509TI.3B32, FAX(954)971-3059 A nes date Is provided as • CONFIDENTIAL AND PRIVILEGED UNLESS OTHERWISE SPECIFIED DATE APPROVED TITLE A 14. BEAD SEAL ANTENNA WITH PRC 1422 SEALENT. 00C(JMENTOebecin BANYAN AIR SERVICE DIMENSIONS ARE IN INCHES 09-27-2006 IRIDIUM ANTENNA INSTALLATION & DER 5•Mass. My oN use of raproductco *afoul the expnrssed tten coneare of DER Sareloatbaxpassly latedcius. UNSPECIFIED TOLERANCE STA 515 - BTWN S-2R & S-3R My M4064 of 0is docurnerd incluctify INN not Potted IS) rasldabon DRAVN BTU W.D.OLIVERI A/C Typr BOEING REV 15. REVISE AIRCRAFT RECORDS TO REFLECT In pen riOsoul send.n consent ci DER Son nee Is expressly Portirkeen. This aporovei Es Pew] upon AN. mod sr-esti@ ID DER Servicsrs torn BANYAN AIR SERVICE FRACTIONS ANGLES DECIMALS .X ± .1 CHECKED BY' R.J.BELGAU Nod No ' 727-31 T'G2006-173-1 I/R INSTALLATION. .15 MACH. al So. Offs of nsporl corrphillon. My iddlaccial data Mich Osamu reale:is. may mull b afnenftn; 0r COnctoslco(s) ±1/32 .2 FORMED .XX t .03 STRESS BY' W.D.OLIVERI TAIL No. r N908JE PROJ 2006-173 -SCALE. N.A. expressed haneln .XXX_ t .010 APPROVED BY. R.J.BELGAU SERIAL No 20115 STRL INSTL SHEET 1 OF 3 8 7 5 4 3 2 1 J EFTA00277609 8 7 6 5 4 3 2 EFTA00277610 IRIDIUM ANTENNA INSTALLATION 01.00 @ STA 515.00 - BTWN S-2R & S-3R STA 510 CONNECTOR CUTOUT IN SKIN STA 520 EXISTING D EXISTING BONDED STRAPS FUSELAGE SKIN (REF) (REF) EXISTING BONDED STRAPS (REF) C 4- B 4 4 EXISTING BONDED STRAPS (REF) EXISTING FUSELAGE SKIN SECTION A-A A (REF) DER SERVICES ,'),`." 2006-173-1 TN. deer b prose.. as • COW IDENTIX. AND PFUYILED0ED DOCUMENT between VIEW LOOKING UP BANYAN AIR SERVICE DER SerrIces. My Other use or (spenducton ecnotrt De esOreesslawrInen mos. of DER SessIcse N.sweaty MPMM. My ndsyse of Pis Ovarrent bOumrq (bvl rot ernlletl b) qv...Jon b pert with. written consent of DER Se.. M -Drew 2700 N.W. 62/10 STREET, 6us C-109, SIZE DRAWN BY, REV FT. LAUDERDALE. R 33XS. lortedden. T. *pus.* Is based v.n dab ft.., sessiebb lo DER Sen.. Rom BANYAN AIR SERVICE (554) 571.3832. FAX (M.) . 714.0 B W.D.OLIVERI UR SOME STRUCTURE REMOVED FOR CLARITY al be SIR ot report corrode., My ...Ye/ dale. eh. becomes rear.. may row. In •^r•ran5 eye con:Susie*/ bIreesedb... SERIAL No. . 20115 SCALE 3= 4 SWET 2 OF 3 8 I 7 I 6 5 4 3 2 3 • EFTA00277611 8 7 6 5 4 3 2 1 EFTA00277612 01.62 01.00 FASTENER CONNECTOR PATTERN CUTOUT (TYP 6 PLS) ITEM 2 / DOUBLER FABRICATION 00.20 ANTENNA USE NUTPLATE AS MOUNT HOLE PATTERN FOR RIVET (TYP 4 PLS) HOLES. (TYP 8 PLS) 4.50 R 0.25 (TYP 4 PLS) 4.13 0 0 0 0 0 0 3.66 0 0 3.19 O O O O 3.19 2.72 -0 o - 0 2.24 0 0 0 o o o 4- ( 1.78 0 Ck O o 1.38 o O ED O 0 O o 1.29 B B 0.84 O 0.38 O O O O O O O 0 0.00 o CO tO CI O W. to Cl CD CO 1O cn O CO LO C') O cr) t•- e ill CO N CO CD 0, cO CV CO O o o o cNi N (vi ri 4 4 4 A A DER SERVICES NQG2006-173-1 This data le ortroldid ae • CONFIDENTIAL AND PRA/ILEDDED DOCUMENT betetern BANYAN AiR SERVICE DERE...Mon. Any caw, ow or reproduction without the eapreesed rattan oznunt of DER BeMc.e4 expreeffy forbidden. Any mg.*. of AN 6:.O...nt I:Coelho (but not United quotation in pert without written coreenl of DER Serelpe b eefe...fY 2700 N.W. 132.3 STREET. &Ate C-I09, SIZE ERAVN BY. REV FT. LAUDERDALE. FL. 11309. forbidden. Thts *pommel Is bawl upon date mad. sysliftes to DER Sonia. eon BANYAN AIR SERVILE (p6e) 971-3832. FAX (964)971-3059 W.D.OLIVERI l/R el Ow erne of 1900 etelpfli3on. Any edditionei date. which becomes eveiletie, rney refue tr. emending tne oonclusicn(s) freereased herein. SERIAL No. .2O 1 1 5 SCALE 0.5 = 1 S ET 3 C.F 3 8 7 6 5 fi 4 3 2 EFTA00277613 C , Form Approved • OMB No. 2120-0020 For FA Use Only US Depa rtment Of Transportation MAJOR REPAIR AND ALTERATION Office Identification Federal (Airframe, Powerplant, Propeller, or Appliance) Aviation Administration SO- (3 DO -17 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model 1. Aircraft Boeing 727-100 Serial No. Nationality and Registration Mark 20155 USA N908JE 2. Owner Name (As shown on registration certificate) Address (as shown on registration certificate) J.E.G.E. Inc. 103 Foulk Road, Ste 202 Wilmington, DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE U.S. Certificated Mechanic SD4R514M AVIONICS DIVISION Foreign Certificated Mechanic Radio Class 1635 NW 51st Place 0 Certificated Repair Station Limited Airframe Ft. Lauderdale, FL 33309 Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authoriz_e_ii.i l yl . 7 .2; ic /d 8 November 2004 -‘,/ e Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is II APPROVED II REJECTED FAA Flt. Standards Manufacturer Inspection Authorization Other (Specify) BY Inspector FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group X Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. _ _---) 19 November 2004 SD4R514M C Steve Ouellette FAA Form 337 (12-88) EFTA00277614 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the FAA approval of the new flight manual supplement on N908JE under Banyan Air Servive, Avionics Division work order #68062. A. Removed existing TDR-94 transponders P/N 622-9210-003 and routed to the manufacture for upgrade to P/N 6252-9210-007 to provide flight ID. System ground and flight checked good. B. The weight & balance is not affected and equipment list was updated. C. Instructions for continued airworthiness are "on condition only". END G' fin Og(10.b ffL, ❑ Additional Sheets are Attached EFTA00277615 ••--- . -I . Form Approved ' OMB No. 2120-0020 0 For FAA Use Only US Department Of Transportation MAJOR REPAIR AND ALTERATION Office Identification (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration 5a —r 51)6-1 7 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions a disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model 1. Aircraft Boeing 727-100 Serial No. Nationality and Registration Mark 20115 USA N908JE 2. Owner Name (As shown on registration certificate) Address (as shown on registration certificate) J.E.G.E, Inc. 103 Foulk Road STE 202 - Wilmington, DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Alteration Unit Make Model Serial No. Repair AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE U.S. Certificated Mechanic SD4R514M AVIONICS DIVISION Foreign Certificated Mechanic Radio Class 1,2,3 1635 NW 51st Place a Certificated Repair Station Limited Airframe Ft. Lauderdale, FL 33309 Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date . 7 Signature of Authori 4i .s.Jualit . 1/6/1•1/9e-:-/ a 4:2 C7 (71 ‘C Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given personsirfi ci ed below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is APPROVED • REJECTED FAA Flt. Standards Manufacturer Inspection Authorization Other (Specify) BY Inspector FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature o d Indivi / Designation No. / r Ahi/6Arc e__ c72O) C SD4R5 14M Steve Ouellette FAA Form 337 (12-88) EFTA00277616 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with allprevious alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the work performed on N908JE under Banyan Air Service, Avionics Division work order #68062. A. Installed a Universal Avionics Systems Corp. Terrain Avoidance and Warning System in accordance with SIP Technical Services, Inc. data list 7280-DL-001-501, Rev. H dated December 2002 or later. (STC# ST09951SC) B. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapter 11, sections 3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 2, paragraphs 24, 25, and 28, AC25-23 and the aircraft's maintenance manual. C. A functional test of the above equipment has been performed FAR25.1309 and FAR25 1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. A weight & balance was calculated. An FAA approved flight manual supplement provided with the above STC, Document No. 7280-FM-001, dated December 13, 2002 or later E. Instructions for continued airworthiness provided by SIP Technical Services Report No. 7280-ICA-001 Rev. F dated June 6, 2002. END *Ay ❑ Additional Sheets are Attached EFTA00277617 pniteb tutes jArrirriCn Prpartrrttnt of Zrartsportation - grbrral czAfliatinn cAbmirtistration , upialentenial `Tuve Certificate teinh.fe t.471 ST09951SC e°rl teak 1,:s,tezeti/o . SIP Technical Services, Inc. 10107 McAllister Freeway San Antonio, TX 78216 a‘e.it,72/<cikelled/f bre dindal4vzs rz./sticevu‘4.-ivz.s . cu.-44,1 dead; ejange art de; *//ze tleJe 7y r1.4 dercAr ens .yieceAdife., ,eevinee4s de izievz-c-vakeaeJis "e9ece.:vnuva.4.t ei4:7tr."/ 4b c/a; Civil Air Refez44iva.s. 6isr:;th2aigivekcl n'iv0cale A3WE ,d&zZe.- Boeing .A6esehi.• 727-100 Series .gesc. , 04"evz c>4.F1//ze Installation of a Universal Avionics Systems Corporation Terrain Awareness Wiazife. - and Warning System in accordance with SIP Technical Services, Data List 7280-DL-001-501, Revision H, dated December 5, 2002, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Document Number 7280-FM-001, dated December 13, 2002, or later FAA approved revision is required. eindg7cyzeit a..s.• Compatibility of this design change with previously approved modifications must be the determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, holder shall give the other person written evidence of that permission. ce,-10cate and14 6:- .111/2/2O/66.iip ektet tcs/ficiza 9ga eizhr c3 cae.e<av:se e...ilae°4‘ede;/ dt; .../ge/z71.44e:stkzkv, €/° Jarre feei .1‘.4.3/2eze, reecch geeicv , a te..rmZaaleiva ev -a, '._/gotallevt.AeGitzikeafinciliark. :gale e3:rev/i&alei -vz, .• August 02, 2001 :2ale rez,...uaed; Lale 9/4,sa.z/ue ..December 13, 2002 gale ez,,vezaeAl.• (Sign ture) ces Co er, Spe ial Ce cation Office South4vest Region (Title) ent not exceeding 3 years, or both. Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonm FAR 2I.47. Page 1 of 2 This certificate may be transferred in accordance with FAA Form 8110-2(10-68) EFTA00277618 . . EFTA00277619 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-100 WITH UNIVERSAL AVIONICS SYSTEMS CORPORATION DUAL MULTISENSOR UNS-ID+ FLIGHT MANAGEMENT SYSTEMS REG #. N908.TE SERIAL #. 20115 This supplement must be attached to the FAA Approved Airplane Flight Manual when the Universal Avionics System Corporation UNS-1D+ Flight Mana•ement System (FMS) is .in§talled in accordance with field approved 337 dated 1Voll (2200 )4' . The M information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement; consult the basic Airplane Flight Manual. FAA APPROVED Gary Justice Principal Avionics Inspector Federal Aviation Administration Flight Standards District Office #17 Ft. Lauderdale, FL 33315 Date: NOV 8 2004 Rev. 0 '.'Pl‘ge 1 of 9 EFTA00277620 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 Table of Contents SECTION PAGE GENERAL 3 LIMITATIONS 3 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 3 PERFORMANCE 6 RECORD OF REVISIONS Revision Pages Description Approved 0 All Initial Release . NOV 8 71104 Date: NOV 8 2004 Rev. 0 Pige 2 of 9 EFTA00277621 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION 1- GENERAL 1. INSTALLATION DESCRIPTION. The Universal Avionics Systems Corporation dual FMS's use inputs from their integral GPS Receivers, Navigation Receivers and DME Transceivers to provide a blended position for navigation. Each FMS contains an internal TSO C129a GPS sensor (GNSS 2400), which is cross-wired to the other FMS such that both systems have GPS 1 and GPS 2 data as inputs. The FMS's receive air data parameters from an Air Data Computer. A Data Transfer Unit (DTU100) is used to load periodic navigation data base updates via zip disks. The systems provide navigation and steering data to the flight director/autopilot system. Refer to the appropriate Operator's Manuals as applicable. The FMS's contain software SCN 802/902 which provides capability for point-to-point navigation, as well as SIDs, STARs, holding patterns and GPS approaches. These SCN's comply with requirements of TSOs C115b and C129a Class Al when interfaced to the internal GPS sensors which are TSO C129a Class Al/B1/C1 certified The UNS- 1D+ FMS may contain either a GLONASS sensor or a GPS sensor, depending on hardware configuration. Lateral and Vertical deviations are provided for En Route, Terminal Area and Approach operations, including GPS overlay approaches. Approaches may be FCS coupled both laterally and vertically. Multi-Mission search patterns are available with SCN 902. 2. LATERAL NAVIGATION APPROVALS. Provided the FMS multi-sensor navigation system is receiving usable signals, it has been demonstrated capable of and has been shown to meet the accuracy specifications of: VFR/IFR En Route domestic, Terminal and Instrument Approach (LOC, BC, GPS and GPS-overlay NDB, VOR, VOR-DME and RNAV) operations within the U.S.National Airspace System using the WGS-84 coordinate reference datum in accordance with the criteria of Advisory Circular AC 20-130A and AC 25-15. Satellite navigation data is based upon use of only the Global Positioning System (GPS) operated by the United States. Additionally, Russian GLONASS satellites provide increased accuracy but are not used for integrity or Receiver Autonomous Integrity Monitoring (RAIM) calculations or predictions. The dual FMS installation with dual internal GPS sensors, as installed, complies with the requirements of FAA Notice 8110.60 for GPS primary means of Class II navigation in oceanic and remote airspace (including NAT MNPS in accordance with AC 120-33 and 91-49), when used in conjunction with the Universal Flight Planning Program, PN 10751 with SCN 24.0 or later FAA approved version. This does not constitute an operational approval. Date: NOV 8 2004 Rev. 0 Page 3 of 9 EFTA00277622 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION I — GENERAL (cont.) RNP- Approvals The dual multi-senSor FMS installation integrates dual GPS sensors and complies with equipage and accuracy requirements of FAA Order 8400.12A paragraph 12b(4), for operations in RNP-10 airspace. This does not constitute an operational approval. This installation also complies with equipage and accuracy requirements of AC 90- 96 paragraph 7b(1), 7d(3)(a) 2, 7d(3)(e) for BRNAV (RNP-5) when operating in Class I airspace, without time limits. The table details time limitations placed on RNP-10 and BRNAV operations with minimum sensors in NAV mode. Sensors RNP-10 Limitations RPN-5 (BRNAV) Limitations Available minimum dual FMS's required) (minimum single FMS required No time limitation when used in 1 GPS only N/A Conjunction with UFP VOR/DME only N/A No time limitation DME/DME only N/A No time limitation 3. VERTICAL NAVIGATION APPROVAL The dual Flight Management Systems, as installed, meet the requirements for VFR/IFR En Route, Terminal Area and Approach VNAV operations in accordance with the criteria of AC 20-129 and AC 90-97, paragraph 7.a (2). SECTION II - LIMITATIONS 1. The FMS Operator's Manual, Report Nos. 2423sv802/902 Dated 9/16/03 (or later revision) must be available to the flight crew whenever navigation is predicated upon the use of the Universal Avionics Flight Management System. 2. The system must utilize software version SCN 802/902.X, where X represents FAA approved minor changes. 4. IFR En Route and Terminal navigation are prohibited unless the pilot verifies the currency of the database or verifies each selected Waypoint for accuracy by reference to current approved data. Date: NOV 8 2004 Rev. 0 Page 4 of 9 EFTA00277623 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION 11-- LIMITATIONS (cont.) 4. Instrument approaches must be accomplished in accordance with approved instrument approach procedures that are retrieved from the FMS database. The FMS database must incorporate the current update cycle. a. Instrument approaches must be conducted in the Approach-mode, and GPS Integrity monitoring (when using GPS for approach guidance) must be available at the Final - Approach Fix, as indicated to the pilot by the 'GPS INTEG' amber annunciator being off. b. When an alternate airport is required by the applicable operating rules, it must be served by an approach based on other than GPS navigation, the aircraft must have operational equipment capable of using that navigation aid, and the required navigation aid must be operational. c. GPS can only be used for approach guidance if the reference coordinate datum system for the approach is WGS-84 or NAD 83. d. GPS will remain selected for all GPS approaches and any approach with a "G" suffix to the approach identifier in the navigation database. GPS will be deselected for any pilot-defined VOR or VOR/DME" RNAV approaches. e. Pilot-defined IFR approaches must be defined using Waypoint coordinates from FMS's navigation data base. f. The FMS's are approved for pilot-defined VFR approaches as a VFR pilot aid only. NOTE: All sensors remain selected for VFR approaches. 5. When operating in other than oceanic and remote regions, the aircraft must have other approved navigation equipment installed and operating appropriate for the route of flight. 6. Displayed FMS navigation p'arameters are referenced to Magnetic North, and operation of the aircraft is limited to latitudes between N730and S600, unless magnetic variation is manually entered by the flight crew. 7. When using VNAV, the Altimeter on each pilot's panel must be used as the altitude reference for all operations. 8. ' Fuel display parameters are advisory only and do not replace primary fuel quantity or fuel flow gauges for fuel load and range planning. SECTION III - EMERGENCY PROCEDURES NO CHANGE TO AFM. Date: NCV 8 2004 Rev. 0 Page 5 of 9 EFTA00277624 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION IIIA - ABNORMAL PROCEDURES 1. If 'GPS RAIM' becomes unavailable (as indicated by a Message and `GPS INTEG' (amber annunciation), continue navigating using the GPS equipment or revert to an alternate means of navigation appropriate to the route and phase of flight, as necessary. When continuing to use GPS navigation, position should be verified every fifteen minutes using another IFR-approved navigation system. 2. Should an FMS system component fail, in most cases the CDU will go blank or the 'FMS MSG' light will flash. Depressing the MSG key will display the Message Page, which will indicate the component which has failed. 3. If sensor information is intermittent or lost, utilize remaining operational navigation equipment as required. 3. The FMS and associated components are protected by the following circuit breakers: C/B Name Amps Location Bus FMS No. 1 5 Pilot 28VDC Avionics Bus No. 1 (Triple-Fed) FMS No. 2 5 Copilot 28VDC Avionics Bus No. 2 (L GEN) FMS DTU 1 Pilot 28VDC Avionics Bus No. 1 (Triple-Fed) SECTION IV - NORMAL PROCEDURES 1. OPERATION Normal operating procedures are outlined in the FMS Operator's Manual, Report No. 2423sv802/902. 2. NAVIGATION DATABASE VERIFICATION. After power-on self tests have been completed, the INITIALIZATION page will appear. The term `NAV DATABASE EXPIRES' followed by a date will be displayed. If the actual date is later than that which is displayed, the FMS will notify the pilot with a 'DATABASE EXPIRED'-message. Refer to the Operator's Manual for navigation database update instructions. 3. SYSTEM ANNUNCIATORS Each FMS has the following annunciations presented on the Universal Electronic Flight Instrument (EFI) displays (refer to the EFI Operator's Manual, as applicable) : MSG Illuminates and flashes in conjunction with the CDU to indicate a message is to be acknowledged on the MESSAGE page. SXTK Illuminates to indicate that selected crosstrack is active. FHDG Illuminates to indicate that the FMS is in Heading sub-mode. APPR Illuminates to indicate that an Approach has been activated. GPS INTEG Illuminates to indicate GPS Integrity is outside of the allowable limit for phase of flight (2.0nm En Route, 1.0 nm Terminal and Approach transition, and 0.3 nm Final Approach segment). Date: NOV 8 2004 Rev. 0 Page 6 of 9 EFTA00277625 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION IV - NORMAL PROCEDURES (cont) 4. AIRCRAFT INTEGRATION a. Universal Avionics EFI display of FMS information 1) FMS information is displayed on the Universal Electronic Flight Instrument (EFI) displays. The associated EFI Control Panel provides control of each display. See the appropriate Operator's Manual, as applicable, for each EFI display system. 2) Lateral deviation display scaling meets with requirements of TSO C129a and AC 20-130A (5.0 nm full scale for En Route, 1.0 nm for Terminal operations, and 0.3 nm for Approach operations). 3) b. En Route and Terminal Area Flight Control System Operation 1) With `FMS'-mode selected by using the EFI Control Panel, the respective FMS information can be presented as Flight Director steering commands by pressing the [NAV] button of the FCP-65 Flight Control Panel. 2) With reasonable navigation data being displayed, the steering information can be Autopilot-coupled, to the pilot's or copilot's Flight Director system, by pressing the 'AP ENGAGE' - button on the APP-65A Autopilot Control Panel. c. Approach Operations NOTE: ILS approaches can be retrieved from the Jeppesen database and linked to the flight plan, but cannot be armed or activated as FMS approaches. The FMS can be used to provide navigation up to the final approach course, at which point the EFI must be changed to display raw ILS data which can be coupled to the Flight Control System (FCS). NOTE: GPS will remain selected for GPS and GPS-overlay approved approaches from the navigation database, as well as pilot-defined VFR approaches. Refer to Operator's Manual, Section V, Approach Procedures. Date: NOV 8 2004 Rev. 0 Page 7 of 9 EFTA00277626 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION IV - NORMAL PROCEDURES (cont) c. Approach Operations (cont.) LOC, B/C, GPS, NDB, RNAV, VOR, VOR/DME, and VFR approaches may be linked into the flight plan and then laterally and vertically coupled to the FCS as follows: 1) Approach Transition: When an entire approach transition (e.g., procedure turn, DME arc, etc.) is to be flown, first arm the approach on the FMS (ARM APPR). If the FMS is not armed manually it will arm automatically at 30nm from the airport. With the desired DIRECT TO or FROM/TO Waypoints selected, or the desired FMS Heading selected with INTERCEPT ACTIVE, select FCS `NAV'- mode by pressing the [NAV] button of the appropriate FCP-65 Flight Control Panel. When the FMS has automatically activated the approach, denoted by the 'APPR' annunciator displayed in the associated EFI display, press the [APPR] button of the Flight Control Panel. When the FCS has captured the "APPR" — mode, a white "VNAV" will appear on the PFD and a white VN on the ADI signifying the 'arming" of the VNAV mode. The "VNAV" and "VN" annunciation will turn to green in color when the FCS has captured the VNAV glideslope. See the EFI operator's manual for specific display annunciations. Continue monitoring both lateral and vertical deviations throughout the duration of the approach. If required, initiate 'Missed Approach Procedures' as described in the Universal Avionics Operator's Manual. 2) Heading Vectors: If given heading vectors by ATC to the final approach course, manually activate the approach on FMS NAV page 1/3. The FMS will enter the "FHDG" mode, the EFI display will now display final approach course data, and the INTERCEPT prompt on Nav page 1/3 will be active. When cleared to intercept final, press the "INTERCEPT "line select key to intercept final. Ensure that commanded heading mode is canceled. Select [APPR] on the FCS Flight Control Panel to capture and track the final approach lateral and vertical information. NOTE: Guidance is provided to the runway threshold or missed approach point. It is the pilot's responsibility to level out at MDA if the runway environment is not in sight. Date: NOV 8 2004 Rev. 0 '' 'Page 8 of 9 EFTA00277627 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION IV - NORMAL PROCEDURES (cont) 3) Press the APP-65A Autopilot Control Panel [AP ENG]-button to couple the AP to the selected FD. The Autopilot will track pseudo-Localizer and pseudo-Glideslope signals from the FMS. b. Advanced Approach Operations 1) Advanced approaches may be identified in the data base by the prefix "A" to the approach listed in the "ARRIVAL" page and in the navigation data base They are characterized by course changes on the final approach segment of greater than 6 degrees and/or having multiple flight path angles. To avoid excessive deviations from course and flight path, these approaches may need to be flown in FCS [NAV] mode until on the final leg of the approach. Select FCS [APPR] sequencing the final waypoint to engage vertically. c. Vertical Navigation 1) Vertical Navigation (VNAV) information is displayed on the EFI display and is available for enroute, terminal or approach descents. Pitch steering commands for enroute and terminal VNAV operations are not provided to the Flight Control System. SECTION V - PERFORMANCE DATA NO CHANGE TO AFM. Date: NOV 8 2004 Rev. 0 Page 9 of 9 EFTA00277628 ••• • EFTA00277629 . . Form Approved 0 • • OMB No. 2120-0020 For FAA Use Only i US Department • - 1- Of Transportation MAJOR REPAIR AND ALTERATION Office Identification Federal (Airframe, Powerplant, Propeller, or ApplianCe) Aviation ••• Administration , INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and -,I disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such- violation (Section 901 Federal Aviation Act of 1958). - —1 Make Model ; , O. Aircraft Boeing 727-100 i Serial No. Nationality and Registration Mark 20115 USA N908JE . 2. Owner Name (As shown on registration certificate) Address (as shown on registration certificate) J.E.G.E, Inc. 103 Foulk Road STE 202 - Wilmington, DE. 19803-3742 3. For FAA Use Only Tri't data identified h plies the applicable airworthines n..quirements is tot the above described aircraft. subj conformity is by a person lutorized In FAR 43, s on 43.7. d-e/ nature FMInspector 5 0 - r-.5 DO - 1 .- OCT 11 7004 Date ry - 4. Unit Identifi atio 5. Type Alteration •• Unit Make Model Serial No. Repair • •.i • ,..• (As described in Item 1 above) -s.-4. AIRFRAME POWERPLANT .i t ---,-• PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE U.S. Certificated Mechanic AVIONICS DIVISION Foreign Certificated Mechanic Radio Class 1,2,3 —.... 1635 NW 51st Place r Certificated Repair Station Limited Airframe Ft. Lauderdale, FL 33309 Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authori di ' lual /fA//44/16eW paC3 O c , Steve Ouellette — 7. Approval for Return to Service • Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of thil. . Federal Aviation Administration and is APPROVED I REJECTED _ FAA Flt. Standards Manufacturer Inspection Authorization Other (Specify) BY Inspector FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group ..... Date of Approval or Rejection Certificate or Signature of Aut • d Indio' Designation No. . . /9 A/47/ 106e2C_c:7,.: SD4R514M Steve Ouellete ----_—. FAA Form 337 (12-88) EFTA00277630 NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be . .compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. i• rr. Description of Work Accomplished f• (lf more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the work performed on N908JE under Banyan Air Service, Avionics Division work order #68062. A. Installed an Artex ELT406-2HM per Artex installation document number 570-5000, Rev. A, dated 12/10/02 mounted in unpressurized aft compartment. The antenna is mounted in the aft tail section. A remote switch is mounted in cockpit in the copilot's insrtument panel. An aural activation monitor is mount within the vacinity of the ELT per the installation document listed above. 1 B. The above installation Aidsi3e&efe,din.iccofdanceX4h. AC43.13-1B, Chapter 7, sections f. 1-5, AC43.13-1B Chapter 11, sections 3-17,AC43.13 -2A ChApter 1, AC43.13-2A Chapter r 2, paragraphs 24, 25, and 213,7AZ,431172A7Chapter 3;paragraph 38 and the aircraft's maintenance manual. • L. C. A functional test of the above equipment has been performed FAR25.1309 and FAR25 .1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not I exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. No Weight and balance was generated as the aircraft was weighed. E. Instructions for continued airworthiness is a battery due time change. This due date is reflected on the log book entry. Annual inspection is required per FAR 91-207 (d). END • .; 0 Additional Sheets are Attached EFTA00277631 Form Approved 0 OMB No. 2120-0020 For FAA Use Only .. US Department Of Transportation MAJOR REPAIR AND ALTERATION Office Identification Federal (Airframe, Powerplant, Propeller, or Appliance) . -- Aviation Administration _ INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and •disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such, ,' violation (Section 901 Federal Aviation Act of 1958). . Make Model 11. Aircraft Boeing 727-100 Serial No. Nationality and Registration Mark 20155 USA N908JE 2. Owner Name (As shown on registration certificate) Address (as shown on registration certificate) J.E.G.E. Inc. 103 Foulk Road, Ste 202 Wilmington, DE. 19803-3742 - 3. For FAA Use Only Tr': data identified herei complies the applicable ainvorthines rLquicements d is approv for the above described aircraft, sub' conformity s n by a person authorized in FAR 43, s on 43.7. NOV 8 2004 Ter, . , ., e) — f-S720 --/ 7 Date Startatura FAA Inspector - . 4. Unit Identificat 0 5. Type Alteration . Unit Make Model Serial No. Repair , AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE U.S. Certificated Mechanic SD4R514M AVIONICS DIVISION Foreign Certificated Mechanic Radio Class 1635 NW 51st Place 0 Certificated Repair Station Limited Airframe , Ft. Lauderdale, FL 33309 Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and . correct to the best of my knowledge. Date Signature of Au .er Indivi 5 ). A /0,-/e-A1,46-2 ,,, e (-1 V , Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given personsAoecified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is x APPROVED III REJECTED FAA Flt. Standards Manufacturer Inspection Authorization Other (Specify) BY Inspector FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group X Date of Approval or Rejection Certificate or Signature of Authorized Indivi ual Designation No. n X/1/ - o 76)- SD4R514M Steve Ouellette -7 1 — FAA Form 337 (12-88) • EFTA00277632 NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 0. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the FAA approval of the new flight manual supplement on N908JE under Banyan Air Servive, Avionics Division work order #68062. A. Removed existing UNS-1D Flight Management System (FMS) control display/computer units and routed to the manufacture for upgrade to UNS-1D+. Reinstalled UNS-1D+ FMS CDU computers. System ground checked good. B. A flight manual supplement has been generated, approved and incorportated into the existing flight manual. A weight & balance and equipment list update are not required. END • • •v-inc .q)4:11 A' A4 tit3O 0 Additional Sheets are Attached EFTA00277633 NV. 8. 2004 NOV. 9:50AM PYKA AEROSPACE NO. 2146 P. 3 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT UNIVERSAL AVIONICS TERRAIN AWARENESS WARNING SYSTEM (TAWS) AIRPLANE MAKE: BOEING AIRPLANE MODEL: 727-100 AIRPLANE SERIAL NO.: A/yog-j-t-- REGISTRATION NO.: c90 /A-5— This supplement must be attached to the FAA Approved Airplane Flight Manual when the airplane is modified by the installation of a Universal Avionics Terrain Awareness Warning System (TAWS) in accordance with FAA STC number ST09951SC. The information contained herein supplements or supersedes the basic Airplane Flight Manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this document, consult the basic Airplane Flight Manual. APPROVED: S. Frances Cox, Manager Special Certification Office Federal Aviation Administration Ft. Worth, Texas 76193-0190 DATE: October 25, 2004 Page 1 of 9 EFTA00277634 • EFTA00277635 NOY. 8. 2004 9:50AM PYKA AEROSPACE NO. 2146 P. 4 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 LOG OF REVISIONS REV, DESCRIPTION REVISED PAGES APPRD. BY DATE IR New supplement All S. Frances Cox 12-13-2002 Allow use of CDU or MFD A display. Format and editorial All See cover page 10.25.2004 corrections throughout. FAA APPROVED Date: October 25, 2004 Page 2 of 9 EFTA00277636 • 1 tat EFTA00277637 NOV. 8. 2004 9:51AM PYKA AEROSPACE NO. 2146 P. 5 Dot. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 TABLE OF CONTENTS SECTION PAGE SECTION I - GENERAL 4 SECTION II - LIMITATIONS 4 SECTION III — NORMAL PROCEDURES 5 1. Operation 5 2. Cold Temperature Operations 5 3. Systems Test 5 4. Pop-Up Terrain Display 6 5. System Annunciators 7 SECTION IV - EMERGENCY/ABNORMAL PROCEDURES 9 EMERGENCY PROCEDURES 9 ABNORMAL PROCEDURES 9 1. Circuit Breakers 9 2. Use of TERR INHIBIT switch 9 3. Response to TAWS Warnings 9 4. Response to Glideslope Deviation Alerts 9 5. Use of Flap Override Switch 10 ff CTION V - PERFORMANCE 10 SECTION VI - WEIGHT AND BALANCE 10 FAA APPROVED Date: October 25, 2004 Page 3 of EFTA00277638 . .- EFTA00277639 , NOV. 8. 2004 9:51AM PYKA AEROSPACE Na 2146 P. 6 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 SECTION 1 — GENERAL This Supplement provides general information for the Enhanced Ground Proximity Warning System installation. The aircraft is equipped with a Universal Avionics TAWS system. The system uses inputs from the air data computer No. I, navigation receiver No. 1, radio altimeter, and the Universal Avionics UNS-1 Flight Management System (FMS) , and an internal terrain database to provide basic GPWS alerts and terrain alerts The TAWS alerts provide the crew with aural and visual indications of possible inadvertent flight into terrain. TAWS alerts are generated if one or a combination of the airplane's: 1) vertical speed, 2) rate of closure to terrain, 3) accumulated altitude loss, 4) airspeed, flap and /or gear configurations or 5) glideslope deviation is unsafe given the airplane's radar altitude and phase of flight. Terrain alerts are generated by comparing aircraft position and altitude to the EGPWS terrain database. This system also provides "Flight Plan Look Ahead" terrain alerts and warnings by comparing the FMS flight plan to the terrain database SECTION II - LIMITATIONS The TAWS display will be used for situational awareness only. Navigation must not be predicated upon the use of the TAWS. The 3-1) view provides no attitude information. To avoid giving unwanted terrain alerts, the TAWS terrain alerts must be inhibited by pressing the TERR INHIB switch when landing at airports that are not included in the airport database or when landing at an airport other than the airport in the FMS flight plan. Deviation from Air Traffic Control Clearances is authorized to the extent necessary to comply with TAWS warning. The use of terrain awareness warning and terrain display function is prohibited during QFE operations. The current local altimeter setting must be entered in the pilot's altimeter for proper terrain alerting. The TAWS database and alerting algorithms do not account for man made obstructions FAA APPROVED Date: October 25, 2004 Page 4 of 9 EFTA00277640 3 r EFTA00277641 NOV. 8.2004 9:51AM PYKA AEROSPACE NO. 2146 P. 7 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 SECTION III — NORMAL PROCEDURES 1. Operation All aircraft crew interface is conducted through the Universal Avionics display, either multi- function display (MFD) or FMS control display unit (CDU), and system annunciator switches. TAWS terrain information may be presented on either an MFD or a CDU. The TAWS requires inputs from the following systems; radio altimeter, air data computer, VHF navigation receiver, FMS, gear position and flap position. 2. Cold Temperature Operations TAWS uses barb-corrected altitude as the reference for Forwared Looking Terrain Alerts (FLTA). TAWS does NOT compensate the baro altitude input for non-standard temperature lapse rates that may be encountered in extreme cold conditions, causing degraded FLTA operation. Basic ground proximity warning modes (1 through 6), as well as Premature Descent Alert (PDA), are radio altitude based and not affected. In extreme cold conditions, the aircraft will be operating at a lower altitude than indicated, thus resulting in TAWS alerts being delayed or missing. The color-banding on the TAWS display will be offset by the cold temperature altitude error. When operating into and out of airports where cold temperatures exist, the crew should be aware of the difference between the indicated baro altitude and the true altitude and the effect this has on FLTA and the terrain display. To determine the effect on FLTA warnings consult the Airman's Information Manual Chapter 7 paragraphs 7-2-3d and 7-2-3e. 3. System Tests BUILT IN TEST TAWS has a Built-In-Test (BIT) function which includes Power-Up Self Tests, Initiated Tests and Continuous Tests. Where there has been degradation in capabilities that result in TAWS being unavailable, BIT annunciates the fact to the flight crew via a GPWS FAIL or TERR 1NOP Lamp. PRE-FLIGHT TESTS A TAWS Self Test should be conducted prior to each flight. Momentarily press the GPWS TEST annunciator. The following indications confirm proper TAWS operation: PULL-UP Annunciator Illuminated TERR Annunciator Illuminated BELOW G/S Annunciator Illuminated G/S INHIBIT Annunciator Illuminated TERR INHIBIT Annunciator Illuminated FAA APPROVED Date: October 25, 2004 Page 5 of 9 EFTA00277642 . EFTA00277643 NO. 2146 P. 8 C. 2.;04 is PYKA TAWS System Doe. No. 7280-1, . 1, Rev A AFM Supplement for Issue 092401 Boeing 727.100 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 tinued) SECTION III - NORMAL PROCEDURES(Con GPWS FAIL Annunciator Illuminated GPWS TEST Annunciator Illuminated TAWS Terrain Display Test Image (Colored Bars) Aurel Annunciations "TERRAIN, TERRAIN" "PULL UP, PULL UP" "DON'T SINK" "SINK RATE" "GLIDESLOPE" "TOO LOW TERRAIN" "TOO LOW GEAR" "TOO LOW FLAPS" "FIVE HUNDRED" TA W S wi ll reb oo t. Du rin g thi s tim e the GP W S FAIL and TERR Once the test is complet e, lit an d a TA W S FA IL me ssa ge wi ll be ge ne rated on the MFD INOP annunciators will remain until the system is operational. (approx one min) of pre ssi ng the GP W S TE ST an nu nc iat or ag ain within five NOTE: As a result S computer will tia tin g thi s tes t, the tes t wi ll can cel an d the TA W seconds of ini continue to operate without rebooting. 4. Pop-Up Terrain Display p vie w of the TA W S dis pla y wi ll "p op -up " on the MFD or In the event of terrain alert, the ma po p-u p and revert to the cti on ke y on the dis pla y wi ll rem ov e the CDU. Pressing any fun selected display function. rai n co nfl ict s are de pic ted by a sta r sh ap ed Te rra in Threat Symbol. Both Prospective ter wa rni ng s are a flashing red nu nc iat ed wi th thi s sy mb ol. Te rra in Warnings and Cautions are an sy mb ol. Te rra in thr eats along pic ted by a fla sh ing ye llo w symbol while Terrain cautions are de pre dic ted fir st po int of conflict wh ite sy mb ol an d rep res en t the the flight plan are depicted by a between the flight plan and terrain TA W S dis pla y ind ica te a Te rra in Al ert (3 0-s ec on d warning). RED threat "stars" on the " on the TA W S dis pla y ind ica te a Terrain Caution(60 -second warning) YE LL OW thr ea t "st ars FAA APPROVED Page 6 of 9 Date: October 25, 2004 EFTA00277644 _ ••••• "••••• EFTA00277645 NOV. 8. 2004 9:52AM PYKA AEROSPACE NO. 2146—P. 9" Doc. No. 7280-FM-001, Rev A Issue 092401 TAWS System AFM Supplement for S.I.P. Technical Services Inc. 10107 McAllister Freeway Boeing 727-100 San Antonio, TX 78216 SECTION 1.1 1 PROCEDURES Continued WHITE advisory alert " stars" on the TAWS display indicate a fligh t plan terrain conflict These alerts are annunciated by a "star" on the display shortly after a VNAV altitude is entered into the flight plan or when a procedure (STAR or approach) containing altitud es is linked to the flight plan. Flight plan terrain advisories do not require immediate action but indicate that adhering to the flight plan as entered will cause a future terrain alert. Waypoints and altitudes should be checked for accuracy. 5. System Annunciators The following system annunciators are provided for the system; A. PULL UP Red PULL UP annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates whenever TAWS has detected terrain in the aircraft's immediate flight path. The annunciator will remain illuminated until the terr ain has been cleared. Aural annunciations of "TERRAIN, TERRAIN, PULL UP" or "PU LL UP, PULL UP" are also provided whenever the red PULL UP annunciator illuminates. B. BELOW GS Amber BELOW GS annunciators are located on the Captain's and Firs t Officer's instrument panel. This annunciator illuminates on approach whenever the TAWS has detected that the aircraft is at least 1.3 dots below the glideslope. This annunciator remains illuminated until the aircraft has returned to within less than one dot of the glideslope. Aural warnings of "GLIDESLOPE-GLIDESLOPE-GLIDESLOPE" sound until the aircraft has returned to within less than one dot below the glidepath. The aural annunciation may be canceled by pressing the BELOW GS armunciator/switch. How ever, the BELOW GS annunciators will remain illuminated. If the aircraft goes below the glideslope after the aural warning and light annunciation has gone out, the light and aural warning will again sound. C. GPWS FAIL Amber GPWS FAIL annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates if the TAWS has fail ed. FAA APPROVED Date; October 25, 2004 Page 7 of 9 EFTA00277646 • EFTA00277647 NOY. 8. 2004 9:53AM PYKA AEROSPACE N0. 2146 P. 10 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 SECTION UI - NORMAL PROCEDURES (Continuedi D. GPWS TEST GPWS TEST switches are located on the Captain's and First Officer's instrument panel shared with the GPWS FAIL annunciator. This switch is utilized to perform a self-test of the TAWS system. E. TERR Amber TERR annunciators are located on the Captain's and First Officer's instrument panel. The "TERRAIN, TERRAIN" aural warning paired with a visual alert is indication of reduced terrain clearance. F. TERR INOP Amber TERR INOP annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates when the terrain function is inhibited by TERR INHIB switch, terrain database is invalid or failed, terrain alert function is inoperative due to hardware failure or lack of a required input such as position or altitude. G. TERR INHIB Blue TERR INHIB annunciator/switch is located on the Captain's instrument panel adjacent to the TERR INOP annunicator. This annunciator/switch is illuminated white visible only when the TERR DRIB is active. FAA APPROVED Date: October 25, 2004 Page 8 of 9 EFTA00277648 EFTA00277649 NOV. 8.2004 9:53AM PYKA AEROSPACE -NO. 2146 — P. 11' Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.1.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 SECTION IV - EMERGENCY/ABNORMAL PROCEDURES EMERGENCY PROCEDURES No change to basic Airplane Flight Manual ABNORMAL PROCEDURES 1. Circuit Breakers The TAWS system is protected by the following tip-five circuit breakers: NAME LOCATION AMPS BUS GPWS P-18 5 28 VDC Ess. 2. Use of TERR INHIB switch. The Terrain Awareness Display inhibit switch (TERR INHIB) must be placed in the INHIB position in the following conditions: 1-Whenever the FMS in the Dead Reckoning (DR) mode 2-Within 15 nm of approach or landing at an airport not contained in the TAWS database. NOTE: When an off airport landing is required the FLTA and PDA functions should be inhibited by activation of the TERR INHIB switch. 3. Response to TAWS Warnings When an aural `TERRAIN, TERRAIN, PULL UP" or a red PULL UP warning light annunciates, execute a positive pull up maneuver, apply maximum rated thrust, and ascend to at least the best climb angle until the warning ceases. Notify ATC if action requires deviation of ATC cleared flight plan. When an aural "CAUTION TERRAIN", "TOO LOW TERRAIN," "SINKRATE" SINK," "TOO LOW FLAPS" or `TOO LOW GEAR" caution annunciates, initiate corrective action to remove the cause of the warning. 4. Response to Glideslope Deviation Alerts When the BELOW GS annunciator illuminates and an aural "GLIDESLOPE" annunciation alert occurs, initiate corrective action to fly the airplane back to the glideslope centerline. To inhibit the "GLIDESLOPE" annunciation on back course approaches, select the BELOW GS warning light/switch. The glideslope inhibit function is only available below 2000 ft AOL when the BELOW GS annunciator illuminates. FAA APPROVED Date: October 25, 2004 Page 9 of 9 EFTA00277650 I I EFTA00277651 NOV. 8. 2004 9:53AM PYKA AEROSPACE NO. 2146—P. 12 Doc. No. 7280-FM-001, Rev A Issue 092401 TAWS System S.LP. Technical Services Inc. AFM Supplement for 10107 McAllister Freeway Boeing 727-100 San Antonio, TX 78216 SECTION IV - EMERGENCY/ABNORMAL PROCEDUR ES (Continued) 5. Use of Flap Override Switch When landing with less than normal flaps, the FLAP OV ERRIDE switch should be usesd to prevent the 'TOO LOW FLAPS" aurel annunciation, SECTION V - PERFORMANCE No change to basic Airplane Flight Manual. SECTION VI - WEIGHT AND B4LANCE Refer to applicable weight and balance document. FAA APPROVED Date: October 25, 2004 Page 10 of 9 EFTA00277652 • EFTA00277653 Form Approved MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 US Department 01 transportation (Airframe, Powerplant, Propeller, or Appliance) For FAA Use On y Federal Aviation Office Identification Administration _ 50-r-37,0- r7 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-.1 (or subsequent revision thereof) for instruc • ns and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC 103 FOULK RD STE 202 WILMINGTON DE 19803-3742 3. For FAA Use Only 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. ---, Certificated Repair Station X RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer LIMITED A/F & ENG. D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and desc . ed on tti reverse o attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Ra) ulation4 and that th information furnished herein is true and correct to the best of my knowledge. \ \ Date Signature of Authorized Individual ' 6/12/02 \ _, i• Christopher Houseworth. Inspector. \ I 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manndr pr cribed by the 0 REJECTED ,..., Administrator of the Federal Aviation Administration and is CI APPROVED Other (Specify) FAA Flt. Standards Manufacturer Inspection Authorization Inspector BY, Person Approved by Transport FAA Designee X Repair Station Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual 6/12/02 Designation No. 1 .- C..- . EYKR782D John K. Urso. Inspector. -- ' & 6 • FAA Form 337 (12-88) EFTA00277654 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) N908JE, BOEING 727-31, S/N 20115, W.O. 18046 REFERENCE F.A.A. FORM 337 DATED 7/2/01 INSTALLING A UNIVERSAL AVIONICS CORP. UNS-ID FLIGHT MANAGEMENT SYSTEMS (FMS) WITH INTEGRAL GPS SENSORS. RECONFIGURED AIRCRAFT WIRING TO PROVIDE V-NAV DISPLAY INFORMATION ONLY, FROM THE EXISTING # I AND # 2 UNS-ID FLIGHT MANAGEMENT SYSTEMS. THIS MODIFICATION AS ACCOMPLISHED PER THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY F.A.A. FROM 8110-3 RESPECTIVELY: WIRING DRAWINGS: • B727-16236-410, REV A, DATED 4/16/02, SHEETS 1 THRU 5, TITLED - NO. 1 FLIGHT MANAGEMENT SYSTEM. • B727-I6236-411, REV A, DATED 4/16/02, SHEETS 1 THRU 5, TITLED - NO. 2 FLIGHT MANAGEMENT SYSTEM. REFERENCE F.A.A. FORM 8110-3 DATED 4/19/02 BY SYSTEMS AND EQUIPMENT DER NO. DERT510087-NM. ACCOMPLISHED OPERATIONAL CHECKS PER UNIVERSAL AVIONICS CORP. RETURN TO SERVICE MAINTENANCE AND CHECKOUT PROCEDURES MANUAL NO. 34-60-21, DATED 19 MARCH 2001 WITH NO DISCREPANCIES NOTED. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 1 OF 5, DATED 06/19/2001, WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE REQUIRED F.A.A. APPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236-100, REV A, SHEETS 1 THRU 9, DATED 5/8/02 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END ❑ Additional Sheets Are Attached -A- U.S. G.P.O 1990-761-753 EFTA00277655 Apr-19-02 08:08A N J Curran 352 243 1011 P_O2 'f DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS April 19, 2002 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio. Helicopter. etc) NAME OF APPLICANT Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-410, Revision A, dated NO. 1 FLIGHT MANAGEMENT SYSTEM April 16, 2002 B727-16236-411, Revision A, dated NO. 2 FLIGHT MANAGEMENT SYSTEM April 16, 2002 PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) CFR TITLE 14, CHAPTER 1, SUBCHAPTER C FAR 25.581 (a)(b)(1) FAR 25.1329 (h) FAR 25.1529 FAR 25.869 (a)(4) FAR 25.1351 (a) FAR 25.1581 (a)(b)(d) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c)(d)(e) FAR 25.1309 (a)(b)(c)(d)(e)(g) FAR 26.1381 (a)(b) FAR 25.1322 (b)(c) FAR 25.1431 (al(b)(c) CERTIFICATION - under authority vcsted by direction tithe Administrator and to accordance with conditions and Limitations or appointment under Part 18.1 or the Federal Aviation Regulations. data limed above and on attached shirts numbered NONE ts or have been examined in accordance with established procedures and found to comply with applicable requiremen the Federal Aviation Rezulations. II Recommend approval of these data I (We) Therefore El Approve these data (Systems & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) SIGNATUR . 0 DESIGN ED NGIN ' REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) DERT-510087-NM Systems & Equipment ‘44661--- Nor an J. an FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME: SC-727-FM S-REVA.DOC EFTA00277656 lot • I EFTA00277657 Jet Aviation Associates Ltd. AFM Supplement to Bldg. 1515 Perimeter Rd. The Boeing Company 727-31 Palm Beach Int'l Airport Serial No. 20115 West Palm Beach, FL 33406 FAA Form 337 FAA CRS EYKR782D Document No. B727-16236-100 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-31 REGISTRATION NO.: N908JE SERIAL NO.: 20115 WITH DUAL UNIVERSAL AVIONICS FLIGHT MANAGEMENT SYSTEMS (UNS1-D) INSTALLED This supplement must be attached to the FAA approved Airplane Flight Manual when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VOR/DME from the Collins No. 1 and No. 2 VOR/DME systems in accordance with manufacture's Installation and Checkout Manual No. 34-60-09, Rev. 2, dated August 15, 1997 or later approved revision and FAA Form 337, dated June 26, 2001. The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult the appropriate basic Airplane Flight Manual. FAA Approved: iriz Federal Aviation Administration Flight Standard District Office - 17 1050 Lee Wagener Blvd. Ft. Lauderdale, Florida 33315 FAA Approved Date: June 21, 2001 Revision A, Dated: 5/ Page 1 of 9 EFTA00277658 1 p EFTA00277659 Form Approved MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 US Dopartment . of Transportation ‘ (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Federal Aviation OffiQeldentificatjon, Administration • .604 7 SDU7 6s 3 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC. 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. - Foreign Certified Mechanic AIRFRAME 1,3. ---, 1515 PERIMETER RD. X Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer LIMITE A/F & ENG. D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse D or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual 1/14/02 , ,i John K. Urso. Inspector. x,I.Z.-- L/C-6 -- , 7. Approval for Return to Sery Pursuant to the authority given persons specified below, the unit identified in item 4 Was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Cs APPROVED ❑ REJECTED FM Flt. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee Person Approved by Transport X Repair Station Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 1/14/02 EYKR782D Ronald K. Bystrom. Manager Quality Assurance. 11-V. FAA Form 337 (12-88) EFTA00277660 NOTICE Weisht.andtalanca Or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all prev7ous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, S/N 20115, N9081E,'W/O 17454. ACCOMPLISHED AN ALTERATION TO THE CABIN INTERIOR FURNISHING ARRANGEMENT PREVIOUSLY INSTALLED UNDER PAGE AVJET STC SA3137SO, DATED 1/17/92, BY REMOVING THE FOLLOWING INTERIOR FURNISHINGS: DESCRIPTION POSITION P/N S/N F.S. R/H O/B AFT FACING SEAT. FORWARD SALON 303413-2 4350 401.94 R/H 1/B AFT FACING SEAT. FORWARD SALON 303413-10 4351 401.94 FORWARD R/H TABLE AND PEDESTAL FORWARD SALON A727-2531-001 NSN 438.50 UH AFT FACING SEAT CENTER LOUNGE 303413-1 4354 732.00 COFFEE TABLE AND PEDESTAL CENTER LOUNGE 727-2535-003 NSN 772.50 THIS ALTERATION WAS ACCOMPLISHED PER JET AVIATION DRAWING B727-17454-200, REV IR, DATED 1/2/02, SHEETS I & 2, TITLED - MINOR DEVIATION TO STC SA3137SO, THE LIMITED 727-100 GENERAL ARRANGEMENT. REFERENCE F.A.A. FORM 8110 DATED 1/6/02 BY STRUCTURES D.E.R. NO. DERT-810028-NE. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES REQUIRED FOR THIS ALTERATION. END ❑ Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277661 Form Approved MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 US Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Federal Aviation Office Identification Administration dift ---( 1 INSTRUCTIONS Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Boeing 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE Inc. 103 Foulk RD STE 202 Wilmington, DE 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERPLANT PROPELLER Type 1 APPLIANCE Manufacturer / 1 1 _ 61 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. X U.S. Certified Mechanic Gary K Palmer Foreign Certified Mechanic 6 Hyacinth Lane Certificated Repair Station #84544584AP Holbrook, NY 11741 Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual 08/01/01 _ Gary K Palmer 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is ►4, APPROVED 0 REJECTED FAA Flt. Standards Other (Specify) Inspector Manufacturer X Inspection Authorization BY Person Approved by Transport FAA Designee Repair Station Canada Airworthiness Group _. Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 08/01/01 84544584IA Gary K Palmer FAA Form 337 (12-88) EFTA00277662 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. Li B. Description of Work Accomplished (If more space is required, attach additional sheets, identify with aircraft nationality and registration mark and date work accomplished.) Fireblocked and upholstered existing, one (1) cabin single chair (Erda SIN 4359) in Townsend: Leather Lambskin Paris Alligator Embossed/Tipped Gold/Black, leather and two (2) cabin chairs (Erda S/N 4357 and 4358) in Clarence House: 10379B1S-37 Velours Mohair, fabric. D.E.R. Identification 62326-01. Fireblocked and upholstered existing, two (2) cabin single chair (Erda SIN 4360 and 4361) in Old World Weavers: Edmond Petit FMPOO 10004 Zoom, fabric. D.E.R. identification 64318-01. Fireblocked and upholstered existing, one (1) cabin single seat (Erda S/N 4354) and one (1) three section divan (Dettmers S/N 520, 521, and 522) in Geltman Ind.: Tiburon Tweed, fabric and one (1) divan (Dettmer SIN 516) in Clarence House: 10379BIS-37 Velours Mohair, fabric. D.E.R. Identification 65624-01. Fireblocked and upholstered existing six (6) single cabin seats (Erda S/N 4350, 4351, 4352, 4353, 4355, 4356), one (1) LH forward sidefacing divan (Dettmers S/N 517), and two (2) 3-place reclining divans (Dettmers S/N 518 and 519) in Old Weavers: EA81340013 Alfa Check, fabric and ETS J. Tassin S.A.: Mastic #19075, leather. D.E.R. Identification 66059- 01. All materials meet FAR 25.853(a) Appendix F, Part l(a)(1)(ii). Aircraft seat cushions have been fireblocked as per the requirements of FAR 25.853(c) Appendix F, Part II, Amendment 25 - 83. Results of sample burn tests are documented on S.A.I.'s Test Plan #7428, #7617, #7722, and #7759 and on attached DER approved 8110-3, Identification 62326-01, 64318-01, 65624-01, and 66059-01. Seat cushions have been tagged as being in compliance with the applicable regulatory requirements. Aircraft seatbelts were sent to Aircraft Belts, Inc. Repair Station YB1R632K for rewebbing, work order number 0046395 and reinstalled on the seats and divans. Replaced 19 each P.L. Porter SLO2300-28 seat recline Hydrolok and 6 each P.L. Porter SLO2300-21 divan recline Hydrolok. Hydroloks were replaced using standard interior practices. Installed Erda Hydro Legrest P/N 302617-3 and mechanical control single P/N MC15-36 on two (2) cabin single seats Erda seat S/N 4360 and 4361 in accordance with Erda drawing 302617 Rev B. Attached: FAA approved Townsend: Leather Lambskin Paris Alligator Embossed/Tipped Gold/Black, feather and Clarence House: 10379BIS-37 Velours Mohair, fabric. Test Plan #7428, form FAA 8110-3 dated 04/16/01, Judy Boggs, DERY-405020-CE. Identification 62326-01. Attached: FAA approved Old World Weavers: Edmond Petit FMPOO 10004 Zoom, fabric. D.E.R. Identification 64318-01. Test Plan #7617, form FAA 8110-3 dated 06/20/01, Judy Johnson, DERY-405020-CE. identification 64318-01. Attached: FAA approved Geltman Ind.: Tiburon Tweed, fabric and Clarence House: 10379B1S-37 Velours Mohair, fabric. Test Plan #7722, form FAA 8110-3 dated 07/12/01, Donna J. Parrish, DERY-410100-CE. Identification 65624-01. Attached: FAA approved Old World Weavers: EA81340013 Alfa Check, fabric and ETS J. Tassin S.A.: Mastic #19075, leather. Test Plan #7759, form FAA 8110-3 dated 07/24/01, Donna J. Parrish, DERY-410100-CE. Identification 66059-01. Attached: Aircraft Belts, Inc.: Certification/Packing List, work order number 0046395 consisting of 11 sheets. Attached: FAA form 8130-3 from P.L. Porter Controls, Inc.: SLO2300-21 and SLO2300-28 Hydrolocs tracking number 7723, 6751, 7176, 6759, 9495, 7367, 7368, and 9292. Pertinent data on file at International Jet Interiors, Inc. under W.O.#: 01119. Customer to install seats and divans in aircraft. Log entry has been made. END DI Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277663 (jv . C - Form Approved OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION U.S. Dc.-partinalt of (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Transportation Federal Aviation : Office Identification Administration s ... tlae) F5 De - t f--"--(--_ INSTRUCTIONS: Print or tspe all entries. See FAR 43.9, FAR 43 Appendix B , and AC43.9-1 (or subsequent revision thereof for instructions and disposition of this form. This report is required' by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed S1,900 for each such violation (Section 901 Federal Asia tion Act of 1958). . • Make Boeing . Model 727-31 • Serial No.20115 ' Nationality and Registration Mark N908JE . i. Aircraft . . Name (As shown on registration certificate). . Addri s (as shown, on registration certifikmte) . TEGR INC_ . 103 FOULKRD STE 202 2. Owner - WILMINGTON DE. 19803-3742 _ 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration ' AIRFRAME —- (As described in item 1 above) ^ )O • s . POWERPLANT PROPELLER . . Type . APPLIANCE . Manufacturer . 6. Conformity Statement A Agency's Name and- Address B Kind of Agency - C. Certificate:No. - TIMCO . U.S_CertificatxxiModianic ' DU4R141M Foreign Certificated- Mechanic Lake City Municipal Airport X Certificated Repair Station Lake City, FL 32025 .. . Manufacturer . ' D. I certify that the repair and/or alteration made to the units identified in item-4 4 •e, and described-on-the restat. oraltaeiuencut. hereto have been made in accordance with- ill, tiv-rnPnts of Part 43 of the U.S. Federal Aviation Regulaticess andthatthe informatices furnished herein. istrue and ccarectto the best of my knowlees , Date August 1, 2001 . Signature of Authorized Individnal Owen H. Pritchard II I. Approval- for Return- To-Sery cc Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Feclizal Aviatioa Administration and is El APPROVED D REJECTED FAA Flt.. Standards Manufacturer Inspection Authorization , Other (Specify! Inspector . FAA Designee X Repair Station - Person- Approved by Transport Canada BY • .. Aim() • .....4. Gro up - Data of Approval or Rejection Certificate or Designation Na 0 L. Palm ' Signatu c • Authorized Ind'y • ual August 1, 2001 • DU4R141M 1 / IIIIIP, On FAA Form 337 (12-88) EFTA00277664 NOTICE • Weight andbalance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued con fomity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is-required, attach additional sheets. Identify with aircraft nationality and registration mark and data work*Cornpleted_) BOEING SIN 20115 REG. NO. N908JE Page 1 August 1, 2001 The following major repairs were accomplished: NR# 27754 Repaired delaminated R/H Mid Flap Trailing Edge wedge by removing the delaminated section and fabricating and installing a new T/E wedge and strips IAW TIMCO REO-L00464 dated 7/17/01 FAA Form 8110-3 approved by DER Richard C. Saltivan DER # DERT-405157-CE dated June 19, 2001. NR# 27918 Repaired the delaminated and corroded Left Hand Inboard Mid Flap bottom upper Rock-shield panel by removing Rock-shield and corrosion, treated and primed area to be bonded,. impregnated fiberglass overlays as required, applied conductive coating and installed panel IAW B727 SRM 5-7-50-2, 51-40-8, MM 51-20-0 & SB 727-32-247 R1 dated June 5, 1981. SUMMARY 1. All work accomplished IAW Boeing SRM, TIMCO REO, FAA Form 8110-3 and Service Bulletin. 2. Records of all work accomplished is on file at this repair station under work order 185003. 3. Aircraft Weight and Balance updated accordingly. end Ei Additional Sheets Are Attached *- U.S. GOVERNMEqF PRLNTLVG OFFICE: 1992-769-012160157 EFTA00277665 • Form Approved (tt'' MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 US Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Federal Aviation Office Identification Administration INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC 103 FOULK RD STE 202 WILMINGTON DE 19803-3742 3. For FAA Use Only ino data identified herein with the applicabl: linverthines requirements aPPlovad, brthte:above described aircraft, subject try by person JUfilterini 3' s 431. ii SO —rD ,e)- 17- Date , ire A Inspector 4. Unit Identifica 99) 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1above) X POWERPLANT PROPELLER Type ' APPLIANCE Manufacturer ... 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. x Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer LIMITED AfF & ENG. D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Signature of Authorized Individ I Date -71WO/ John K. Urso. Inspector. C.- ,a441 --- 7. Approval for Return to Servl Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is a APPROVED M REJECTED Other (Specify) FAA Fit. Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Airworthiness Group Date of Approyal or Rejection Certificate or Signature of Authorized Individual Designation No. 7/2 1— /&/ EYKR782D Ronald K. Bystrom. Manager Quality Assurance FAA Form 337 (12-88) EFTA00277666 NOTICE Weight and balance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteratio n must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) AIRCRAFT: BOEING, TYPE: 727-31, S/N 20115, DATE: 06/14/2001, W.O. 16236, PAGE 1 OF 2 INSTALLED A SINGLE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY SYSTEM (TSO C113). THIS MODIFICATION WAS COMPLETED USING JET AVIATION DRAWING NO. B727-16236-270, ARGUS 5000 C/E MOVING MAP DISPLAY, REV. A, DATED 06/19/01. REFERENCE FAA FORM 8110-3, DATED 6/20/01, BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM. THE EXISTING LASERTRAK WIRING WAS RE-BUSSED DUE TO RELOCATION OF LASER TRAK C.D.I. THIS MODIFICATION WAS COMPLETED USING JET AVIATION DRAWING NO. 34-61-32-1, LAZERTRAK SYSTEM MODIFICATION, REV IR, DATED 5/24/01. THE STRUCTURAL INSTALLATION OF THE ARGUS:5(104/GFAMDVAIO MAP,DISPLAY nsum AND THE RELOC ATION OF THE LASERTRAK C.D.I. WAS COMPLETED USING JgTANTIM1'413119 , ff,ING:N9:1372-7-1p31V-i1270, ARGUS 5000/CE MOVING MAP EQUIPMENT INSTALLATION, REV. IR, DATED 05d9'/OrREffitEN r 41,0,-5115AIED 06/03/2001, BY STRUCTURES DER NO. DERT-810028-NE. 7110 A can, &A — THE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY IS A PICTORIAL NAVIGATION INSTRUMENT, WHICH PROVIDES VISUAL REFERENCE OF AIRCRAFT POSITION RELATIVE TO LANDING FACILITIES, NAVIGATIONA L AIDS AND SPECIAL USE AIRSPACE. THE ARGUS 5000/CE RECEIVES GEODETIC POSITION AND OTHER NAVIGATION INFORM ATION FROM THE NO. 1 UNS-ID FMS THROUGH AN EVENTIDE AVIONICS ARINC 419/429 ADAPTER UNIT AND THE AIRCRAFT'S NO. 3 HONEYWELL "LASERREF' INERTIAL REFERENCE SENSOR (IRS) DIRECTIONAL HEADING SYSTEM WHICH , PROVIDES MAP GRAPHICS AND BEARING ORIENTATION. THE FOLLOWING SWITCHES ARE LOCATED ON P16 FORWARD CONTROL STAND, BELOW THE ARGUS 5000/CE MOVIN G MAP DISPLAY: ARGUS INFO MOMENTARILY DEPRESSING THE ARGUS INFO ILLUMINATED (BLUE) SWITCH BRINGS UP INFORMATION ABOUT MAP OBJECTS ON THE ARGUS 5000/CE MOVING MAP DISPLAY. IF THE ARGUS INFO SWITCH IS PUSHED IN FOR 1 SECOND, THE ARGUS 5000/CE WILL RETURN TO THE MAP DISPLAY IN THE SAME MODE AND AT THE SAME RANGE SET, WHEN INFO WAS ENTERED. ARGUS SEL MOMENTARILY DEPRESSING THE ARGUS SEL ILLUMINATED (BLUE) SWITCH CYCI RS THE ARGUS 5000/CE DISPLAY THROUGH THE VARIOUS MAP OBJECTS. ARGUS TEST MOMENTARILY DEPRESS THE ARGUS TEST SWITCH TO ENABLE DISPLAY SIMULATION TEST. THE ARGUS 5000/CE MOVING MAP DISPLAY IS APPROVED FOR IFR ENROUTE NAVIGATION ONLY WHEN RECEIVING NAVIGATION INFORMATION FROM AN IFR APPROVED GPS, LORAN, OR OTHER LONG-RANGE NAVIGATION SYSTEM . THE ARGUS 5000/CE DATABASE MUST BE CURRENT (NOT EXPIRED). THE ARGUS 5000/CE IS APPROVED FOR USE AS A SUPPLEMENTAL NAVIGATION DISPLAY FOR VFR AND IFR OPERATIONS BUT IS LIMITED TO THE APPROVAL OF THE LORAN C OR GPS NAVIGATION SYSTEM. THE ARGUS 5000/CE MOVING MAP DISPLAY HAS BEEN SHOWN TO MEET THE CRITERIA OF FAA rso-c113, AIRBORNE MULTIPURPOSE ELECTRONIC DISPLAYS, AND HAS BEEN PREVIOUSLY INSTALLED UNDER EVENTIDE INC. FAA APPRO VED STC SA0054NY, IN AN AIRCRAFT AND MEETS THE FAA REQUIREMENTS FOR OPERATION IN THE AIRCRAFT DURING INSTRUMENT FLIGHT AND CAN BE USED AS A REQUIRED INSTRUMENT. THE NEW EQUIPMENT AND. ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER EVENTIDE AVIONICS INSTALLATION MANUAL NO. 5003, REVISION 03.07, DATED JULY 10, 1995 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTAL LED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION PARAGRAPH 3, 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPT ER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-I6236-0 41, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. 1S] Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277667 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) AIRCRAFT: BOEING, TYPE: 727-31, SIN 20115, DATE: 06/1442001, W.O. 16236, PAGE 2 OF 2 AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER 11, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED IAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS OUTLINED IN EVENTIDE AVIONICS DRAWING NO. 14O003, REV. B, DATED JUNE JUNE 4, 1999, AND STATES THAT THE ARGUS 5000/CE MOVING MAP DISPLAY SYSTEM IS "ON CONDITION". THE REQUIRED F.A.A. ARPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236-I01, REV IR, PAGES 1 THRU 6 DATED JiJ lie 2 00 I HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END ❑ Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277668 . AI as EFTA00277669 • Jet Aviation Associates Ltd. AFM Supplement to Bldg. 1515 Perimeter Rd. The Boeing Company 727-31 Palm Beach Int'l Airport Serial No. 20115 West Palm Beach, FL 33406 FAA Form 337 FAA CRS EYKR782D Document No. B727-16236-101 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-31 REGISTRATION NO.: N908JE SERIAL NO.: 20115 WITH A. SINGLE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY This supplement must be attached to the FAA approved Airplane Flight Manual when the airplane is modified by the installation of a single Eventide Avionics Argus 5000/CE Moving Map Display receiving navigation inputs from the No. 1 UNS-1D Flight Management System (FMS) in accordance with manufacture's Installation Manual No_ 50 3 Revision 03.07, dated July 10, 1995 or later approved revision and FAA Form 337, dated "7/ 7 O/ 1 The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult the appropriate basic Airplane Flight Manual. FAA Approved: Federal Aviation Administration Flight Standard District Office - 17 1050 Lee Wagener Blvd. Ft. Lauderdale, Florida 33315 FAA Approved Date: JUN 2 1 2001 Page 1 of 6 EFTA00277670 • 6 EFTA00277671 O-01 08:53 Jet Aviation P-02 ,Jun -20-01 08:03A N 3 Curran 352 243 1011 P _ 02 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DATI:. STATEMENT OF COMPLIANCE WITH THE FEDERAI. AVIATION REGULATIONS 06/20/2001 • •I AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. • TYPE (Alt-Mane. Radio. Helicopter. etc) NAME OF APPLICANT Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-270, Revision A, dated ARGUS 5000/CE MOVING MAP DISPLAY 06/19101 PURPOSE OF DATA • In support of major alteration to.Boe-ing 727-31, serial number 20115, registration number N905.1E. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.869 (a)(4) FAR 25.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1529 FAR 25.1309 (a)(b)(g) FAR 25.1581 (a)(b)(d) FAR 25.1351 (a) FAR 26.1357 (a)(c) CERTIFICATION -'Witt ratthont• .vault by ain-criaa of tart- AitagigolfiltOr slid it, WroidliaCe 1.101 tau:gime, aid tiviii.O•As of tippAix1AnnI grfttles, Fan ISJ if the Finlitral Ariati.• Kepis hods, Isla loud obwre AuK1006 al/talked OK'd, ..00t Iscrrsi 'WINE hare bora tisairrid no stionti.or ...III, ntsobik lord prolletturn and hoad no cn..pty will. applicable mtikeoph-xti ei Ow I edc.1.4.'114. Rtptatanwl a Recommend approval of these data I (We) Therefore L] Approve these ties (Systems & Equipment Aspects. Desi/a Approval Only. Does Plot ('osassita he Installatio n Approval) SI GNATILIKEIS) N El) ENG) NG REPRESENTATIVEISI DESIGNATION NOM BER(SI CLANSIFIE •rtnhts €40---- DERT-510087-NM Systems & Equipment — an C FAA Form 8110-3 n i-70) SUPERSETWC PREVIOUS EDITION CiPO 9O1-613 FLLENAIME: SC-127-NCINGMAP_ADOC EFTA00277672 ..I EFTA00277673 JET AVIATION ASSOCIATES, LTD k 4 71& . JEFNIf/R11-10111 1515 PERIMETER ROAD CRS-EYKR782O PALM BEACH INT'L AIRPORT WEST PALM BEACH, FLORIDA 334O6-1493 MODIFICATIO\ DAWING 561-233-7262 FAX 561 -233-7279 PROPRIETARY NOTES Th s drcrwlng contoins specifications and/or data. technical materiel, proprietary designs and information that ere the sate property of JET AVIATION ASSOCIATES. LTD. to be held and treated by its recipient on o confidential basis and is not to be shown or disclosed to any unauthorized organization or person without the written authorization of JET AVtATION ASSOCIATES. LTD. TITLE: LASERTRAK SYSTEM MODIFICATION PAGE: 1 OF 1 DWG NO.: REASON: RE-BUSS LASERTRAK INSTRUMENT LIGHTING FROM CENTER PANEL 34-61-32-1 TO CAPTAINS INSTRUMENT PANEL DUE TO RELOCATION OF INSTRUMENT A NOTES: 1. AIRCRAFT WIRING INSTALLATION IAW FM A.C. 43.13-1B, CHAPTER 11, SECTIONS 1, AND 3-20. 2. ALL WIRE PER MIL-W-22759 UNLESS SHIELDED. 3. ALL SHIELDED WIRE PER MIL- C-27500TG. 4. ALL WIRE 20 AWG UNLESS SPECIFIED OTHERWISE. 5. ALL CIRCUIT BREAKERS PER MS36574. 6. ALTERNATE TWISTED WIRE COLORS MAY BE SUBSTITUTED: PRIMARY SUB TRIPLE TWISTED: RED (R) WHITE (W) •. BLUE (B) BLUE (B) YELLOW (Y) ORANGE (0) TWISTED PAIR: RED (R) WHITE (W) BLUE (B) BLUE (B) 7. LOWER CASE LEITERS ARE SHOWN UNDERLINED. I.E. ci. 8. THIS MODIFICATION DRAWING ONLY CHANGES THE EXISTING LASERTRAK SYSTEM PER THE WIRING SHOWN, FOR ALL OTHER INFORMATION I REGARDING THE LASERTRAK SYSTEM REFER TO ORIGINAL PAGE AVJET DWG. 34-61-32. THIS MODIFICATION DRAWING SHALL BE ATTACHED TO THE ORIGINAL PAGE AVJET DRAWING FOR REFERNCE. ITAPT BRGAIST IND. I INSTR LTS{ H ci rr,„T, i 09504 i tI M I-- 20 20 • ill ----018-20---o — 019 -20 — — —5 PAGE DWG. 33-11-11 L .A.,__. __...y__. _ _.•\„,.._ LOC: CAPT. INSTR. PANEL rIASERTRAK CDI I D9315 I- H IT ) D9315 1 20 I INSTR LTS { Ii } 09315-9-20 I I ...- LOC: CAPT. INSTR. PANEL Q SYMBOL AND NUMBER REFERS TO PARTS LIST ITEM NUMBER. =DC GND -C> =AC GND GROUND NOTES: { A SYMBOL AND NUMBER REFERS TO INSTALLATION NOTES. -D> =SHLD GND --I> =CHASSIS GND O SYMBOL AND LETTER REFERS TO LIKE LETTER IN SYMBOL ON THIS DWG. NO. NEW WIRE REMOVED WIRE EXISTING WIRE WIRE TYPE NOTES: ( ) (* (_ - - -) ) /G. SCALE: NONE SER. NO.: 20115 PREPARED BY: G.L. KARR APPROVED BY: T. JARDINE 1 A/C MODEL: 727-100 REG. NO.: N908JE DATE: 05/24/01 DATE: 05/24/01 EFTA00277674 ♦. EFTA00277675 ty DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 3, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter,etc.) NAME OF APPLICANT Boeing 727-31 Airplane _ Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1270 Argus 5000/CE Moving Map Equipment Installation Sht 1-5, Rev IR B727-16236-1331 Aircell Equipment Installation, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA •• authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations,data listed above and on attached sheets numbered 0 have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data. I (X Therefore Approve these data. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) David E. Haralson Jr-;.,:ie. iici-ez.— DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDMON ER01207.doc EFTA00277676 id EFTA00277677 Q-• O Form Approved MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 US Departmen of Transportation t (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Federal Aviation Office Identification Administration INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). _ Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC 103 FOULK RD STE 202 WILMINGTON DE 19803-3742 3. For FAA Use Only crv3 data Identified heroin compile* or* the applicable ainevorthinee requirements is approved for the above described aircraft. Contor by a person -uthorized inFAR 43, s on 43.7. JUN t 1 20P1 , 50- SR) - 1 7 Date ginnfett of FAA inspector 4. Un Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer ,,. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. x Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer LIMITED AF &ENG, D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual -7/0 ) . John K. Urso. Inspector. /L.- t eA—35-- 7. Approval for Return to Se ce Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 0 APPROVED ❑ REJECTED Other (Specify) FAA Flt. Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Airworthiness Group Date of Appr9val r Rejection Certificate or Signature of Authorized Individual - . /. FAA Form 337 (12-88) Designation No. EYKR782D Ronald K. Bystrom. Manager Quality Assuranc .//' EFTA00277678 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with afl previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) AIRCRAFT: BOEING, TYPE: 727-31, S/N 20115, DATE: 06/14/2001, W.O. 16236, PAGE 1 OF 2 REMOVED THE EXISTING NO. 1 AND 2 HONEYWELL NZ-920 FMS SYSTEMS AND THE DL -900 DATA LOADER UNIT, AND INSTALLED DUAL UNIVERSAL AVIONICS CORP. UNS-ID FLIGHT MANAGEMENT SYSTEMS (FMS) WITH INTEGRAL GPS SENSORS, A UNIVERSAL AVIONICS CORP. RADIO TUNING UNIT (RTU), AND A UNIVERSAL AVION ICS CORP. DTU-100 DATA TRANSFER UNIT (DTU). THIS MODIFICATION WAS COMPLETED USING ita AVIATION DRAWI NG NO. B727-16236-410, NO. 1 FLIGHT MANAGEMENT SYSTEM, REV IR, DATED 04/10/01 AND B727-16236-411, NO.2 FLIGHT MANAG EMENT SYSTEM, REV. IR, DATED 04/15/01. THE RTU WAS INSTALLED USING JET AVIATION DRAWING NO. B727-16236-293, FLIGHT MANAGEMENT SYSTEM RADIO TUNING UNIT, REV IR, DATED 04/16/01. REFERENCE FAA FORM 8110-3 DATED 05/29/2001 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM. crli Mr" 25,4+ 11,313;i ts:;::, sC r..:•, ,d,3 orb FOi tno ---, ,,Avfnft= 2t Inc dirlartrup11 THE STRUCTURAL INSTALLATION OF EACH FMS, THE DTU;`' irrtintlIT WEItte9y1P4t7TgRy, .IL7T AVIATION DRAWING NO. B727-16236-1410, DUAL FMS W/RTU EQUIPMENT INSTALLATIONS, REV. IR, DATED 05/1'7/91, cg FAA FORM 8110-3, DATED JUNE I, 2001 BY STRUCTURES DER NO. DERT-810028,- ANTENNAS WER AILED USING JET AVIATION DRAWING NO. B727-16236-144I, GPS ANTENNA INSTALLATI REV. A, DATED 05/29/01, REFERENCE FAA FORM 8110- 3, DATED 6/18/01 BY STRUCTURES DER NO. DERT-510024-CE. THE UNS-1D SYSTEMS RECEIVE BARO-CORRECT1ED ALTITUDE AND TAS INFORMATION FROM THE NO. 1 AND NO.2 AIR DATA COMPUTERS RESPECTIVELY, VOR/DME BEARING AND DISTANCE INFORMATION FROM THE NO. I AND NO.2 COLLINS VIR-432 AND DME-442 SYSTEMS, AND CROSS SIDE GPS INFORMATION AS WELL AS EACH UNITS INDEPE NDENT GPS SENSOR DATA, FUEL FLOW DATA FROM THE AIRCRAFT FUEL FLOW SYSTEM AND IRS INFORMATION FROM THE EXISTING NO. 1, 2, AND 3 HONEYWELL "LASERREF" SYSTEMS. THE UNS-ID FMS HAS BEEN PREVIOUSLY INSTALLED UNDER UNIVERSAL AVIONICS SYSTEMS CORP. FAA APPROVED STC SA5072NM, IN AN AIRCRAFT AND CERTIFIED FOR VFR AND IFR NAVIGA TION WHICH QUALIFIES THIS INSTALLATION AS A "FOLLOW ON" INSTALLATION PER AC 20-130A. THE UNS-1D FMS SYSTEMS HAVE BEEN SHOWN TO MEET ALL OF THE REQUIREMENTS OF AC-20-130A FOR VFR-IFR NAVIGATION ENROUTE, TERMINAL, OVER WATER AND IN REMOTE AREAS, AND FOR NON-PRECISION APPRO ACHES. THE NO.1 AND 2 FMS SYSTEMS ARE DIGITALLY INTEGRATED TO THE EXISTING HONEYWELL FIVE-TUBE ELECTR ONIC FLIGHT INSTRUMENT SYSTEM (EFIS). THE PILOT AND COPILOT'S EFIS SYMBOL GENERATOR'S HAVE HONEYWELL SERVICE BULLETIN A21-2000-028 AND THE MULTI-FUNCTION GENERATOR HAS HONEYWELL SERVICE BULLETIN A21-2000-029 TO INCORPORATE NON-PRECISION GPS SCALING VIA GAMA ARINC 429 LRN INTERFACE WHICH MEETS REQUIREMENTS OF TSO C129A AND AC 20-130A. THE FMS SYSTEMS ARE CROSS-COUPLED TO EITHER THE PILOT OR COPILOT EFIS FOR DISPLAY AND NAVIGA TION. THE EFIS CONVERTS THE DIGITAL TO ANALOG OUTPUTS AND PROVIDES ALL LATERAL STEERING TO THE AUTOPILOT AND FLIGHT DIRECTOR SYSTEM. VERTICAL NAVIGATION (VNAV) FROM EITHER FMS SYSTEM IS NOT DISPLAYED OR COUPLED IN THIS INSTALLATION. THE FOLLOWING REQUIRED ANNUNCIATORS FOR THE FMS SYSTEMS ARE DISPLAYED ON THE EFIS DISPLAYS: FMS MSG INDICATES A MESSAGE IS TO BE ACKNOWLEDGED ON THE MSG PAGE. (COLOR: AMBER) LOCATED ON EADI. XTK SELECTED CROSSTRACK IS ACTIVE. (COLOR: CYAN) LOCATED ON EHSI. WPT INDICATES WAYPOINT ALERT TWO MINUTES PRIOR TO WAYPOINT IN EN ROUTE MODE, AND 15 SECONDS PRIOR IN APPROACH MODE. WHEN THIS ANNUNCIATOR FLASHES, IT INDICATES THAT AN UPCOMING VERTICAL FLIGHT PATH ANGLE (FPA) CHANGE IS WITHIN TWO MINUTES. (COLOR: AMBER) LOCATED ON EHSI. APP AN APPROACH HAS BEEN ACTIVATED. (COLOR: CYAN) LOCATED ON EHSI. El Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277679 NOTICE Weight andtalance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration must be compatible with allprevious alterations to assure continued conformity with the applicable airworthiness requirements. Nk. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) AIRCRAFT: BOEING, TYPE: 727-31, S/N 20115, DATE: 06/14/2001, W.O. 16236, PAGE 2 OF 2. THE FOLLOWING REQUIRED ANNUNCIATORS WERE LOCATED ON THE EXISTING PILOT AND COPILOT'S INSTRUMENT PANEL ADJACENT TO THE EADI UNITS: FMS HDG THE FMS IS IN HEADING SUB-MODE. (COLOR: BLUE) GPS INTEG GPS INTEGRITY IS OUTSIDE OF THE ALLOWABLE LIMIT FOR A PHASE OF FLIGHT (2.0-NM EN ROUTE, 1.0-NM TERMINAL AND APPROACH TRANSITION, AND 0.3-NM FINAL APPROACH SEGMENT). SEE SECTION III, ABNORMAL PROCEDURES. (COLOR: AMBER). THE ADDED ANNUNCIATORS ARE DIMMED AND TESTED USING THE EXISTING PILOT AND COPILOT ANNUNCIATOR COUPLERS. THESE UNITS HAVE BEEN MODIFIED USING JET AVIATION MODIFICATION NO. 33-39-02-1, CAPT. AND F/O ANNUNCIATOR COUPLER MODIFICATION, DATED 04/12/01, REFERENCE FAA FORM 8110-3, DA IED 05/29/2001 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER UNIVERSAL AVIONICS CORP. RETURN TO SERVICE MAINTENANCE AND CHECKOUT PROCEDURES MANUAL NO. 34-60-21, DATED 19 MARCH 2001 WITH NO DISCREPANCIES NOTED. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 1 OF 5, DATED 06/19/2001, WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH•12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK, INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER 11, SECTION 4. ELECIRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTAT J.FD IAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLY WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.I3-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS AS REQUIRED BY FAR 25.1529 IS DETAILED IN THE UNIVERSAL AVIONICS CORP. UNS-1D FLIGHT MANAGEMENT SYSTEM TECHNICAL MANUAL NO. 34-60-09, DATED AUG 15/97. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATE6112001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333- CE. THE REQUIRED F.A.A. APPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236-100, REV IR, SHEETS 1 THRU 9, DATED ne 2-1 i 20 0 I HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END ❑ Additional Sheets Are Attached EFTA00277680 "fr .4 EFTA00277681 Oak Jet Aviation Associates Ltd. AFM Supplement to BIdg. 1515 Perimeter Rd. The Boeing Company 727-31 Palm Beach Int'l Airport Serial No. 20115 West Palm Beach, FL 33406 FAA Form 337 FAA CRS EYKR782D Document No. B727-16236-100 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-31 REGISTRATION NO.: N908JE SERIAL NO.: 20115 WITH DUAL UNIVERSAL AVIONICS FLIGHT MANAGEMENT SYS TEMS (UNS1-D) INSTALLED This supplement must be attached to the FAA approved Airplane Flight Manual when the airplane is modified by the installation of dual Universal Avionics Sys tems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Manageme nt via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Iner tial Reference Sensors (IRS), dual internal GPS sensors, and VOR/DME from the Collins No. 1 and No. 2 VORJDME systems in accordance with manufacture's Installation and Checkout Manual No. ?4-60-09, Rev. 2. dated August 15, 1997 or later approved revision and FAA Form 337 , dated- 7/2/0/ 0 The information contained herein supplements or supers edes the basic manual only in those areas listed herein. For limitations, procedures, and perform ance information not contained in this supplement, consult the appropriate basic Airplane Flight Man ual. FAA Approved: Federal Aviation Administration Flight Standard District Office - 17 1050 Lee Wagener Blvd. Ft. Lauderdale, Florida 33315 FAA Approved Date: JUN 2 1 2001 Page 1 of 9 EFTA00277682 Os 1 EFTA00277683 May-29-01 01:59P N 3 Curt-an 352 243 1011 P _ 06 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 05129/2001 -, AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane. Radio. Helicopter. etc) NAME OF APPLICANT Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-293, Initial Release, FLIGHT MANAGEMENT SYSTEM RADIO TUNING UNIT dated 04/16/01 B727-16236-410, Initial Release, NO. 1 FLIGHT MANAGEMENT SYSTEM dated 04/10101 B727-16236-411, Initial Release, NO. 2 FLIGHT MANAGEMENT SYSTEM dated 04/15/01 33-39-02-1, Initial Release, dated CAPT AND F/O ANNUNCIATOR COUPLER MODIFICATION 04112/01 L PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N90BJE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1329 (h) FAR 25.1529 FAR 25.869 (a)(4) FAR 25.1351 (a) FAR 25.1581 (a)(b)(d) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c)(d)(e) FAR 25.1309 (a)(b)(c)(d)(e)(g) FAR 25.1381 (a)(b) FAR 25.1322 (b)(c) FAR 25.1431 (a)1131(c) CERTIFICATION - Under authority vested by direction of theAdmiwistrator and in accordance laid. conditions and Ensiles-tows of appoinemeat ander Part I23 of the Federal Awl-mien IRegulatiosts, data listed above and on attached sheets 'mothered NONE have been remained in accordance with establistard procedures sod fooad to comply with applicable requirements of the Federal Aviation Regulations. 0 Retommeoil approval of these data I (We) Therefore El Approve these data (Systems & Equipment Aspetts, Design Approval Only. Does Not Constitute Installation Approral ) SIGNATURES F D LUG TE GLNEE RETRESENTATIVE(S) DESIGNATION NUMBERIS) CLASSIFICATTON(S) ,Q DERT-510087-NM Systems & Equipment No an J. an _ 01111 110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME: SC-727-FM S.DOC EFTA00277684 a • EFTA00277685 DATE DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 1, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION • MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION • TITLE B727-16236-1261 AT-855/RTA-880 Antenna Installations, Sht.1-7, Rev A • B727-16236-1410 Dual FMS WI RTU Equipment Installations, Sht 1-6, Rev IR Note: - 1. This approval is for structural aspects only. • 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. • PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 . . . CERTIFICATION - Under authority vested by direction of the Administrator .and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered 0 have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data. I ('Therefore Approve these data. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) David E. Haralson .a.are. 14,-.1.-- DERT-810028-NE Structural FAA FOITTI 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01202.cloc EFTA00277686 a i EFTA00277687 U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTATION June 18, 2001 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT Boeing B727-31 Airplane Jet Aviation LIST OF DATA IDENTIFICATION TITLE Jet Aviation GPS Antenna Installation Engineering Drawing Beoing B727-31, N908JE, S/N 20115 No. B727-16236-1441, END END END END END END END END Dtd. 5/29/2001, Rev. A Note: The certification basis of this aircraft includes FAR 25.571 Damage - tolerance and fatigue evaluation of structure. Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness of Structural Repairs on Transport Category Airplanes, the damage tolerance and fatigue evaluation of END END the structure must be performed before 6/18/2002. Notes: 1) The structural aspects only of the above listed data are approved herein. 2) This approval is valid for the aircraft model and serial number listed below 3) This approval is based on structural analysis on file at DER Services corporate office in Ft. Lauderdale, FL. Model No. B727-31 Serial No. 20115 PURPOSE Approve data for antenna installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS (LISTSPECIFIC SECTIONS) 25301, 25303, 25.305, 25.307, 25.601, 25.603, 25.605, 25.609, 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I (We) Therefore P1 Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Robert J. Belgau DERT-510024-CE Structures FAA FORM 8110-3 (11-70) SUPERSEDES PREVIOUS EDITIO N DER SERVICES PROJECT NO. 2001-082 EFTA00277688 16 v i EFTA00277689 Form Approved a MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 US Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Ont Federal Aviation Office Identification Administration 5-0- FS`DO - i 7 9 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructi s and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exc ed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC. 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1above) X POWERPLANT PROPELLER Type •- APPLIANCE Manufacturer ,,, 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. X Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer LIMITED AIF & ENG, D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual 7/2/01 • John K. Urso. Inspector. 16, U -V 7. Approval for Return to Service k Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is C4 APPROVED ❑ REJECTED Other (Specify) FAA Flt. Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 7/2/01 EYKR782D Ronald K. Bystrom. Manager Quality Assuranc FAA Form 337 (12-88) EFTA00277690 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirem ents. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, SIN 20115, N908JE, W/O 16236. INSTALLED 2 EA NEW GARMIN GPS ANTENNAS P/N 011-00134-00 (TSO C129A). 1 EA AT FUSELA GE STATION 284.8, BL 0.0, AND 1 EA FUSELAGE STATION 934.3 RBL 4.56, PER JET AVIATION DRAWING B727-16236-1413, REV IR, DATED 6/5/01 TITLED - DUAL AUXILIARY GPS ANTENNAS INSTALLATION. REF F.A.A. FORM 8110-3 DATED 6/6/01 BY STRUC TURES D.E.R. NO. DERT-510394- CE. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-IB, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNE CTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRA FT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER 11, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SF.I.FCT ED AND INSTALLED LAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAG RAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-IB, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRA FT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS LAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS CONTAINED IN ENGINEERING REPORT JMER-836, REV IR, DATED 6/10/01. REFERENCE FAA FORM 8110-3 DATED 6/11/01 BY STRUCTURES DER NO. DERT-510394-CE. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATIO N. END ❑ Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277691 44t.c.c000v..)4 ••• yr 0 AgiA U ri't S to 002 • U.S. DEPARTMENT OF TRANSPORTATION PEDERAL AVIATION ADMINISTRATION DATE STATEMENT OP COMPLIANCE W ITH THE FEDERAL AVIATIO N REGULATIONS Tune 6, 2001 • AIRCRAFT OR AIRCRAFT COMP MAKE ONENT WENTIFICATION MODEL NO. TYPE (Airplane. Reif*, Helicopter, etc .) NAME OP APPLICANT BOEING 8727-3I , Airplaii ...----A-kl../ViaaalLasicKjar LIST OP DATA es I ul, ...., IDENTIFICATION TITLE B727-16236-1413 IR DRAWING — Sheets 1— 3 (6/5/01) DUAL AUXILIARY GPS ANTENNAS INSTALLATION NOTE: Approval for the structural aspects relate d to the above design data will be covered by a separate Form 8110-3 which will be issued for the Proof of Structure and will include required inspection items) to ensure Continued Airworthiness associated with this modification. . . END END END PURPOSE OF DATA To provide a record of design app roval of the above data applicable to B727-31, for manufacturing and confortnity. See NO SIN 20115, Registration No. N90&1E. TE above. APPLICABLE REQUIREMENTS (Li spe st cifi c sections) FAR 25.6601 FAR 25.609 FAR 25.603 FAR 25.611 FAR 25.605 FAR 25.613 CERTIFICATION - Under authority vet ted by direction of the Administrator arxi in 2,c,cordanee appointment under part 183 of az Pcderal Avi atio wick cordidons sad limitations of examined in sem-dame with #=0111 n Reg ula tior n. ellta list ed abo ve and on attached slims numbered 01(4 procodures and found m comply with app IVA have been licable requirements of !be Federal Aviation Regulat I* Therefore ions. 0 Recommend approval of these dota X Approve Mete data (Sec NOTE above) siGNATurtr.(s) OF DESIGNATED REPRESEN TATIVE(S) DESIGNATION NUNIBMS ) CLASSIFICATION(S) DERT - 510394 - CE STRUCTURES Kenneth W. Thompson - FAA 8110.3 (11-70) SUPERSEDES PREVIOUS EDITION sheet 1 of 1 EFTA00277692 a %I EFTA00277693 .. U.S. DEPARTMENT OF TRANSPORTATION. • DATE - FEDERAL.AVIATION ADMINISTRATION . , STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 11, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT BDEilia /172L-31 EURELANE.---IgLAYialisnlAsurdatcda11_, LIST OF DATA IDENTIFICATION TITLE • JMER-836 IR ENGINEERING REPORT — Dated 06/10/01 STRUCTURAL SUBSTANTIATION - DUAL AUXILIARY GPS ANTENNA INSTALLATION ON A BOEING B727-31 AIRCRAFT, S/N 20115 NOTE: The operator of B727-31 aircraft S/N 20115 modified by drawing B727-16236-1413 dated 6/5/01 issued at no revision, is required to incorporate in the Airworthiness Limitations Section of the Instructions for Continued Airworthiness applicable to the existing Maintenance Program, an inspection item at a frequency not to exceed 3700 flights to detect signs of distress (0.25 inch or smaller crack and/or working rivets) common to the GPS antenna installation as detailed in drawing B727-16236-1413. Refer to FAR PART 25 Appendix H and Report JMER-836 IR page 4.1 (CONCLUSIONS) for instructions. PURPOSE OF DATA To provide a record of design approval of the above data as applicable to B727-31 S/N 20115 and to show compliance to the following FAR's: . . APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 FAR 25.307 FAR 25.605 FAR 25.613 FAR 25.303 FAR 25.571 FAR 25.609 FAR 25.625 FAR 25.305 FAR 25.603 FAR 25.611 Chlt111-ICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered N/A have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. I (k) Therefore . Recommend approval of these data X Approve these data (Structural aspects only) . - SIGNATURE(S) OF DESIGNATED REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 60- 7- DERT - 510394 - CE . STRUCTURES Kenneth W. Thompson .. • FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION sheet 1 of 1 EFTA00277694 .1. 11 EFTA00277695 Form Approved O f ' MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 OS Deoartrraant For FAA Use Only 0 Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Office identification Administration INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC. 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in item 1above) X POWERPLANT PROPELLER Type • • APPLIANCE Manufacturtr \ ,.. _ 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. x Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer LIMTIED A/F & ENG, D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individu 7/2/01 John K. Urso. Inspector. ,6- (1,,,_.,- 7. Approval for Return to Servi Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 0 APPROVED • REJECTED Other (Specify) FAA Fit. Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized individual Designation No. 7/2/01 EY1CR782D Ronald K. Bystrom. Manager Quality Assurance FAA Form 337 (12-88) EFTA00277696 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with 'all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, S/N 20115, N908.1E, W/O 16236. INSTALLED A NEW KGS ELECTRONIC MODEL UC-28-14, 28 VDC TO 14 VDC CONVERTER AND THREE POWER OUTLETS IN THE COCKPIT IN ACCORDANCE WITH KGS ELECTRONIC MODEL UC-28-14 INSTALLATION MANUAL AND ADVISORY CIRCULAR 25-10 (INSTALLATION OF MISCELLANEOUS NON REQUIRED ELECTRICAL EQUIPMENT) USING THE FOLLOWING JET AVIATION DRAWINGS SUBSTANTIATED BY F.A.A. FORM 8110-3 RESPECTIVELY WIRING DRAWING: • B727-16236-352, REV IR, DATED 5/25/01, SHEETS 1 & 2, TITLED - 28-14 VDC CONVERTER WIRING DIAGRAM. REFERENCE F.A.A. FORM 8110-3 DATED 6/7/01 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-CE. STRUCTURAL DRAWING: • B727-16236-1352, REV IR, DATED 6/6/01, SHEETS 1 THRU 5, TITLED - 28-14 VDC CONVERTER EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3 DATED 6/10/01 BY STRUCTURES DER NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER KGS ELECTRONIC MODEL UC-28-14 INSTALLATION MANUAL WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/20011 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER 11, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED IAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.I3-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-IB, CHAPTER 10, SECTION 2 AND AC 43.I3-2A, CHAPTER 1 PARAGRAPH 9. THERE IS NO CHANGE TO THE MANUFACTURERS MAINTENANCE FOR CONTINUED AIRWORTHINESS DUE TO THIS MODIFICATION. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END ❑ Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277697 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 06/07/2001 ... AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc) NAME OF APPLICANT Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE " B727-16236-352, Initial Release, 28-14 VDC CONVERTER WIRING DIAGRAM dated 05/25/01 B727-16236-580, Initial Release, CABIN NO. 2 60 Hz SYSTEM dated 05/25/01 B727-16236-600, Initial Release, SPARE WIRING (PROVISIONS) dated 05/25/01 • ---- PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.869 (a)(4) FAR 25.1353 (a)(b) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c) FAR 25.1309 (a)(b)(g) FAR 25.1431 (a)(b)(c) FAR 25. 1322 (b) FAR 25.1529 FAR 25.1351 (a) CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part la3 of the Federal Aviation Regulations. data listed above and on attached sheets numbered NONE have been examined in accordance with established procedures and found to comply with applicable requiremen Regulations. ts of the Federal Aviation ❑ Recommend approval of these data I (We) Therefore E3 Approve these data (Systems & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approva l) )• SIGNATURE( ESIGN NGIN REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) - - DERT-510087-NM Systems & Equipment No an J. ran FAA Foim 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 90I-6I3 FILENAME SC-727-CAB-PWR.DOC EFTA00277698 4 J EFTA00277699 DATE DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION June 10, 2001 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter,etc.) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1352 28-14 VDC Converter Equipment Installation, Sht 1-5, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations,data listed above and on attached sheets numbered 0 have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data. I ( )34 Therefore Approve these data. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICAT1ON(D David E. Haralson P.,..,,e. 1-4,-.1.-- DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01209.doc EFTA00277700 aa a EFTA00277701 Form Approved 42 MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 US Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Federal Aviation Office Identification Administration INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision ()— r5D6-i7 7/- thereof) for instructs s and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to ex d $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC. 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only • 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer \ ,. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. x Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer LIMITED A/F & ENG. D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachm ents hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual 7/2/01 John K. Urso. Inspector. 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 4 was ns in the manner prescribed by the Administrator of the Federal Aviation Administration and is APPROVED lID REJECTED FAA Flt. Standards Other (Specify) Inspector Manufa cturer inspection Authorization BY Person Approved by Transport FAA Designee X Repair Station Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 7/2/01 EYKR782D Ronald K. Bystrom. Manager Quality Assurance. ae " , . FAA Form 337 (12-88) EFTA00277702 NOTICE Weight and balance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration must be compatible with .alf previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, SIN 20115, N908JE, W/O 16236. INSTALLED A UNITRON 60 HZ CONVERTER P/N PS-62-66D AND 26 EA CABIN OUTLETS PER UNITRON 60 HZ CONVERTER INSTALL MANUAL NO. PS-62-66D-6. THIS MODIFICATION WAS ACCOMPLISHED PER THE FOLLOWING JET AVIATION DRAWINGS WHICH ARE SUBSTANTIATED BY F.A.A. FORM 8110-3 RESPECTIVELY WIRING DRAWING: • B727-13236-580, REV IR, DATED 5/25/01, SHEETS 1 THRU 5, TITLED - CABIN NO. 2 60 HZ SYSTEM REFERENCE FAA FORM 8110-3 DATED 6/7/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS: • B727-16236-1580, REV IR, DATED 6/11/01, SHEETS 1 THRU 7, TITLED - CABIN NO. 2 60 HZ EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3, DATED 6/13/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-:1B, CHAPTER 11, SECTION 4. ELECIRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16, ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.I3-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. THERE IS NO CHANGE TO THE MANUFACTURERS MAINTENANCE FOR CONTINUED AIRWORTHINESS DUE TO THIS MODIFICATION. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END ❑ Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277703 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION • REGULATIONS 06/07/2001 -.. AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc) NAME OF APPLICANT Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-352, Initial Release, 28-14 VDC CONVERTER WIRING DIAGRAM dated 05/25/01 B727-16236-580, Initial Release, CABIN NO. 2 60 Hz SYSTEM dated 05/25/01 . B727-16236-600, Initial Release, SPARE WIRING (PROVISIONS) dated 05/25/01 , . PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial num ber 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections ) FAR 25.869 (a)(4) FAR 25.1353 (a)(b) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c) FAR 25.1309 (a)(b)(g) FAR 25.1431 (a)(b)(c) FAR 25. 1322 (b) FAR 25.1529 FAR 25.1351 (a) CERTIFICATION — Under authority voted by direction of the Administra tor and in accordance with conditions and limitations data listed above and on attached sheets of appointment under Part IS3 of the Federal Aviati numbered NONE have been examined in accordance with established proce on Regulations. Regulations. dures and found to comply with applicable requir ements or the Federal Aviation El Recommend approval of these data I (We) Therefore 0 Approve these data (Systems & Equipment Aspe cts, Design Approval Only, Does Not Constitute Installatio n Approval) siGNA7-0 £SIG G REPRESENTATIVES) DESIGNATION NUMBER(S) CLSSIFICATIONS) 11-ele,--- DERT-510087-NM Systems & Equipment No an J. ran AA Form 8110-3 (11-70) sUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME SC-727-CAB-PWR.DOC EFTA00277704 a • EFTA00277705 • DATE DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 13, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter,etc.) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1580 Cabin #2 60 Hz Equipment Installation, Sht 1-7, Rev IR Note: • 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations,data listed above and on attached sheets numbered 0 have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data. I (X Therefore Approve these data. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) David E. Haralson 1,;-4Oae. ilicied......--- DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01210.doc EFTA00277706 4k • `V EFTA00277707 No Form Approved MAJOR REPAIR AND ALTERATION OMB No. 2120.0020 US Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) For FAA Use O ly Federal Aviation Office Identification Administration c0-- r5DO - 17 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instr ions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to xceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC. 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in item 1above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer ‘,. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. X Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer LIMITED A/F & ENG, D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachm ents hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual 7/2/01 . John K. Urso. Inspector. r\ 4- 16-'6(----! — 7. Approval for Return to Servige Pursuant to the authority given persons specified below, the unit identified in item 4 wa inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is APPROVED III REJECTED FAA Fit. Standards Other (Specify) Inspector Manufa cturer Inspection Authorization BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 1 7/2/01 EYKR782D Ronald K. Bystrom . Manager Quality Assuranc ..... FAA Form 337 (12-88) EFTA00277708 NOTICE Weight and balance or operating limitation changes shall be entered in the appropr iate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirem ents. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, S/N 20115, N9083E, W/O 16236. INSTALLED AN AIRCELL ATG.01 FLIGHT PHONE SYSTEM CONSISTING OF AN ANTENNA P/N CI-5000 , A TRANSCEIVER P/N 900002-2, and AN ANTENNA MATCHING UNIT P/N 83518, 4 EA HANDSETS P/N 400-10035-001 AND 4 EA HANDSET CRADLES P/N 400-10038-001. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWI NGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING: • B727-13236-330, REV. IR, DATED 4/30/01, SHEETS 1 THRU 3, TITLED - AIRCELL ATG.01 AIR / GROUN TELEPH D ONE REFERENCE FAA FORM 8110-3 DATED 5/29/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-N M. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-1330, REV. A, DATED 5/29/01, SHEETS 1 THRU 4, TITLED - AIRCELL ATG.01 AIR / GROUND TELEPHONE ANTENNA INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 6/18/01, BY STRUCTURAL D.E.R. NO. DERT-510024-CE. • B727-16236-1331, REV. IR, DATED 5/24/01, SHEETS 1 THRU 6, TITLED -AIRCELL EQUIPMENT INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 6/3/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER AIRCELL ATG.01 FLIGHT PHONE SYSTEM INSTALLATION MANUAL REV IR, DATED 6/11/99 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICA TORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-IB, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTIO N 3, PARAGRAPH 11-37. _ AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFO RM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.I3-1B, CHAPTER 11, SECTION 4. FT FCTRICAIJELECIRONIC WIRING WAS SELECT ED AND INSTALLED IAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-IB, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPL IES WITH AC43.13-IB SECTION 16. ELECIRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPT ER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. PER THE AIRCELL ATG.01 FLIGHT PHONE SYSTEM MANUAL ALL COMPONENTS ARE CONSIDERED LINE REPLACEABLE UNITS AND DO NOT API-ECT THE MANUFACTURERS INSTRUCTIONS FOR CONTINUING AIRWORTHINESS. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATE6112001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333-CE. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES REQUIRED FOR THIS INSTALLATION. END ❑ Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277709 --M4y-29 - 01 01:59P N J Curran 352 243 1011 P C.) / DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 05129/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane. Radio, Helicopter. etc) NAME OF APPLICANT Boeing Jet Aviation Associates 727-31 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-330, Initial Release, AIRCELL AGT.01 AIR/GROUND TELEPHONE dated 04/30/01 •- - - • PURPOSE OF DATA In support of major alteration to Boeing 727-31. serial num ber 201 15, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1357 (a)(c) FAR 25.869 (a)(4) FAR 25.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1529 FAR 25.1309 (a)(b)(g) FAR 25.1351 (a) CERTIFICATION - Under sithoriry . eyed by direction or tht Administrator and is setordsset will clisdielons and /imitations et" 'pp:amine/se taedtr data kited ibtwc sad** tinseled sheen niseslweed NONE have bets emainintd in aceordsnce with reublishtel peiscrchirts and Tan 113 *fibs Federal Atistis• ;Ululation:4 &Dilations. Amid to esertrily with applicabh rtquirttnents et the Fedmri Aviati on O Recommend approval of these data I (We) Therefore 1 Approve these data (Systems & Equipment Aspects. Desig n Approval Only, DIM Not Constitute Installation Appr oval) SIGNATURE ESIGNA GINEERI PRESENTATIVE(S) DESIGNATION N UM ILERM CLASSIFICATIONS) !at--. DERT-510087-NM Systems & Equipment No n J. C n EFTA00277710 o EFTA00277711 U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTATION June 18, 2001 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL TYPE Oftplane, RaSe, Iftlicopra: ac.) NAME OF APPLICANT Boeing B727-31 Airplane Jet Aviation LIST OF DATA 1DEN fIFICALLUN It ILL Jet Aviation Aircell AGT.01 Air/Ground Telephone Antenna Installation Engineering Drawing Beoing B727-31, N908JE, S/N 20115 No. B727-16236-1330, END END END END END END END END Dtd. 5/29/2001, Rev. A Note: The certification basis of this aircraft includes FAR 25.571 Damage - tolerance and fatigue evaluation of structure. Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness of Structural Repairs on Transport Category Airplanes, the damage tolerance and fatigue evaluation of END END the structure must be performed before 6/18/2002. tlotes: 1) The structural aspects only of the above listed data are approved herein. 2) This approval is valid for the aircraft model and serial number listed below 3) This approval is based on structural analysis on file at DER Services corporate office in Ft. Lauderdale, FL. Model No. B727-31 Serial No. 20115 PURPOSE Approve data for antenna installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS (LISTSPECIFIC SECTIONS) 25.301, 25.303, 25.305, 25.307, 25.601, 25.603, 25.605, 25.609, 25.613 CF.RTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition and Ii • tions of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets number have been examined in accordance with established procedures and found to comply with applicable requirements of the ederal Aviation Regulations. Recommend approval of these data 1 (y) Therefore Fil Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBERS) CLASSIFICATION(S) Robert J. Belgau DEBT-510024-CE Structures 19 e.---- -. 0/276415 FAA FORM 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. 2001-082 EFTA00277712 I EFTA00277713 DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 3, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radfo, Helicopter,etc.) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE 8727-16236-1270 Argus 5000/CE Moving Map Equipment Installation Sht 1-5, Rev IR B727-16236-1331 Aircell Equipment Installation, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA . authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations,data listed above and on attached sheets numbered 0 have been examined in accordance with established procedures and found to comply with applicable requirem ents of the Federal Aviation Regulations. Recommend approval of these data I (X Therefore Approve these data. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVES) DESIGNATION NUMBER(S) CLASSIFICATION(S) David E. Haralson Pe-,:fe. /4,-d._ DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01207.doc EFTA00277714 a NO EFTA00277715 DEPARTMCNT OF TRANSPORTATION • DATE FEDERAL AVIATION ADMINISTRATION . STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS JUNE 12, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 'HAKE MODEL NO. TYPE (Airlakoc. Radio, Helicopter, NAME OF APPLICANT ad) BOEING 727-31 AIRPLANE JET AVIATION • LIST OF DATA IDENTIFICATION TITLE. A.T.E. INC. BOEING 727-31 S/N 20115, AERO-M SATCOM ANTENNA INSTL., UPPER B.S. STRUCTURAL REPORT 360-390; GPS ANTENNA INSTL., UPPER B.S. 312-328; AIRCELL AGT.01 ANTENNA INSTL. , No. ATE6I 12001 LOWER B.S. 400-420 DAMAGE TOLERANCE ANALYSIS; SR 1-31, REV. (IR) • NOTE; REQUIREDINSPECT1ONS AT'T'ACHED THESE DATA APPLY ONLY TO BOELNG 727-31 S/N 20115 . PURPOSE OF DATA 1 TO APPROVE DATA FOR DAMAGE TOLERANCE ANALYSIS, B-727-3 I S/N 20115 APPLICABLE REQUIREMENTS (List spainc cations) . - FAR 25.571 (STRUCTURAL ASPECTS ONLY) • . CERTIFICATION — Under authority vested by direction of the Administrator and in accordance with conditions and limitations • . of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered I of l have been examined in accordance with established procedures and found to comply with applicable requirements i of the Federal Aviation Regulations. I (Ye) Therefore Recommend approval of these data Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING DESIGNATION NUMBER(S) CLASSIFICATIONS) DERT-510333-CE STRUCTURAL • • • • . FAA Form 8110-3 (I t.70) SUPERSEDES PREVIOUS EDMON cro 901.613 EFTA00277716 • •• it EFTA00277717 O Form Approved MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 us Department For FAA Use Onl of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Office Identification Administration 5 0— F 5 Do — 17 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructs s and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to ex red $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 . 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC. 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1above) X POWERPLANT PROPELLER . Type APPLIANCE Manufacturer ‘,. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. x Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer LIMITED A/F & ENG. D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized individual 7/2/01 John K. Urso. Inspector. laJ-- -- 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 4 was _p_ected in the manner prescribed by the Administrator of the Federal Aviation Administration and is APPROVED U REJECTED Other (Specify) FAA Fit. Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 7/2/01 EYKR782D Ronald K. Bystrom. Manager Quality Assurance FAA Form 337 (12-88) EFTA00277718 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registra tion mark and date work accomplished.) BOEING 727-31, S/N 20115, N908JE, W/O 16236. ACCOMPLISHED AN UP-GRADE TO THE EXISTING HONEYWELL WEATHER RADAR SYSTEM FROM PRIMUS 870 TO PRIMUS 880. REMOVED THEl 1 & 2 WC-870 CONTROLLERS P/N 7008471-803 AND INSTALLED WC-880 CONTROLLERS P/N 7008471-405 (TSO C63c), REMOVED THE WU-870 ANTENNA & RECEIVER / TRANSMITTER UNIT P/N 7012640 -902 AND INSTALLED NEW WU- 880 ANTENNA & RECEIVER / TRANSMITTER UNIT P/N 7021450-801 (TSO C63c). INSTALLED A HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM CONSISTING OF AN LP-860 PROCESSOR P/N 7011822-904 (TSO C110) AND AN AT-855 ANTENNA PIN 7014062-901 (TSO C110). THE LIGHTNING SENSOR SYSTEM INTERFACES WITH THE PRIMUS 880 RADAR SYSTEM THRU THE # I & 2 WC-880 CONTROLLERS. RELOCATED EXISTING SECURITY SYSTEM ANTENNA P/N DMC57 -1 TO THE TOP OF THE RADAR ANTENNA & RECEIVER / TRANSMITTER UNIT. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING: • B727-16236-260, REV. IR, DATED 5/29/01, SHEETS 1& 2, TITLED - WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) REFERENCE FAA FORM 8110-3 DATED 6/7/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. • B727-16236-261, REV. IR, DATED 4/10/01, SHEETS ITHRU 3, TITLED - HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM REFERENCE FAA FORM 8110-3 DATEDS/29/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-1261, REV. A, DATED 5/30/01, SHEETS 1 THRU 7, TITLED - AT-855/RTA-880 ANTENNA INSTAL LATIONS REFERENCE F.A.A. FORM 8110-3, DATED 6/1/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. • B727-I6236-1262, REV. IR, DATED 5/21/01, SHEETS 1 & 2, TITLED - LSZ-860 LIGHTNING SENSOR EQUIPM ENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3, DATEDS/28/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER HONEYWELL PRIMU S 880 RADAR SYSTEM INSTALLATION MANUAL NO. 34-42-12, REV 3, DATED 2/15/00 AND THE HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM INSTALLATION MANUAL NO. 34-41-50, REV 5, DATED 2/15/01 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO. B727-16236-080, REV IR, DATED 6/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPM ENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELFCTRICAL LOAD ANALYSIS UPDATE REPORT B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH 43.13-1B, CHAPTER 11, SECTION 3, PARAG RAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-IB, CHAPTER 4, SECTIONS I, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRA FT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER II, SECTION 4. ELECTRICAIJELECIRONIC WIRING WAS SELECTED AND INSTALLED IAW AC43.13-IB, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAG RAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPM ENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-IB, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS CONTAINED IN HONEYWELL PRIMUS 880 RADAR SYSTEM INSTALLATION MANUAL NO. 34-42-12, REV 3, DATED 2/15/00 AND THE HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM INSTALLATION MANUAL NO. 34-41-50, REV 5, DATED 2/15/01. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATIO N ❑ Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277719 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULA TIONS 06/07/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc) NAME OF APPLICANT Boeing Jet Aviation Associates 727-31 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-260, Initial Release, WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) dated 05/29/01 , • k... PURPOSE OF DATA •In support of major alteration to Boeing 727-31, serial num ber 20115, registration•number N980JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) FAR 25.1309 (a)(b)(g) . FAR 25.1529 FAR 25.1316 (b) CERTIFICATION — Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment ander data Fisted above and on attached sheets numb Part 183 orate Federal Aviation Regulations, ered NONE have been examined in accordance with established proce Regulations. dures and found to comply with applicable requiremen ts of the Federal Aviation El Recommend approval of these data I (I.Ve) Therefore X Approve these data (Systems & Equipment Aspects, Design Appr oval Only, Does Not Constitute Installation App roval) SIGNATU F DESIGN NG INE INC REPRESENTATIVE(S) DESIGNATION NUMBERS) CLASSIF/CAT/ON(S) DERT-510087-NM Systems & Equipment Nor an. J. ran . FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME SC-727-RDRDOC EFTA00277720 I EFTA00277721 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULA TIONS 06/07/2001 r AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc) NAME OF APPLICANT , Jet Aviation Associates Boeing Airplane • 727-31 West Palm Beach, FL LIST OF DATA IDENTIFICATION . TITLE B727-16236-260, Initial Release, WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) dated 05/29/01 i.. PURPOSE OF DATA In support of major alteration to Boeing 727-31, seri al num ber 20115, registration number N980JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) . FAR 25.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 25.1316 (b) CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and Etnitatimis of appointmen data listed above and on attached sheets t under Part I &I of the Federal Aviation Regulations numbered NONE have been examined in accordance with established procedures and , Regulations. found to comply with applicable requirements of the Federal Aviation ❑ Recommend approval of these data I (We) Therefore X Approve these data (Systems & Equipment Aspects, Design Approva l Only, Does Not Constitute Installation Approval) SIGNATU F DESIGN GINE G REPRESENTATTVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) • DERT-510087-NM Systems & Equipment Nor an J. ran FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901-6 13 FILENAME: SC-727-REIRDOC EFTA00277722 • EFTA00277723 May -29-01 01:58P N J Curran :352 2L1-:3 1O11 41, ••=mowm..1 • DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, ctc) NAME OF APPLICANT Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-261, Initial Release, HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM dated 04/10/01 • - . PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 26.1357 (a)(c) FAR 25.869 (a)(4) FAR 25.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1529 _ FAR 25.1309 (a)(b)(g) FAR 25.1351 (a) CERTIFICATION - trader authority vested by direction of the Administratsr sad is accordance with cooditivos and limitations of appointment under Parr ILI artist Federal Avisiien Regulations, dm) ram' aticre mid *a ttutitrd Skeels sumbered NONE tune Ices east:sized is setordaset with esiablished procedures sad found to comply with applicable rectoiroueom .f the Fed eTht Avialie • Rttoilatlikt- O Recommend approval of these data I I (We)Therefore 0 Approve these data (Systems & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) SIGNATU FD — •TED EN ERING RETRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION'S) 1 .1 &17- ---..- DERT-510087-NM Systems & Equipment Nor an . urran FAA Form 8110-3 (11.70) SUPERSEDES PREVIOUS EDMON GPO 901-613 FELENAME: SC-727-LTOSNSRDOC EFTA00277724 I EFTA00277725 DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 1, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane. Radio, Helicopter, etc.) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB - LIST OF DATA IDENTIFICATION TIRE B727-16236-1261 AT-855/RTA-880 Antenna Installations, Sht 1-7, Rev A B727-16236-1410 Dual FMS WI RTU Equipment Installations, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA . authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered 0 have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data. I Therefore Approve these data. ' SIGNATURE(S) OF. DESIGNATED ENGINEERING REPRESENTATIVE(S) , .. DESIGNATION NUMBER(S) ,,.:, : CLASSIFICATION(S) David E. HaralOn P,-.2(e. ii,,,,z.-I- ,,;:,s:4,' -4, DERT-810028-NE •••..'$1,- --.7=7 - -.-.4:-. ,- .• :1•447:, k• ••44 Structural ' ,44 . • - -• ,c,-"4-•. • -.. FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01202.doc EFTA00277726 • EFTA00277727 DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS May 28, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1262 LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2, Rev IR B727-16236-1342 Aero-M SATCOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561(b)(c) 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition s and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered 0 have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data. I 0,tX Therefore Approve these data. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) David E. Haralson Pc- t..,re /iced-46-- DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01205.doc L EFTA00277728 • EFTA00277729 DATE DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS May 28, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1262 LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2, Rev IR B727-16236-1342 Aero-M SATOOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA ._ authorized personnel. • PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561(b)(c) 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered 0 have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data. I Therefore Approve these data. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) David E. Haralson P.,,- e. // ,-1..,.--- DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01205.doc EFTA00277730 lr ft EFTA00277731 Form Approved 00 4 MAJOR REPAIR AND ALTERATION US Department OMB No. 2120-0020 of Transportation (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Federal Aviation Office Identification Administration 50- fsbo - 17 i INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instruc ' ns and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 . 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC. 103 FOULK RD. STE 202 , WILMINGTON DE. 19803-3742 . 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer \ s. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. X Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer _LIMITED AJF & ENG, D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachm ents hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual 7/2/01 • John K. Urso. Inspector. 1e ---c' 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 4 w inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is C.4 APPROVED ■ REJECTED FAA Flt. Standards Other (Specify) Inspector Manufac turer Inspection Authorization BY FAA Designee Person Approved by Transport X Repair Station Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 7/2/01 EYKR782D Ronald K. Bystrom. Manager Quality Assurance. FAA Form 337 (12-88) EFTA00277732 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirem ents. 8. Description of Work Accomplished (If more space is required, attach additional sheets, identify with aircraft nationality and registra tion mark and date work accomplished.) BOEING 727-31, S/N 20115, N908.1E, W/O 16236. ACCOMPLISHED A TCAS CHANGE 7 UPGRADE TO THE EXISTING HONEYWELL TCAS II SYSTEM PREVIOUSLY INSTALi.ED UNDER PAGE AVJET CORPORATION STC SA3094SO DATED 8/24/93. REFERENCE F.A.A. FORM 337 DATED 8/25/93. THE TCAS PROCESSOR P/N 4066010-904 WAS MODIFIED TO P/N 4066010-910 (CUSTOMERS UPGRADED UNIT) IN ACCORDANCE WITH TIMCO MASTER DRAWING LIST 01T012L001, REV IR, DATED 5/21/01. REFERENCE F.A.A. FORM 8110-3 DATED 5/21/01 BY SYSTEMS AND EQUIPMENT DER NO.DERT-510239-CE. THE TCAS II CHANGE 7 PROCESSOR WAS INSTALLED AND TESTED IN ACCORDANCE WITH TIMCO ENGINE ERING ORDER DOCUMENT 01T012E006, REV IR, DATED 5/21/01 WITH NO DISCREPANCIES. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE AIRCRAFT EQUIPMENT LIST WAS AMENDED AND ENTERED IN THE AIRCRAFT RECORDS. AIRWORTHINESS DIRECTIVE 94-01-04 AMENDMENT 39-8786 IS N/A TO THIS INSTALLATION BY PROCESSOR P/N. THERE IS NO CHANGE TO THE AIRCRAFT WEIGHT AND BALANCE. THERE IS NO CHANGE TO THE AIRCRAFTS MAINTENANCE FOR CONTINUED AIRWORTHINESS REQUIREMENT S DUE TO THIS INSTALLATION. THE REQUIRED F.A.A. APPROVED HONEYWELL INC, TCAS II FLIGHT MANUAL SUPPLEMENT DOCUMENT TCAS-A PPS-0294, REV A, DATED 3/21/00 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END ❑ Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277733 communications Aviation Communications & Surveillance Systems 21111 N. 19[11 Avenue Phoenix, AZ 85027-2708 602-436-7070 Fax: 602-436-6899 May 16, 2001 TIMCO 623 Radar Road Greensboro, NC 274 Attn.: Mr. Gregg Stutes Re: Letter of Authorization to use technical data Dear Mr. Stutes, This letter is to authorize TIMCO ("Recipient") to use the following technical data owned by L-3 Communications Corporation — Aviation Communications & Surveillance Systems (L-3) for the limited purpose indicated here below. The technical data subject to this Letter of Authorization (`date) is the L-3 developed data used to apply for the following FAA certifications: Supplemental Type Certificate STC SA4S34NM, as defined by ML4070349, for B727 aircraft. L-3 Authorization to use Data is limited to the following B727 aircraft tail number, namely: • B727 SIN 20115 L-3 Authorization to use Data is granted hereby for the sole purpose to provide the Recipient with technical information for its internal use and engineering review purposes. The Recipient recognizes L-3's proprietary rights in Data and will limit its disclosure to a need-to-know basis for its employees. The Recipient will not use Data for any other purposes than the internal use and engineering review purpose established for this Authorization. The Recipient will not sell, license, rent, market, transfer, assign, distribute, or otherwise disclose to any third party, exploit or permit any other use of Data. L-3 does not provide any warranty whatsoever on Data, whether express, or implied, or implied by law, including but not limited to merchantability and fitness for any particular purpose_ EFTA00277734 I I EFTA00277735 In no event shall L-3 be liable for. • Any direct, incidental, indirect, special or consequential damages including but not limited to loss of use, revenue or profit, even if L-3 has been advised, knew or should have known of the possibility of such damages; or • Damages caused by the Recipient's failure to perform its obligations and responsibilities; or • Claims, demands or aeons against the Recipient by any other party. The term of this Authorization is one (1) calendar year from its date. If during such term L-3 believes that its proprietary rights in Data are being infringed or injured or otherwise are at risk, L-3 reserves the right to terminate Authorization hereunder and, upon notice to Recipient, request the Recipient to discontinue any further use of Data. Upon termination of Authorization hereunder, the Recipient will either destroy or return Data in its possession and notify L-3 that no further use of Data will take place. For any communication concerning this Authorization, please contact F.W. (Bill) Lynch, Certification Engineer: Phone: (602) 436.2421 Fax: (602) 436.6899 E-mail - bill.lynch@L-3com.com PIease, countersign this Letter of Authorization and return it to us as follows: original by mail (with the original signature of your authorized representative); a copy by fax to the undersigned. Thank you for your interest. S E.W. (Bill) L ch Agent for L-3 Communications, ACSS EFTA00277736 I I EFTA00277737 United gRatts graica Bepartment of Zransportation—fidtral aviation administration supplemental Zppe Certificate Page Avjet Corporation Y.2€21,..e..ezpitt-eur4 43.4ezed-io 9809 Tradeport Drive Orlando, Florida 32827 25 Federal Aviation A3WE Boeing 727-100 Series gLi' di' n'94-;-& - ---611 '.6CAanf e': Installation of Provisions only for a Honeywell TCZ-910 TCAS II System in accordance with Page Avjet Master Drawing List MDL-91- 41, Initial Release, dated November 19, 1991, or later FAA approved revisions. /'7m-tat This approval should not be extended to other airplanes of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. zdte7a- ca, irv.e# / Az.n/e/Azzr- rre 44.eziyi.ende44.cw,LW, c14-7724nale z.'-cfa zik,wea&,e.11,214:14,/iy, //it • Cat in e3 ik t9 ‘41:Araidirtiz&im,ilezirte:nc.:Ilran'er-n, !Lk peZtJa,i: October 21, 1991 January 15, 1992 iinei4w./i•r hn Tigue (Signature nager, Atlanta Aircraft Certification Office (Title) Any alteration of this certificate is punishable by a.fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. This certificate may be transferred in accordance with F.-1R 21.47. FAA folua 8110-2 (10-68) EFTA00277738 r I EFTA00277739 DATE U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION -67'24/0/ L AVIATION REGULATIONS STATEMENT OF COMPLIANCE WITH THE FEDERA ION AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICAT TYPE (AIRPLANE, RADIO, HEUCOPTER, NAME OF APPLICANT MAKE MODEL NO. ETC.) 727-100 Airplane TIMCO Boeing LIST OF DATA TITLE IDENTIFICATION Boeing 727-100 TIMCO Master Data Honeywell TCAS II Change 7 Software Upgrade for a List, 01T012L001 Rev IR Dated 5/21/01 - END OF DATA - - - . • PURPOSE OF DATA a Boeing 727-100 aircraft. STC SA4834NM is app rov e the inst alla tion of a TCA S Cha nge 7 in To document and the approval basis for this installation. APPLICABLE REQUIREMENTS (Listspedricsections) FAR 25.1301 (a), (c) - v • vest ed by dire ctio n of the Adm inist rato r and in acco rdance with conditions and limitations of CERTIFICATION - Under authority e and on attached sheets numbered Fed eral Avi atio n Reg ulat ions , data liste d abov appointment under Part 183 of the ed proc edur es and foun d to comply with applicable have been examined in acco rdan ce with esta blish requirements of the Federal Aviation Regulations ) Therefore 0 Recommend approval of these data 1 ... Approve these data E(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIV • DERT-510239CE System & Equipment Robert McClellan 14 GPO 901-613 FAA For m 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION • EFTA00277740 • III EFTA00277741 FORM NO.: EN•0003 TIMCO ENGINEERED SYSTEMS, I.. DATE: 01/01/00 u,"WON 5,40 CommY A MASTER DATA LIST • TITLE: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE MDL NO. 01T012L001 REV/DATE: IR / 5/21/01 STC / FAA PROJECT NO.: SA4834NM / 650259 AIRCRAFT TYPE: BOEING 727-100 ENGINEER: P. FERGUS APPROVAL: ROBERT MCCLELLAN SHEET 1 OF 1 DOCUMENT REVISION TITLE SHT NUMBER LTR DATE 01T012C002 IR 5/21/01 HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE FOR A BOEING 727-100 1 ISSUED vim 2 2 zttl wool collinot. Th'sda's'Pr'Perv'''PrglIe0V: rTritTa:,','°iTtezierrdsarazix=sovr',d,==sur,Veotr=unThsc=roarnTdV,===.L1 er,:mgte=1,72;ebs=t7V-I"E"'"er""s`e"'In'and Copyright (C) 2000 TIMCO Engineered Systems, Inc. EFTA00277742 011.012L0015 Stock No.: 091100108 I • EFTA00277743 Form No.: EN-0008 TIMCO ENGINEERED SYSTEMS. !sc. Date: 01/01/00 ANAWVI$.13 CO/MWY A CONFIGURATION DOCUMENT . TITLE: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE FOR A BOEING 727-100 CFG NO, 01T012C002 REV/DATE: IR/ 5121/01 ENGINEER: P. Fergus APPROVAL: Robert McClellan SHEET 1 OF 1 I. CONFIGURATION DATA A. APPLICABLE MDL: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE # 01T012L001 B. EFFECTIVITY I SSUED 2 2 20 1. BOEING 727-100 SERIAL NO. 20115 MAY CONTROL C. DESCRIPTION CION.MEta 1. THIS INSTALLATION WILL CONSIST OF USING STC SA4834NM AS THE APPROVAL BASIS TO PERFORM THE TCAS CHANGE 7 MODIFICATION TO THE TCAS COMPUTER UNIT, D. DEVIATION FROM PREVIOUSLY APPROVED DATA , 1. NONE Items marked with an asterisk (*) are for manufacturing and certification and will not be supplied. If required, the documents will be sent directly to the customer's certification authority only after TIMCO receives assurance that their confidentiality will be protected. DOCUMENT REVISION NUMBER LTR DATE TITLE SHT 01T012E006 IR 5/21/01 Installation of a Honeywell TCAS II CU with Change 7 in a Boeing 727-100 6 01T012R007 IR 5/21/01 Description and Substantiation of a TCAS II Change 7 Installation 2 'This data Is the properly of. and proprietary to, TIMCO Engineered Systems, Inc, and Is restricted for use by designated persons, firms or corporations with whom contracts have been entered Into. User agrees to Indemnify TIMCO Engineered Systems, Inc. and to hold It hornless against any claim arising by reason of the possession or use thereof. lis unauthorized use and duplication Is prohibited, and it Is protected under an unpublished copyright' Copyright (C) 2000 TIMCO Engineered Systems. Inc. •1 Stock No.: 091100403 EFTA00277744 1:1017012 Jet AviattonN0IT012C002S.doc 1 F • e EFTA00277745 Form No.: EN•0002 TIMCO ENGINEERED SYSTEMS. Pro. Date: 01/01/00 AmAwn.SALES Cosawm A ENGINEERING ORDER E.O. TITLE: Installation of a Honeywell TCAS II CU with Change 7 in a Boeing 727-100 E.O. NO.: 01T012E006 AIRCRAFT: Boeing 727-100 REV: IR DATE: 5/21/01 INITIAL RELEASE REVIEWS R Fergus ISSUED PkEPARE , -,',:- .,,:,.-' .:,! MAY 2 2 21101 David Thornton DOCUMENT. CONTROL. tilEtKEtit ii-A:: ::T-f4aV :„ - •• .. :•-,',,,,.., Richard Cunningham ,QA- 13gyIE -.. :.-:,, -----=: s 41;-,EE,_.;.• -,,;-:-? Robert McClellan ',_, , Rtiv-E- 1 - : ... . ..,, _........ .. •. -,N.-5i.-s3,- -:•.; -,. ..x...4 ---A_,-- --,,,,. ,--44-*: --:•••-,4•:•.-!..--,-_ ...,...... :•••••• •,-,•:-:.,,.„•,,, ,-,-,...t,„ TIMCO ENGINEERED SYSTEMS, INC. 623 Radar Road Greensboro, North Carolina 27410 Telephone: (336) 668-4410 This data is the property of, and proprietary to. TIMCO Engineered Systems. Inc. and is restricted for use by designated persons, firms or corporations viith whom contracts have been entered Into. User agrees to indemnify TIMCO Engineered Systems, Inc. and to hold it harmless against arty claim arising by reason of the possession or use thereof. Its unauthorized use and duplication is prohibited, and it is protected under art unpublished copyright,' Copyright (C) 2000 TIMCO Engineered Systems. Inc. 01T012E0065 Stock No.: 091100106 EFTA00277746 S a EFTA00277747 Honeywell Inc . AFM SUPPLEMENT 21111 North 19th Ave. General TCAS/ACAS Applications Phoenix, .AZ 85027 Spec. No. TCAS -APPS- 0294 FAA APPROVED WHEN EQUIPPED WITH HONEYWELL TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM ( TCAS II ) This supplement must be attached to the FAA Approved Airplane Flight Manual for aircraft that have been modified by installation of the Honeywell Traffic Alert and Collision Avoidance System (TCAS II) in accordance with a Honeywell STC (see SECTION I). The information contained in this document supplements and supersedes the basic manual only in those areas listed. For limitations, procedures, and performance information not contained in this supplement, consult the basic Airplane Flight Manual. FAA APPROVED Manager, Flight Test Branch, ANM-160L Federal Aviation Administration Los Angeles Aircraft Certification Office Tranport Airplane Directorate Date EFTA00277748 r 4.• • EFTA00277749 I 0 Form Approved MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 US Departmwt of Tran_sportatIon (Airframe, Powerplant, Propeller, or Appliance) For FAA Use O ly Office Identification Federal Aviation Administration So- r-sDo- f 7 cik)' INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instreitions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to keed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC. 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1above) X POWERPLANT PROPELLER Type • APPLIANCE Manufacturer . s. • 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. ---, 1515 PERIMETER RD. x Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer LTMIT11I2 AIF & ENG, D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized lndi idual 7/2/01 . John K. Urso. Inspector. L,,, /C. 7. Approval for Return to Servl Pursuant to the authority given persons specified below, the unit identified in item 4 w s inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is CI APPROVED III REJECTED Other (Specify) FAA Fit. Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. , 7/2/01 Ronald K. Bystrom. Manager Quality Assuranc / EYKR782D FAA Form 337 (12-S8) EFTA00277750 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. • 8. Description of Work Accomplished (if more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, S/N 20115, N908JE, W/O 16236. INSTALLED A UNIVERSAL AVIONICS TT-3000 SERIES AREO-M SATCOM SYSTEM PER UNIVERSAL AVIONICS AIRBORNE SATELLITE TELECOMMUNICATIONS SYSTEM INSTALLATION MANUAL NO. 23-15-02 DATED 3/7/01. SYSTEM CONSISTS OF 2 EA HANDSETS, 1 EA ANTENNA, 1 EA HIGH POWER / LOW NOISE AMP AND THE SATELLITE DATA UNIT. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING: • B727-13236-340, REV. IR, DATED 4/30/01, SHEETS 1 THRU 3, 'I I1LED -1T-3000 AERO-M AIRBORNE SATELLITE TELECOMMUNICATIONS SYSTEM. REFERENCE FAA FORM 8110-3 DATED 5/29/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-1340, REV. A, DATED 5/29/01, SHEETS 1 THRU 5, TITLED - AERO-M SATCOM ANTENNA INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 6/18/01, BY STRUCTURAL D.E.R. NO. DERT-510024-CE. • B727-16236-1342, REV. IR, DATED 5/2I/01, SHEETS 1 THRU 7, TITLED - AERO-M SATCOM EQUIPMENT INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 5/28/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. SYSTEM TESTED PER UNIVERSAL AVIONICS INSTALLATION MANUAL FOR TT-3000 SERIES AERO-M, DOCUMENT 23-15-02, DATED 3/7/01 WITH NO DEFECTS NOTED. NOTE: UNIVERSAL AVIONICS SERVICE BULLETIN NUMBER 10101.00-23-2669, BLOCKING OF BREATHING HOJ RS IN SATCOM ANTENNA P/N 10101-00, DATED 7/25/00, WAS INCORPORATED AT ANTENNA INSTALLATION. THIS HAS NO EH.ECT OF THE STRUCTURAL OR MECHANICAL INSTALLATION OF THE ANTENNA. AN EMI TEST, REPORT NO. B727-16236-080, REV IR, DATED 6/19/01 WAS CONDUCTED AND THE INSTAII.FD EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/401 WAS COMPLETED IN ACCORDANCE WITH 43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC 43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED THE INSTALLATION CONFORM TO AC 43.13-1B, CHAPTER 5, SECTIONS 1 AND 2, CHAPTER 7, SECTIONS 1, 2,4 AND 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURE OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC 43.13-1B, CHAPTER 11, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED IAW AC 43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17- 19 AND AC 43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC 43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH SECTION 16. ELEC1RONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURES INSTRUCTIONS AND AC 43.13-2B, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS MODIFICATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC 43.13-1B, CHAFFER 10, SECTION 2 AND AC 43.13-2A, CHAF1ER 1 PARAGRAPH 9. PER THE AERO-M SATCOM INSTALLATION MANUAL ALL COMPONENTS ARE CONSIDERED LINE REPLACEABLE UNITS AND DO NOT Al.PECT THE MANUFACTURERS INSTRUCTIONS FOR CONTINUING AIRWORTHINESS. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATE6112001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333-CE. THERE ARE NO COCKPIT PROCEDURAL CHANGES OR FLIGHT MANUAL SUPPLEMENTS REQUIRED FOR THIS INSTALLATION. END ❑ Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277751 May-29-01 01:58P N 3 Curran 352 243 1011 P _ 02 c DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc) NAME OF APPLICANT Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE • B727-16236-340, Initial Release, TT-3000 SERIES AERO-M AIRBORNE SATELLITE TELECOMMUNICATIONS dated 04/30/01 SYSTEM - • PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 25.1316 (b) CERTIFICATION - Vetter authority vested by direction of theAdmInblrator and in accordance with conditions and reasitationa of appointment nodes- Part 113 or the Federal Aviatina Revalatiosts. data ;wed above aid on attached slims numbered NONE hare been examined in accordance with established procedures and found to coutply with applicable nrelairensenta of the Federal Aviation Rscalm:ans. 0 Recommend approval of these data I (We) Therefore El Approve these data (Systems & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) SIGNATUR FD NA D EN ' ERING REPRESENTAT1VE(S) DESIGNATION NUNIBERIS) CLASSIF1CATIONIS) r Zezee---_ DERT-510087-NM Systems & Equipment No an Jurran oral 8110.3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901.613 FILENAME: SC-727-SATCOMDOC EFTA00277752 a 3 EFTA00277753 U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTATION June 18, 2001 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS _ AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL TYPE (Airplane, Radio. Hs! copra, etc) NAME OF APPLICANT Boeing B727-31 Airplane Jet Aviation LIST OF DATA IDIENIIFICA1 ION III LE Jet Aviation Aero-M Satcom Antenna Installation Engineering Drawing Boeing 727-31 / S/N: 20115 / N908JE No. B727-16236-1340, Dtd. 5/29/2001, Rev. END END END END END END END END A Note: The certification basis of this aircraft includes FAR 25.571 Damage - tolerance and fatigue evaluation of structure. Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness END END of Structural Repairs on Transport Category Airplanes, the damage tolerance and fatigue evaluation of the structure must be performed before 6/18/2002. •- Notes: I) The structural aspects only of the above listed data are approved herein. 2) This approval is valid for the aircraft model and serial number listed below 3) This approval is based on structural analysis on file at DER Services corporate office in Ft. Lauderdale, FL. Model No. B727-31 Serial No. 20115 PURPOSE Approve data for antenna installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS (LISTSPEC.'FIC SECTIONS) 25.301, 25.303, 25.305, 25.307, 25.601, 25.603, 25.605, 25.609, 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition and appointment under Part 183 of the Federal.Aviation Regulations, data listed above and on attached sheets numberedliml tions of O been examined In accordance with established procedures and found to comply with applicable requirements of the Fe eral have Aviation Regulations. Recommend approval of these data I ) Therefore ri ,;i1 1 Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S)DESIGNATION NUMBER (S) CLASSIFICATION(S) Robert J. Belgau DERT-510024-CE Structures e........................ .„QA)15 FAA FORM 81I0-3 (11-70) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. 2001-082 EFTA00277754 Vi EFTA00277755 DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS May 28, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1262 LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2, Rev IR B727-16236-1342 Aero-M SATCOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561(b)(c) 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered 0 have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data. I Therefore Approve these data. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) David E. Haralson it7,-„,e. 14.....r...._ DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01205.doc EFTA00277756 • • EFTA00277757 DEPARTMENT OF TRANSPORTATION • DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS JUNE 12, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. NAME OF APPLICANT TYPE (Airoule, its dio. Heticaptcr, etc.) BOEING 727-31 • • AIRPLANE - JET AVIATION LIST OF DATA WENTIFICAllON T171.-E A.T.E. INC. BOEING 727-31 SIN 20115, AERO-M SATCOM ANTENNA INSTL., UPPER B.S. 360-390; STRUCTURAL REPORT GPS ANTENNA INSTL., UPPER B.S. 312-328; AIRCELL AGT.01 ANTENNA INSTL., No. ATE6112001 LOWER B.S. 400-420 DAMAGE TOLERANCE ANALYSIS; SH. 1-31, REV. (IR) - . •- NOTE: REQUIRED INSPECTIONS ATTAQBED THESE DATA APPLY ONLY TO BOERNIG 727-31 S/N 20115 . . . . PURPOSE OF DATA . . TO APPROVE - DATA FOR DAMAGE TOLERANCE ANALYSIS, B-727-3I S/N 20115 , APPLICABLE REQUIREMENTS (Lis specific sectioas) . - . FAR 25.571 (STRUCTURAL, ASPECTS ONLY) ' . • . CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations • of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets . numbered 1 of 1 have been examined in accordance with established procedures and found to comply with applicable requirements ,g, of the Federal Aviation Regulations. I (Ye) Therefore Recommend approval of these data Approve these data ' SIGNATURES) OF DESIGNATED ENGINEERING DESIGNATION NUMBER(S) CLASSIFICATION(S) /' • DERT-5 I 0333-CE STRUCTURAL t . . - • . • _. FAA Form 8110-3 tit :70) SUPERSEDES PREVIOUS EDMON cro 901-613 EFTA00277758 .14 ii. • 4 • • EFTA00277759 UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND 2 MANUFACTURER AND MODEL 3 AIRCRAFT SERIAL 4 CATEGORY REGISTRATION MARKS NUMBER N908JE BOEING 727-31 20115 TRANSPORT 5 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and certifies that, as of the date of issuance, the aircraft to which issued has been inspected and found to conform to the type certificate therefor, to be in condition for safe operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provide by Annex 8 to the Convention of International Civil Aviation, except as noted herein. Exceptions: NONE 6 TERMS AND CONDITIONS Unless sooner surrendered, suspended, ed, or a termination date is otherwise established by the Administrator, this airworthiness certificate is effective as lo g as e maintenance, prey: ative maintenance, and alterations are performed in accordance with Parts 21, 43, and 91 of e F • e I Aviation Regul o , as appropriate, and the aircraft is registered in the United States. DATE OF ISSUANCE DESIGNATION NUMBER R may 17 2001 SO17 Any alteration. reproduction, or misuse of this flute may be punishable by a fine not exceeding 31,000, or imprisonment not exceeding 3 years or both. THIS CERTIFICATE MUST DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) AFS Electronic Forms System -JetForm FormFlow -1211998 EFTA00277760 Is P EFTA00277761 I UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE I . MANUFACTURER AND MODEL 3 AIRCRAFT SERIAL 4 CATEGORY 1 NATIONALITY AND NUMBER REGISTRATION MARKS IP. N505LS BOEING 727-31 20115 TRANSPORT 5. AUTHORITY AND BASIS FOR ISSUANCE of issuance, the This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and certifies that, as of the date condition for safe aircraft to which issued has been inspected and found to conform to the type certificate therefor. to be in airworthiness code as operation. and has been shown to meet the requirements of the applicable comprehensive and detailed provided by Annex 8 to the Convention on International Civil Aviation, except as noted herein, Exception 4- NONE 6. TERMS AND CONDITIONS Administrator, this Unless sooner surrendered. suspended, revoked, or a termination date is otherwise established by the ions are performed in airworthiness certificate ts effective as long as the maintenance, preventative maintenance, and alterat in the United accordance withParts 21. 43. and91 of the Federal AviationRegulations. as appropriate, and the aircraft is registered States. DATE OF ISSUANCE DESIGNATION NUMBER R 07-23-90 JAY GLO7 Any alteration. reproduction, or misuse of this certi to ma punishable by a fine not exceeding $1.000. or imprisonment not exceeding 3 years. or both. THIS CERTIFICATE MUST DIS ED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. *U.S.G.RO.: 1994-568-762 FAA Form 8100-2 (8-62) EFTA00277762 I la r 2, a at SM S '► EFTA00277763 el Form Approved O/v1B No. 2120.0020 MAJOR REPAIR AND ALTERATION U.S. Department of (Airframe, Powerplant, Propeller, or Appliance) Transportation For FAA Use Only Federal Aviation Office Identification Adniinistration _ - ,zto —./- 9 /0 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B , and AC 43.9-1 (or subsequent revision form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty thereof for instructions and disposition of this not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Boeing 727-31 Serial No. Nationality and Registration Mark 20115 N505LS 1. Aircraft Name (As shown on registration certificate) Address (as shown on registration certificate) NORTHWEST DELAWARE CORP 1105 N. MARKET ST 2. Owner WILMINGTON DE 19899 3. For FAA Use Only • . 4. Unit Identification . 5. Type Unit Make Model Serial No. . Repair Alteration AIRFRAME - (As deieribed in item 1 above) — - - XX POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B Kind of Agency C. Certificate No. • TIMCO . U.S. Certificated Mechanic DU4R141M Foreign Certificated Mechanic Lake City Municipal Airport X Certificated Repair Station Lake City, FL 32025 Manufacturer ' D. I certify that the repair and/or alteration made to the units identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual August 23, 1999 Arthur E. Saylor a' ,4 6?"aft 7. Approval for Return To Sex-vice Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 10 APPROVED • REJECTED FAA Flt. Standards Manufacturer Inspection Authorization Other (Specify) Inspector FAA Designee X Repair Station Person Approved by Transport Canada .. BY Airworthiness Group • Date of Approval or Rejection Certificate or Designation No. Signature of Authorized ividual August 23, 1999 DU4R141M Scott L. Palm FAA Form 337 (12-88) This 337 supersedes 337 dated August 7, 1999 EFTA00277764 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished ted.) (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work comple Boeing 727-31 Reg. No. N505LS S/N 20015 August 23, 1999 Page 1 The following major repairs were accomplished: 1. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 56 IAW TIMCO E.O. 99-1190 Rev. I/R dated 12 JUL 99 Approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delmainated skin above #2 engine pylon L/H side at stations 1342.4, 1371.5 and 1387.85 IAW TIMCO E.O. 99-1191 Rev. I/R dated 23 Jul 99 approved per FAA Form 8110-3 by DER D. Joynes DER #DERY-635317-NM dated 21 July 99. 3. 060H1-0027 Repaired cracked and disbonded #2 engine upper skin on aft fairing assembly IAW ROHR Engineering Repair t 3, Data Sheet and FAA Form 8110-3 by DER Jeffrey D. Shutrump DER #DERY-605526-NM dated Augus 1999. SUMMARY 8110-3's. 1. All work accomplished IAW TIMCO E.O.'s, ROHR Engineering Repair Data Sheet and FAA Form 2. Records of all work accomplished is on file at this repair station under work order 060/T-361. end ❑ Additional Sheets Are Attached * U.S. GOVERNMENT PRINTING OFFICE: 1992.169.012/601S7 EFTA00277765 9) Form Approved MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 U.S. Department of (Airframe, Powerplant, Propeller, or Appliance) Transportation For FAA Use Only Federal Aviation • Office Identification Administration .---- / ---5 1) —C•C 7X INSTRUCTIONS: Print or type all entries. See FAR 43.9,. FAR 43 Appendix B , and AC 43.9-1 (or subsequent revision thereof for instructio form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each ns and disposition of this Aviation Act of 1958). such violation (Section 901 Federal Make Model Boeing 727-31 Serial No. Nationality and Registration Mark 20115 N505LS 1. Aircraft Name (As shown on registration certificate) Address (as shown on registration certificate) NORTHWEST DELAWARE CORP 1105 N. MARKET ST 2. Chvner WILMINGTON DE 19899 3. For FAA Use Only • 4. Unit Identification 5. Type' Unit Make Model Serial No. Repair Alteration , AIRFRAME (As described in item 1 above) — )O( POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. TIMCO • U.S. Certificated Mechanic DU4R141M Foreign Certificated Mechanic Lake City Municipal Airport X Certificated Repair Station Lake City, FL 32025 Manufacturer D. I certify that the repair and/or alteration made to the units identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with requirements of Part 43 of the U.S. Federal Aviation Reguiations and that the information furnished herein is true and correct to the best of my knowledge. Date August 7, 1999 Signature of Authorized Gregory A Christman 4/ ____- i 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the aruier prescribed by the Administrator of the Federal Aviation Administration and is E3 APPROVED El REJECTED FAA Flt. Standards Manufacturer . Inspection Authorization Other (Specify) Inspector FAA Designee X Repair Station Person Approved by Transport Canada BY Airworthiness Gro Date of Approval or Rejection Certificate or Designation No. August 7, 1999 Signature of Au - ed Individual out L. Palm DU4R141M FAA Form 337 (12-88) EFTA00277766 4 . NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Boeing 727-31 Reg. No. N505LS S/N 20115 August 7, 1999 Page 1 The following major repairs were accomplished: 1. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 45.5 IAW 'HMCO E.O. 99-1190 Rev. UR dated 12 JUL 99 approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delaminated skin above #2 engine pylon L/H side at stations 1342.4, 1371.5 and 1387.85 IAW TIIVICO E.O. 99-1191 Rev. I/R dated 23 Jul 99 approved per FAA form 8110-3 by DER D. Joynes DER #DF.RY-635317-NM dated 21 July 99. 3. 060H1-0027 Repaired cracked and disbonded #2 engine upper skin on aft fairing assembly IAW ROHR Engineering Repair Data Sheetand FAA Form 8110-3 by DER Jefa ey D. Shutrump DER #DERY-605526-NM dated August 3, 1999. SUMMARY 1. All work accomplished TAW 'HMCO E.O.'s , ROHA Engineering Repair Data Sheet and FAA Form 8110-3's. 2. Records of all work accomplished are on file at this repair station under work order 060/T361. end ❑ Additional Sheets Are Attached * U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 EFTA00277767 trul,21 1999, 22:06 PDT MsgNum: CPZ-LRK-99-00014H Pa 117/Zr/99 WED 16:06 FAX 9 544 7667 ge 2 of 2 0001 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DATE STATEMENT OF COMPLIANC .__. E WITH THE FEDERAL AVIATI AIRCRAFT OR AIRCRAFT CO ON REGULATIONS WI:1 /141 i1 Aj 0 1 MPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter. etc.) NAME OF APPLICANT Boeing 727 Airplane • Boeing Commercial • Airplane Group LIST OF DATA IDENTIFICATION TITLE . Subject Center Engine Support Skin. Panel Corrosion, Delaminatio • n Requestor: TIMCO (CPZ) for The . Limited (LII) • Part Number/ Serial Number: 65 -17556 Model No.: 727-100 Serial No.: Registry No.: NSOOLS 20115 Basic No.: E2218 Variable No.: E3704 Line No.: 735 • Flight Cycles: 21643 Ho urs : •: . • 31 83 5 . . Service Bulletin /AD: N/A . . - - CPZ-L Mk99-02041;R • . - TIMCO telex with description Of . Date&•9.1u1•199p- - • blend delamination areas at StatiOnSI3713 out and doubler repairs to corrosion and •-.,-,..i. . : 1387.85, and 1342.4. - - CPZ-1_11. 199-000.061-I • Boeing reply that repairs ar6itiiidniiit Dated- 12 Jul-1999 . : - iy. tgfaciory with prciviSi0ns. : . , — — .. , - • • CPZ-LRIC---99-0208TR: • -. ' •ITMCO telex . • . with-statementthatl4aii: hai bee Dated 19 Jul 1'999 for 8110-3 form. n co inp ieted fier• disi:iiisition• andreq'tieSi • : • ' • •• - • • • • - ' • :: . _ - • .. - . • . . - - • • • . . ... —, . - • • • .— • • ,. . • PURPOSE OF DATA Structural Substantiation of Re pair Plan APPLICABLE REQUIREMENTS (List specific section) CAR 4b - - Subpart C: 4b.200 through 4b.20 2, 4b.270 Subpart D: 46.300 through 4b.30 4(a), 4b.306(a)&(b) CERTIFICATION - Under authority vested by direction of the Administrator and of appointment under Part 183 of the Federal Re in gulations, data listed above and on accordance with.conditions and limitations : have been examined in accordanc attached sheets numbered requirements of the Federil Aviation Regulatio e wit h established procedures and found ns. to comply with applicable I (We-) Therefore Recommend approval of these data • Approve these data SIGNATURE(s) OF DESIGNATED ENGIN ING REPR ESENTATIVE(s) DESIGNATION NUMBER(s) CLASSIFICATION(s) D. Joy nes ..---1) .....„...—,. DERY-635317-NM Structures FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITI ON Page 1 of 1 EFTA00277768 a I e • EFTA00277769 07/15/99 15:54 FAX 3366651786 TIMCO ENGINEERING • • ar•PZEIME.M.FIRM. -0 LAKE CITY f?)002 U.S. DEPARTMENT OF TRANSPORTATIO N FEDERAL AVIATION ADMINISTRATION DATE STATEMENT OF COMPLIANCE WITH THE FE DERA L AVIATION REGULATIONS July 12, 1999 AIRCRAFT OR AIRCRAFT COMPON ENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Herrcopler, etc .) NAME OF APPLICANT ,Boeing . 727 Airplane TIMCO LIST OF DATA IDENTIFICATION TITLE TIMCO E.O. 99-1190, 8727; SEAT TRACK: STATION Rev. I/R. 662, RBL 56 CORROSION BLEN DOUT REPAIR. Dated 12 JUL 99 TIMCO REPORT NO. STRESS ANALYSIS; SEAT TRAC S.A. 99-1190, Rev. l/R. K CORROSION REPAIR AT ST A 663 RBL 54 Dated 12 JULY 99 . END . . NOTES: 1. This approval is for Northwe st Delaware aircraft N505LS, S/ N 20115 only. PURPOSE OF DATA In support of a Major Repair accomp lished on aircraft S/N 20115. This only and is not installation approval. approval is for design and static analy sis APPLICABLE REQUIREMENTS (List spe cific sections) FAR 25.301, 25.305, 25.601, 25.603, 25.605, 25.609 and 25.613. CERTIFICATION - Under authority vested by dire ction of the Administrator Part 183 of the Federal Aviation Regulatio and in accordance with con ditions and limitations of appointment with established procedures and ns, data listed above and on attache under found to comply with applicable d she ets num ber ed WA requirements of the Federal Aviatio hav e bee n exa min ed In accordance n Regulations. IN Recommend approval of those da ta I (wile) Th erefore O. Approve th ese data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTAT IVE(S) DESIGNATION NUMBERS(S) CLASSIFICATION(S) Wayne Fink DERT-510117-CE 4 ._------- STRUCTURES _....... . __. orm - SUPERSEDES PREVIOUS ED ITION ELECTRONIC FORMAT (4-99) EFTA00277770 a In • • EFTA00277771 8- . . 4: bb YM ;6UF6K 27 FKUUKAM bl9bH.1.2232;g 2/ 8 .••. " • • • . - •. •• — _ U.S. DEPARTMENT OF TRANSPORTATION DATE . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS August 3, 1999 4 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 4 MAKE MODEL NO_ TYPE (Airplane. Radio, Helicopter, etc.) NAME OF APPLICANT Boeing 727 . Airplane Rohr, Inc. LIST OF DATA IDENTIFICATION _ TITLE (Ref. ERDS C1036) EROS CI 036 Engineering Repair Data Sheet, Definition of discrepancy and repair design for P/N dated August 3, 1999 1/A545300-1 (Aft Skin - Upper Skin Assembly) . 41 -/4.' • B- Cox Skin Disband VA545300-1 Stress Analysis !Doted August 3, 1999 • • • . - • ' . PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. APPLICABLE REQUIREMENTS (List specoc sections) (1) FAR 25.301 (1) FAR 25.307(a) (1) FAR 25.605(a) (1) FAR 25.619 (1) FAR 25.303 . (I) FAR 25.601(a) (1) FAR 25.609(a) (1) FAR 25.305(a)(b) (1) FAR 25.603 (1) FAR 25.613(a)-(d) .c • CERTIFICATION — Under authority vested by direction of the Administrator and in accord ance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations. data listed above and on attache d sheets numbered ' NONE have been examined in accordance with established procedures and found to comply with applicable requirement) of the Federal Aviation Regulations. I (We) Therefore 7 Recommend approval of these data SIGNATURE(S) OF LJESIUNATED ENGINEERING EgApprove these data • E ESENTATIvES Off$IGNATION NUMBER(3) CLAS3IFICATION(8) (1) Jeffrey D.Shutrump DERY-605526-NM Structures - . . " FAA Form 81104 (11-70) SUPERSEDES PREVIOUS EDITION (Computer Generated by Rohr, Inc.) EFTA00277772 , • Y so a 4 • • EFTA00277773 CLASS EROS NO. REV. PAGE O0OO ENGINEERING REPAIR MAJOR C1036 MOO ROHR, INC. I DATA SHEET (EROS) HaHH 6.50 Lagoon Drive Chub VIr2. Ca ttnta 91910 - Z198 FORM 8110.3 REQUIRED S.O. NQ N/A REV. OF 2 F3 PART NO. PART SERIAL NO. MODEL COMPONENT SERVICE I-CURS CUSTOMER VA545300-1 N/A V727RE AFT FAIRING -UPPER SKIN ASSY UNK THE LIMITED Lz xggrIR! W1 REPAIR: DISCREPANCY: (BE SPECIFIC - PRINT CLEARLY ) ITEM A. Repair. ITEM A. The upper skin on the AFT fairing assembly, P/N UPPER SKIN REPAIR .VA545300-1, on the #1 Engine position shows a disbanded condition on approximately 50% of the AFT surface, including 1. Remove discrepant upper skin from assy. Care should be two crescent shaped cracks on an existing repair (fiberglass?). taken not to disbond the lower skin of the assy. On this same arevon the lower surface of the panel, an area of 2. Fabricate a new upper skin from .032 gauge 202443 per QQ- material is also missing and filled as above. The lower repair A-250/5. stops before transitioning to pan down of honeycomb. • 3. Remove lower surface Clad (bonding side). Do not thin below See page 2 for sketch of location and description. .029. 4. Make sure all remaining "old" adhesive is removed from core. MATERIALS: Clean and prep skin (using PAA or Pasa-Jell 105) and exposed Upper Skin .032 2024-T3 QQ-A-250/5 core (using Pasa-Jell 105) on panel. Clean repair area per 727' Lower Skin .016 2024-0 QQ-A-25015 SRM 51-40-6, Par. G(2) (SRM 51-40-5). Heat treated to —T42 per MIL-H-6088 5. Prime bond side of skin and core with BR-127 adhesiVe Honeycomb .310-3116-10 (5052) MIL-C-7438 primer, per manufacturer specifications. 6. Apply two.coats of FM-73 adhesive material, per manufacturer specifications. 7. Bond replacement upper skin to core and lower skin per 727 SRM, 51.40-6, paragraphs E, J & K 8. Perform Post Bond inspection byvisually inspection of periphery for evidence of adhesive bead, and tap test the whole panel for voids. ORIGINAL when tilts stamp rearms! co is to rid ink t!ZEZZT696T9 PREPARED BY DATE AIRWORTHINESS APPROVAL DATE Don Adams 8-02-99 -_? 7 FOR.41NO. E6687,5 EFTA00277774 > EFTA00277775 OOOO 42OOO RDS NO. REV. PAGE ENGINEERING REPAIR ROHR ROHR.INC. DATA SHEET C1036 2 OF &X Lag= Dave (ERDS) .0. NO. REV. Chtia Vida. CAlrfunia 91910-2098 SUPPLEMENT SHEET N/A 2 (DISPOSITION CONTIUNUED) (1;scR6Rirkticy ecivrieiver)) LOWER SKIN REPAIR 1. Remove existing repair (fiberglass) from discrepant area on lower surface. . 2. Cut filler to size of discrepant area from .016 gauge .11tIZ71 2024-13 per QQ-A-25015. 3. Fabricate doubler from .020 gauge 2024-0, per QQ-A- 250/5 to cover filler. Doubler to overlap filler periphery by 1.50 min. Optional to use 2024-T3, no heat treatment required. 4. Form doubler to match lower skin contour per BAC 5300. Heat treat to -T42 per BAC 5602 or MIL-H-6088. Verify hardness per SRM requirements. 5. Inboard and outboard edges of doubler to be tapered to .010 min. Care should be taken so the edges of the doubler land mid spaced between existing assembly fasteners_ 6. Install doubler using steps 3 through 8 above. 7. Install new panel, filler & doubler using BP fasteners to complete assembly. Apply sealant to edge of logo light cut out , and seal all gaps at assembly. 8. Clear Alodine all external clad surfaces per MIL-C-5541, Class 3. ORIGINALl uvrmusr, When this stamp , is in red Ink FORM NO. E7983-1 EFTA00277776 EFTA00277777 8- 3-99 4:55 PM ;SUPER 27 PROGRAM 6196912232;# 5/ 8 DODD By B. COX DATE 08/02/99 EH= PAGE 1 of 4 cHK'D1-51)07O) ERDS Cl DATE OM ROHR TITLE Skin Disbond VA545300-1 ROHR, INC. Use or disclosure of this information is subject to the restriction on the title page or on the first page of this document Super 27 I. Discrepancy: The outer skin of the upper skin assembly of the aft fairing is disbonded and the aft edge of the outer skin has two cracks. See sketch below from ERDS. I!. Proposed Disposition: Remove the outer skin of the upper skin assembly and bond on a new outer skin using FM 73 adhesive and BR.127..adhesive primer. The cracks at the aft edge have been reported to be along a previous repair that was filled with a fiberglass patch repair. The fiberglass patch will be removed and replaced with a metallic patch and doubler. All metallic materials will be the same as BP materials. III. Static Analysis: The aft fairing is analyzed in section 10 of Reference'. In section 10 of Reference ', the substructure has been analyzed to withstand all the aerodynamic loading without using any of the skin as affective. Therefore, this analysis will only investigate the capability of the adhesive to carry the shear stress to the core conservatively assuming that the skin will carry the aerodynamic loading. strut Stress Analysis (VA-CR1 54 Rev. C) 1,09112 Dui 'MA EFTA00277778 .1 EFTA00277779 8- 3-99 4:55 PM ;SUPER 27 PROGRAM 6196912232;# 6/ 8 DODE1 BY B. COX DATE 08/02/99 El= PAGE 2 of 4 CHK'D ERDS Cl 036 DATE ROHR TITLE Skin Disband VA545300-1 ROHR, INC. Use or disclosure of this information is suhicet to the restriction on the title page or on the first page oruris document The noted adhesive primer is compatible with the adhesive as shown in the excerpt of MIL-HDBK-337 at the end of this analysis. Conservatively assume all the aerodynamic load is reacted by a 1.0-Inch wide by 30 inches long beam that is simply supported between the fuselage and outboard edge. The core shear stress (f6) is expressed by = V / hb where V is the vertical load being reacted at the supported end h is the centroid distance of the sandwich panel h = t/2 + to/2 b is the beam width From page 10.7 of Reference ', the aerodynamic pressure (P) on the aft fairing Is .5 psi limit (.75 psi ult). Therefore the ultimate vertical load at one end of a simply supported beam is V = .75(30)(1.0)/2 = 11.25 lbs (ult). From VA545300, = .016, t. = .032 and t, = .30. h = .016/2 + .03212 + .30 = .324 in - = V hb = 11.25 / .324(1.0) = 34.7 lbs/in2 From the certification sheet shown at the end of this analysis, the allowable lap shear for the FM 73 adhesive is 6,523 psi at 75° F. Since there is no test data readily available for this adhesive system for core bond, e comparison of this adhesive system will be made to EA9649R (RMS 058). From figure 3.3.2 of Reference 2, aluminum core and face sheet with EA9649R adhesive has an allowable of 220 psi for the BP core configuration. Since the lap shear for the repair adhesive is significantly higher than EA9649R (2,838 psi at 75° F), it is reasonable to assume that 34.7 psi core shear Is acceptable for this adhesive system. The repair at the aft end of the fairing is acceptable by inspection since the aerodynam ic load is very little to nil at this location. IV.. Fatigue Analysis: Repair is acceptable for fatigue strength by inspection since the ultimate marg in is high and there are no additional stress concentrations compared to the type design. 2 MecheiniU:11 Design Allowables (RHR 85-013) frnreqvo 1-46A- EFTA00277780 • • A • 4 • EFTA00277781 8- 3-99 4:55 PM ;SUPER 27 PROGRAM 6196912232;# 7/ 8 DODD BY B. COX DATE 08/02/99 CIODO PAGE 3 of 4 CHK'D EROS C1036 DATE ROHR TITLE Skin Distxind VA545300-1 ROHR, INC Usc or disclosure of this information -3 subject to Me ie ti Iction on the title page or on the first page of this do:mai/sot ktEleliD331C-337 1 DEsosnlbe.r 1982 . e e t 4•- t I R i t —6 A- i! i l 1 i1 I Pi ti It iti. P ac i V I-- la in (. II i5 V 4 . la t, i t 111 3 g . --zi ti CC77 5 11 t •t m 0g Cs 5 1 l! g S I l 4 Q g cS a _ , m r av I- - ,m . 14— li s tit iii E 6 c% 6 :frt. 0 Set • A r§ E u. VIE IL . LL LL rig g I b . ag DS • _ = > i' -g = .2 I 1 .g " S. -1 i E• 4-4 1%7/1 Ilredi EFTA00277782 • • EFTA00277783 8- 3-99 4:55 PM ;SUPER 27 PROGRAM 5198912232;# 8/ 8 -k DODO BY B. COX DATE 08/02/99 DODO PAGE 4 of 4 CHK'D ERDS C1036 DATE ROHR TITLE Skin Disband VA545300-1 ROHR, INC. Use or dIscIosure Of this Intbrinalion Is subject to the restriction on the title page or on tho first paio of this document CytliCFADAE1 ISICIFirstitowl swat Kowa to 0nu*. kfarSAM2107 /3 CSR irrrICAT ON . sow VIMCO-LARM CITY TO PA O. BOK 1909 LAM criry PL. 32066 GRIP VIW2O-1M34 arrl TOEIC;iway 30 EAST • gizaxxnx. Mime= 2cluTE 19. BOX 1029 OUR 'OMER IA= CITY • 0023439/001 PT* 32025 WinOWNt turrg 5111sSzo OR131&R 598376 06/17/99 Br* BATaijOrriT B EtsweltjuzysT wait • taBeiBit =Km= mAntwacTaRBD =maw UM 2742-13037 aum.13,1$)9 500.00 DP * 2742 TOTAL 1* taTeR OTY so0.00 t TEL - TOTAL OT? 500.00 Tas atinTrzse THE sumotrara AT Trbas op EIBIPMENT OONFORK0 TU ALEIFEXCIUMIK rtalaNGS AWD spEciFiCATIOVS NOT= =WC SpEteris ratriarg: 1244-A-132 RSV B, TW(-2 TM x =Ms 2 POEM P GROUP 3 llama 21.O8392VS OR FRU= legrra ACCIPTANCe Bi2 PART or TIM Num 3tragensint rYtngst_ unri ARK ORGY TO metuow WXTR ThZ marumcgo AnCE0strva oapkvAER To Imam caRTnnemoN. saa CSC FOR AM 2 ism ASsZ81 7Was, * TzsT DA A 75 P LAP MAR 180 6584. 5552, 61044 6522, 6122 PEI 453U, 437B, 405.5# 4368, 45t5 PSX winGtilrr 061, .01, .061 FISF 8 /£ a:ZUMeggrg tinDOVd Lz Nef 5S;'e 6B-r -g rormywn t3I1L3 EFTA00277784 A ..t... al.• • 3 ••• I. S. EFTA00277785 .ra to I Work Order 43736. , • : i, , ,. !Form Approved MAJOR REPAIR AND ALTERATION iv L.,: c OMB No. 2120-0020 US Department of Transportation (Airframe, Powerplant, Propeller or Appliance) - ." • 7- For FAA Use Only - Federal Aviation Office Id ntification Administration . ir.07 ' • '; • r" 4 • . INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, 'and AC,43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failu re to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make • -. - Model • • . ' Boeing .ri :-..,;!• =- ', ., , :: 1 . ,...; :11-". 1:1V., ' . ',.. 727-31 ' ''' i • ; • 1 , v 1 1. Aircraft - Serial No. " S. , • •:. • • Nationality and Registration Mark ,. •• •. 20115 .N505LS Name (As shown on registration certificate) I Address (As shown on registration certificate) . ' '; • i • • .. • • 4 • • — •• 2. Owner Northwest Delawa.re Corporation 1105 N Market St . . . 1 ' Wilmington, DE 19899 : ' ,. .. 3. For FAA Use Only 'The data identified herein complies with the applicable airworthines s requirements and is approved only for the above described aircr aft, ,,,, , , .. subject to conformity inspection by a person authorized in FAR 43, • se Lion ' 43.7 . : ., . . ../ 2 z _Zieee . . .i •i GL-CMH FSDO. , ate i attire of FAA Ins ecter esus Zubia • Unit Identification •• 5. Type Unit Make ,. „ .• . Model • Serial No. ' • . •• l. Repair Alteration • - • .• AIRFRAME • (As described n item 1 above) , • , ., 1 • 'v• . • % , ". ..... .;• i ,:, •I ,li -, r -: r •:•1• I.•,• ::. . i • ,: . • ••• • ' . .• X . , , 4 • 1 • .••• • . . a. ••• • • -. POWERPLANT • • •. , it i •i • . . ••• .0. " 1. • .1 • :6 • •'' +'•;i•..••. • . ' " t I • • s . I . ' ' . 5 .,. •• . ZI ‘, 4 )4" .g • '•`.. PROPELLER I ' .' i let; •qtr. ••• . :1 • .:" ‘:' • I S . ' • ••••rvzr;• ;* ' : !I' Type - ' • •,, . . .- APPLIANCE Manufacturer • I' - • 6. Conformity Statement ' A. Agency's Name and Address . B. Kind of Agency ElectroSonics C. Certificate No. . . „ . ... U. S. Cert ifica ted Mechanic Repair Station AEIR005K, 4391 International Gateway Foreign Certificated Mechanic Radio Class 1,2 & 3; Instrument Port Columbus International Airport X Certificated Repair Station Columbus, OHIO 43219 Class 3, Accessory Class 3 Manufacturer Limited Altimeter D. I certify that the repair and/or alteration made to the unit( s) identified in item 4 above and described on the been made in accordance with the requirements of Part reverse or attachments hereto have 43 of the U. S. Federal Aviation Regulations and that is true and correct to the best of my knowledge. the information furnished herein Date ' Signature of Authorized Indiv• -- _, -• • . - - _ . ., _ April 28, 1999 1 . • • '• ' • • i ..,. ;; , •t . • . r I t • ' - 7. Appro al Ret Service i •-. • • t Pursuant to the authority given persons specified below, ' - •. th Oriitlid fie in item 4 was inspected in the manner Administrator of the Federal Aviation Administration and is. prescribed by the Q APPROVED 0 REJECTED ; ', ..- ! 1 FAA Flt Standards 0%,......"• O. inspector Man ufac ture r Inspection Authorization Othe r (Spe cify) .: A'Irt‘''..V •. ...N. BY 1- 1 ' ; ' FAA Designee X Repair Station Person Approved by Transport ,— . Canada Airworthiness Group ! '1 '1. I . Date of Approval or Rejection Certificate or Signature of Authorized Ind* d al I Designation No. . • 1 : 4 s al -iI AE1R0 , 05K i _ ..... 0 • --- - --- • • Q8) EFTA00277786 NOTICE Weight and balance or operating limitation changes shall besentered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. • 8. Description of Work Accomplished (if more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKE/MODEL/DESCRIPTION STATION 622-7293-101 3 Collins VHF-422b Comm C37c, C38c 450.0 2. The following equipment was installed in the aircraft. • ,j= INSTALLATION PART NUMBER QTY MAKE/MODEL/DESCRIPTION ISO STATION DATA • 822-1115-001 3 Collins VHF-422c Comm C37c, C38c 450.0 523-0772719 3. The above work was accomplished IAW FAA Advi'sory Circular AC 43.13-1B, Chapter 11,12 and AC 43.13-2A, Chapters 1, 2. 4. This work has been accomplished under ElectroSonics Work Order 43736. 5. Removed existing Collins VHF-422b corn's to accomplish 8.33Khz modifications Collins S.B.17. Following modification, reinstalled as VHF-422c and performed a complete operational check. 6. A complete test of the installation of the modified units has been conducted to confirm that other aircraft systems are free of interference as a result of this installation. All tests found to be satisfactory. 7. Collins does not specify any new continued airworthiness instructions for the above equipment. The owner/operator should consult the Boeing maintenance manuals for general avionics continued airworthiness requirements. 8. The owner/operator must comply with manufacturer's maintenance instructions to ensure continued airworthiness any time the above equipment is removed and/or repaired and reinstalled. 9. The aircraft Weight and Balance is unchanged and Equipment List has been amended. 10. The aircraft must be loaded IAW the prescribed loading information from the manufacturer. END • 0-1 ■ ;,'-1 C2 S-A S-0 C-1 C-2 A-1 ■ S-A S-0 C-1 C-2 A-1 0-1 0-2 , . A-2 Ss-,..-,Eivro .A-3 - 0-3 . ... SITFIVED 0-4 • •• , 05 " '''/A ' — 3 1999 . A5 ,; 0-6 A CM FSDO- COI LIMMIS OH •- FSDO Col IMBOS. OH 0-7 S C-3 C-4 -C-5 A-11 A-10 A;9 A-7 C-3 C-4 C-5 A-11 A-10 A-9 A-7 0-3 Ali ❑ Additional Sheets Are Attached U.S. GPO:1991-0-568-012/40035 EFTA00277787 p.* Work Order 43736. . - • . • ; . .,, Form Approved . t MAJOR REPAIR AND ALTERATION ' ' ' '''••i - ' • OMB No. 2120-0020 • . ',I • :. US Dopartmant of (Airframe, Power plant, Propeller or Appliance) l•••'''' ,, -- - • ' • • For FAA Use Only Transportation ._ . Federal Aviation 5.. , . .-,..- . . . - , .. ,..*:.,,,.•••,-- Office Identification Administration Lk,: • QL - - ' GL0 7 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). ' • - , -, ' - . , 5, , • -, • • • Make Model .,i 1' 1P -ti :.?:; , , Boeing - - ' 727-31 1. Aircraft Serial No. Nationality and Registration Mark ; 20115 • i ,, ' - N505LS Name (As shown on registration certificate) .. Address (As shown on registration certificate) • .* Northwest Delaw , Corporation . , , are „1105 N Market St 2. Owner * • - . :t., • 1 . Wilmington, DE 19899 . - '• 3. For FAA Use Only • 1 ,; . 'The data identified herein complies with the applicable airworthiness , . . requirements and is approved only for the above described aircraft, ,•.• ,- . 7 , -.., 7; • . , subject to conformity inspection by a person authorized in FAR 43, section . 43.7 / , .::**,'; I. • • I 24' 77 —,,(//g" GL-CMH FSDO Date . ..4 tr ' nature of FAA I sp , Jesus Zubia I- ' "." ' 4. Unit Identification 5. Type , ,I.,, , " r - i ' • ''',.'4, . . .t, :. .;r:::. - Unit Make , - Model , .Serial No. , Repair Alteration AIRFRAME , .. (As described !I!'. Item 1 above),, ,. :;1. .. .,..:i.., t ,..,, , ., , - i t X , POWERPLANT • ,,. 1! 5, --- •1 J.,, it* ' ‘ ' 't I . • I • 1 t s • , ' • 1, • ' r...1 ' • .; .' • . 1:1 . PROPELLER Type , , . , . . •. • -, 1,, • APPLIANCE ., Manufacturer ' .• . , , I ' 6. Conformity Statement A. Agency's Name and Address, ••" B. Kind of Agency . . " — ' i • ' C. Certificate No. • '' ' ElectroSonics U. S. Certificated Mechanic Repair Station AE1R005K , 4391 International Gateway Foreign Certificated Mechanic Radio Class 1,2 & 3; Instrument Port Columbus International Airport X Certificated Repair Station Class 3, Accessory Class 3 Columbus, OHIO 43219 Manufacturer Limited Altimeter D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and describe d on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U. S. Federal Aviation Regulat ions and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Au orized Indivi i , I ...., ....... , ..• -• April 28, '1999 i .e-- i , , , , i ) 17..., i , f . 7. Approval or turn o rvice - - Pursuant to the authority given persons specified below, the unit identi in tern 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is •./ APPROVED ❑ REJELILI) . r FAA Flt Standards •, t q.?1 •I --..: C Manufacturer Inspection Authorization Other (Specify) Inspector BY 1...:- t. • -• i • v .i •. FAA Designee X Repair Station Person Approve d by Transpo rt Canada Airworthiness Group I Date of Approval or Rejection Certificate or Signa r of Authorized idual ; . , Designation No. • - i t - ).i -19 AE1R005K . FAA Form 337 (12-88) EFTA00277788 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. Ss, 8. Description of Work Accomplished (if more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 1. The following equipment was removed from the aircraft: .71 PART NUMBER QTY MAKE/MODELJDESCRIPTION STATION 622-6520-005 2 Collins CTL-22 200.0 622-6520-005 '1 Collins CTL-22 259.5 2. The following equipment was installed in the aircraft. • ; ' , • PART NUMBER MAKE/MODELIDESCRIPTION •'':: i . r; 4 •• INSTALLATION QTY TSO STATION s .• „ • DATA 822-1120-005 • 2 Collins CTL-22c C37c, C38c 200.0 523-0072719 82271120-.005 1. Collins CTL-22c .1' ' C37c, C38c, , 259.5 • .1.„ „. . , ., 3. The above work was accomplished IAW FAA Advisory Circular AC 43.13-1B, Chapter 11,12 and AC 43.13-2A, Chapters 1, 2. , • • 4. This work has been adcomplished under ElectrOSonics Work Order 43736. 5. Removed existing CTL-22 to accomplish the 8.33KHZ spacing modifications Collins S.B. 31. Following modification, reinstalled units'and performed a complete operational check. 6. A complete test of the installation of the modified units lls been conducted to confirm that other aircraft systems are free of interference as a result of this installation. All tests found to be satisfactory. I t i 7. Collins does not specify any new continued airworthiness instructions for the above equipment. The owner/operat0r shoUld consult the Boeing •mairitenanc4 manuals- for general avionics continued airworthiness requirements. i Ii t 1 i 8. The owner/operator must comply with manufacturer's maintenance instructions to ensure continued ; airworthiness any time the above equipMent is removed and/or repaired and reinstalled. 9. . The aircraft Weight and Balance is unchanged and Equipment List has been amended. , • .r• ,; .., 10. The aircraft must be loaded TAW the prescribed loading information from the manufacturer. END. - •fl" • t It •• ; 0; • '7 ,. •!.C. 0 S-A S-0 C-1 C-2 A-1 0-1 m-i -2 S-A -i.) 6-1 C-2. A-4 •I ' - .. . * A.-2 A-2 0-2 4 1 . -• . crcrivto , r.ZF.CEIVE'D -• JO A-3 0-3 ! 0.3 • :. • , A-4 A50.1-0' 0-4 Al l(281999 , 0_5-- • • • • 1.iiii, ..1.-.3 - A75 ' 0,5 A-5 .t-i•IJ ••. 0-6, 1 'A • L. LL Oh CMH FSDO COLUMBUS. OH • • 'MUSKY' ^ • • CORIM•Bliz C-3 - b=d, c-5 ik:.ii.• ".4-161 i'•9 At7 04 03 , C-3 C-4 C-5 A-11 A-101 A-9 A-7 A-8 ,......___-_, 0-7 ' - 0-8 . • t, . , : tr i • . I • ,-.. .i ,. .1.J.:; , - O Additional Sheets Are Attached U.S, GPO:1991-0-568-012/40035 EFTA00277789 Form Approved OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only of Transportation Office Identification .e.y.f4.4 Federal Aviation Administration 490 ,3- 0 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This form is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Boeing 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 N505LS Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner Northwest Delaware Corp. 1105 N PA S Wilmingtioh; p 93 i 3. For FAA Use Only AUti 1 0 1098 FAA-DILLAS SW05 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME avoraveswer4*~~~0~4•0 (As described in item 1 above) 410010.41~111001~111~~10•4114111 X X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A Agenciis Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated Mechanic TX2R203L Associated Air Center 8201 Lemmon Avenue Foreign Certificated Mechanic Airframe Class 3 & 4 Dallas, Texas 75220 Radio Class 1, 2 & 3 x Certificated Repair Station Manufacturer D. 1 certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual 814/98 >7# 7b4JWA lvd ri' l— 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is F:i APPROVED ❑ REJECTED FAA Flt. Standards Other (Specify) Manufacturer Inspection Authorization Inspector BY FAA Designee x Repair Station Person Approved by Transport Canadian Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 8/4/98 TX2R203L 7-i7, -.49/ti- A- FAA Form 337 (12-88) EFTA00277790 NOTICE alteration must be Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An ments. compatible with all previous alterations to assure continued conformity with the applicable airworthiness require 8. Description of Work Accomplished date work completed.) (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and Aircraft: Boeing 727-31 Aircraft Total Time: 31,675.6 Registration #: N505LS Aircraft Total Cycles: 21,567 Serial #: 20115 August 4, 1998 The following alteration was accomplished at Associated Air Center, Dallas, Texas under Work Order 1565. 1) Mode "S" Transponder ICAO Code Strapping Change in accordance with AAC Drawing 1565-001 Rev A dated July 28, 1998, 8110-3 approved by D.E.R. SW-997, David A. Kimbrell July 29, 1998. The following repair was accomplished at Associated Air Center, Dallas, Texas under Work Order 1565. 1) Repair - L/H Horizontal Stabilizer Trailing Edge Beam at Elevator Station 156 in accordance with AAC Repair Drawing 1565-002 dated July ---, 1998, 8110-3 approved by D.E.R. SW-810, Robert M. Manashi August 4, 1998. El Additional Sheets Are Attached U.S. GOVERNMENT PRINTING OFFICE 1992-769-012/60157 EFTA00277791 DAK-98-089 DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS JULY 29, 1998 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, NAME OF APPUCANT BOEING 727-31 etc.) ASSOCIATED AIR CENTER AIRPLANE DALLAS, TEXAS LIST OF DATA IDENTIFICATION TITLE 1565-001 MODE S TRANSPONDER ICAO CODE STRAPPING CHANGE REV. A 07/28/98 • - -••-•• ,-. .--- - - - --- - - • .- .., NOTES : TC DATA SHEET A3WE. ELECTRICAL DESIGN ASPECTS OF THIS DATA IS APPROVED. THIS APPROVAL APPLICABLE TO B727-31 S/N 20115 ONLY. THIS 8110-3 FORM IS IN SUPPORT OF FAA FORM 337. PURPOSE OF DATA TO SUPPORT THE AVIONICS/ELECTRICAL MODIFICATIONS. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.1301(a)(b)(c) CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets number ed 0 have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. I (0) Therefore n Recommend approval of these data Approve these data ( SI NATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) DAVID A. KIMBRELL SW-997 AVIONICS/ELECTRICAL :f1 ; , SYSTEMS --- :ni FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS Eornont( ( COMPUTER GENERATED) GPO 901-813 EFTA00277792 4 .., t b EFTA00277793 AUG-04-1998 10:39 ASSOC AIR 214 357 2845 214 357 2845 P.O1 (1.3. DEPARTMENT OF TRANSPORTATION DATE #98421 FEDERAL AVIATION ADMINISTRATION AUGUST 04, 1999 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE No.& 'to.. hokopasf. rz) NAME OF APPLICANT BOZ.ZNO 727,-31 AIRPLANE ASSOCIATE) AIR . (N5OOL3) Cwt LIST OF DATA IDE1471 !CATION TITLE ASIOCIATED AIR C/D1TER DRAINO NO. 1565-002 REPAIR - L/ft HORIZONTAL STABILZEER T/E Tipp= REM - ZZXV STA REV . "2R" , 136. DM= O7-29.1933 (SKUT 1, 2 AND 3 07 3) . NOTES: 1. THE STRUCTURAL ASPECTS °NIA or THE ABOVE LISTED DATA X= Abl5A0v2D =Man. Titio NW/WV/Lt. IS TOR TEE IINGINIZZRING D191024 DATA O'NLY. 2. MIS APPROVAL IS VALID armY FOR 8=130 MODEL No. -727-31, AIRcRAPT S/N 2O115 AND Is IssuzD Itt SIMPORT OF A MAJOR =PAIR or THE SUBJECT AIRCRirT. PU - - 468E OF DATA IN SUPPORT or A )0JOR REPAIR ON BONING 14013EL NO. 727-31, AIRCRAFT 3/N 20115. APR_ z REQUIREMENTS pa vials; airasom) CAR 4b.20O (a) , (b) , 4b.201 (a) . (10 . (a) , 4b.202, 4b.3OO, 415.901, db. 302, 413.303, 4b.304 (a) , (b) , 4b-3O6 fa) . 04 , (d) . CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered )0000000(XXXXX00004 have been examined in accordance with establithed pnneadunes and found to COmply with applicable requirements of the Federal Aviation Regulations. 0 Recommend Approval of this data I (W) THEREFORE El Approve these data • Illij=gaityk,uzjite,,AL4,14:rivii-ut'ertl- -v 6ENTATiVE S SIGNATioN NUMBE frY4s 0 .. 0 ek.A Roam — . • •• .. . SW-910 STRUCTURES — • ------ 0 .7Q) aupERSIMesPREvIOUI trirrioN a209314I3 ..J TOTAL P.01 EFTA00277794 4 EFTA00277795 UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATiON STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND 2. MANUFACTURER AND MODEL 3 AIRCRAFT SERIAL 4 CATEGORY REGISTRATION MARKS NUMBER N50SLS BOEING 727.--31 20115 TRANSPORT . 5 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and certifies that. as of the date of issuance. the aircraft to which issued has been inspected and found to conform to the type certificate therefor. to be in condition for safe operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation, except as noted herein. Exceptions: NONE 6 TERMS AND CONDITIONS ,, Unless sooner surrendered. suspended. revoked, or a termination date is otherwise established by the Administrator, this airworthiness certificate is effective as long as the maintenance, preventative maintenance. and alterations are performed in accordance withParts21. 43, and 91 of the Federal Aviation Regulations. as appropriate, and the aircraft is registered in the United States. DATE OF ISSUANCE TATIVE DESIGNATION NUMBER R 07--23-90 t ____. GLO7 Any alteration, reproduction. or misuse oft C itti e may be punishable by a tine not exceeding S1.000. or imprisonment not exceeding 3 years. or both. THIS CERTIFICATE M ST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) * U.S.G.P.O.: 1994-568-762 1 EFTA00277796 EFTA00277797 , .:11, Form Approved omeApre MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, or Appliance) or se my of Transportation Federal Aviation Ifo t LAS / (A/C_ Administration S 'iAJOc INSTRUCTIONS: Print or type all entries See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This form is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Boeing 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 N500LS Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner Northwest Delaware Corp. 1105 N Market St Wilmington, DE 19899 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME . (As described in item "I above) sessesseasseareis X X POWERPLANT PROPELLER Type APPLIANCE Manufacturer - . - 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. -Certificate No.:- • Associated Air Center U.S. Certificated Mechanic 8201 Lemmon Avenue Foreign Certificated Mechanic 7- TX2R203L‘i a • • • Dallas, Texas 75220 Class 3 & 4 x Certificatea Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signatur of Authorized Individual 8/2/97 i 7. Approval for Reyirn Service 4 fr it-7--,- Pursuant to the authority given persons specified below, the unit identified - item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 0 APPROVED ❑ REJECTED FAA Fit. Standards Other (Specify) Manufacturer Inspection Authorization Inspector BY FAA Designee X Repair Station Person Approved by Transport Canadian Airworthiness Group Date of Approval or Rejection Certificate or Signature of uthorized individual Designation No. 8/2/97 TX2R203L .4-169-4-c--- - Orin (12- EFTA00277798 • wo• NOTICE Weight and balance or operating limitation changes shall be entered in the appropriatebleaircraft record. An alteration must be airworthiness requirements. compatible with all previous alterations to assure continued conformity with the applica 8. Description of Work Accomplished n mark and date work completed.) (tf more space is required, attach additional sheets. Identify with aircraft nationality and registratio Aircraft: Boeing: 727-31 Aircraft Total Time:31,471.2 Registration #: N500LS Aircraft Total Cycles: 21,468 Serial #: 20115 August 2, 1997 The following work was accomplished at Associated Air Center, Dallas, Texas under Work Order 1476. 1) Repair - Airstair Door Actuator Attach Clip in accordance with AAC Repair Drawing 1476-001 IR dated July 16, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 2) Repair - #1 & #3 Pylon Corrosion on Forward Engine Mounts in accordance with AAC Repair Drawing 1476-002 IR dated July 17, 1997, 8110-3 approved by D.E.R. SW- 916, Jim Martin July 22, 1997. 3) Repair - #8 Leading Edge Slat Crack at I/B Slat Guide in accordance with AAC Repair Drawing 1476-003 IR dated July 17, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 4) Repair - Corrosion on R/H Wing Upper Surface at WBL 70.5 Between Str. 1-14 in accordance with AAC Repair Drawing 1476-004 IR dated July 21, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 5) Repair - Floor Beam BS 600. RBL 25 Figure 8 Hole in accordance with AAC Repair Drawing 1476-005 IR dated July 22, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 6) Repair - Aft BB Door Interior Structure Cracked in accordance with AAC Repair Drawing 1476-006 IR dated July 22, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 7) Repair - Wing to Body Fairing Damaged Dome Nut in accordance with AAC Repair Drawing 1476-007 IR dated July 25, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 25, 1997. 8) Repair of Center Engine Exhaust Nozzle in accordance with Rohr, Inc. Engineering Repair Data Sheet No. C0625 Rev. A dated July 23, 1007, 8110-3 approved by D.E.R.(s) NM-2731, Jeffrey D. Shutrump for Structures, NM-738, Tony Bradlaugh-Dredge for Powerplant and NM-2182, Michael August for Special Administrative July 23, 1997 and AAC Repair Drawing 1476-008 IR dated July 25, 1997, 8110-3 approved by D.E.R. SW- 916, Jim Martin July 25, 1997. SrAdditional Sheets Are Attached U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 EFTA00277799 EFTA00277800 ****鬓*滿***************崇*帐***兴*台扁盆**幡*%************************* 扒一昌老…3吻O 。’参昱。一＾。呦等参叻·餡·阉·Q 宕「⑩＞。aQ髑MI2 品＾卜③③一＾芻冒一 I-－入內＇卜③曲屆3蚪 Q O< ＜ ￡ 篆 ①◎為「8 ◎◎巛鬲出剑划瀏铡剴国吲刊荆蒯剽唰门回剑唰剧剡浏剑闪蜊~＾° 節冲矬筒N “⑩ 沏＂g熬 卜·2 g －雲昌 · N 場＝~＝< 噪細Q訕 － － N’叫卜矬耆M 釜 扈 占 宸 － 昌 噪 訕 Q訕 ＜ ＜ 一瞩「出g 鬲 晌－－°N 蘧鼋艺①叻 叻闫°。蚋z ＂鞋g 鼍 募 … 锣 盛 一 M ‘ … I 卜g ＂蜘庄－⑩。箇”‘编齟Q齟卜 忍 。 窗N 。 一 la- r EFTA00277801 ARC'91.1 f. U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/22/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-0011-- REPAIR - AIRSTAIR DOOR ACTUATOR ATTACH CLIP REV. IR 7-16-97 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 NSPEC-1-01\ PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition s and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered ,/ V X have been examined in accordance with established procedures and found to comply with applicable requirem ents of the Federal Aviation Regulations. MI Recommend approval of these data I( ) Therefore 171 Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) JIM MARTIN SW-916 STRUCTURES 7: FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277802 s a I EFTA00277803 AAC-110 IS -1 U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/22/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-002 REPAIR - # 1 & # 3 PYLON CORROSION ON FWD ENGINE MOUNTS REV. IR 7-17-97 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSPECTION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrator and In accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered V L7,( oe have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I ) Therefore 71 Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 1.7 . 4.' JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277804 II • • ... EFTA00277805 RPC°1-1. 1SB U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/22/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-003 REPAIR - # 8 UE SLAT CRACK AT 1/B SLAT GUIDE REV. IR 7-17-97 • THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 t°41SPFC1-\°N PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 . .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered Z / pL have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. 1 J Recommend approval of these data I ) Therefore r -- . Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 7- . -7 e/ JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277806 • . • EFTA00277807 AfIC•91,15. U.S. DEPARTMENT OF TRANSPORTATION DATE • FEDERAL AVIATION ADMINISTRATION 7/22/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. -TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-004 L✓ REPAIR CORROSION ON R/H WING UPPER SURFACE AT WBL 70.5 REV. IR 7-21-97 BETWEEN STR. 1 - 14 • THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 iNIS?E_CION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered 0‹. ("<' have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I ) Therefore 71 Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) ,,, JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277808 ..9 • S • • EFTA00277809 Af:IC,.91. ILO U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/22/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-005 (. REPAIR - FLOOR BEAM STA. 600 RBL 25 FIGURE 8 HOLE REV. IR 7-22-97 REPORT NO. 1476-005 c- . STRUCTURAL SUBSTANTIATION - REPAIR - FLOOR BEAM STA. 600 RBL 25 REV. IR 7-22-97 FIGURE 8 HOLE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSpECTION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 • .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered Z 0.., have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. El Recommend approval of these data I ) Therefore ji-i6Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) JIM MARTIN SW-916 STRUCTURES orm (11-70 PERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277810 i, • • EFTA00277811 iL U.S. DEPARTMENT OF TRANSPORTATION DATE . FEDERAL AVIATION ADMINISTRATION 7/22/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-006 `--- REPAIR - AFT B/B DOOR INTERIOR STRUCTURE CRACKED REV. IR 7-22-97 REPORT NO. 1476-006 (V SRUCTURAL SUBSTANTIATION - REPAIR - AFT B/B DOOR INTERIOR REV. IR 7-22-97 STRUCTURE CRACKED THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 IN R P F CT10 N PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered a/ oe have been examined In accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I Therefore 171 Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 7 — e JIM MARTIN SW-916 STRUCTURES • _ FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277812 r • • • EFTA00277813 fiRC>97' U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/25/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-007 ,.- REPAIR - WING TO BODY FAIRING DAMAGED DOME NUT REV. IR 7-25-97 ‘-- THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 \ s ‘ 'OC) s, G PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.300 .304 .305 CERTIFICATION - Under authority vested by direction of the Administrator and In accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered ,24" pZ of have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I 04 Therefore Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 57 ,.,,, JIM MARTIN SW-916 STRUCTURES • FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277814 • • • • EFTA00277815 RAC, crl , ILL . U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/25/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS • AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-008 ( - REPAIR - OUTER SKIN NOZZLE CENTER ENGINE REV. IR 7-25-97 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 JA/Ch L--,(Th ,_, .... PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.300 .304 .305 CERTIFICATION - Under authority vested by direction of the Administrator and In accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered oe 1/ oc- have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I (ye) Therefore i- 1 Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277816 • 0. • EFTA00277817 JWG 97.084 U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION JULY 28, 1997 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Au-plane. Radro. Ilelicopier. etc.) NAME OF APPLICANT Boeing 727 - 100 Airplane Associated Air Center LIST OF DATA IDENTIFICATION TITLE Drawing No. 97 - 2211 - 210 ✓ Autopilot Interface Unit Modification W/D. Rev -- Date: 7/28/97 END Note: (1) The above data is approved for the electrical/ electronic and avionics design aspects only. PURPOSE OF DATA To Support Major Alteration on S/N 20115 Only. APPLICABLE REQUIREMENTS (fist specific sections) FAR 25.869(a), 25.1301, 25.1431(c). CERTIFICATION - Under authority vested by direction of the administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered X X X X X X X X X have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I (326) Therefore x Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) SW - 880 Systems & Equipment // John W. Goswick V orm - EFTA00277818 a • . • •• • EFTA00277819 7-23-27 3:12 PM ;SUPER 27 PROGRAM 5125912232;# 2/ 5 U.B. DEPARTMENT OF TRANGPORTATION DATE FEDERAL AVIATION ADMINISTRATION July 23, 1997 I STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) . NAME OF APPLICANT Boeing 727-31 Airplane Rohr, Inc. LIST OF DATA IDENTIFICATION TITLga------ • Rohr Inc., ERDS C0825 Engineering Repair Data sheet Revision A dated July 23, 1997 INSPEU k • • _.. PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. _____ APPLICABLE REQUIREMENTS (List SpecOo Sections) (1)(3) FAR 25.301 (2)(3) FAR 25.605 (a) (1)(3) FAR 25.303 (2)(3) FAR 25.609 (1)(3) FAR 25.305 (a)(b) ,.. CERTIFICATION — Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 153 of the Federal Aviation Regulations, aata listed above and on attached sheets numbered NONE have been examined In accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I (We) Therefore Approve these data 8iGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVES DESIGNATION NUMSER(S) CLASSIFICATION(S) (1) Jeffrey D. Shutrump e -, ,. . NM-2731 Structures v• (2) Tony Bradlaugh-Dredge NM-738 Powerplant _ -t. •-•-‘. (3) Michael August ".Z . NM-2182 Special Administrative --- FAA Form 81104 (11-70) SU RSEDES PREVIOUS EDITION (Computer Generated by Rohr, Inc.) EFTA00277820 • pep 40 EFTA00277821 UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION • STANDARD PiRWORTHINESS CERTIFICATE I NATIONALITY AND 2 MANUFACTURER AND MODEL [ 3 AIRCRAFT SERIAL 4 CATEGORY REGISTRATION MARKS NUMBER N5OOLS BOEING 727-31 20115 TRANSPORT AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and ceatties that. as of the date of issuance. the aircraft to which issued has been inspected and found to conform to the type certificate therefor, to be in condition for safe operation, and has been shown to rp,set the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention oh International Civil Aviation. except as noted herein Exceptions NONE 6 TEAMS AND CONDITIONS Unless sooner surrendered, suspended, revoked. or a termination date is otherwise established by the Administrator, this airworthiness certificate is effective as long as the maintenance. preventative maintenance, and alterations are performed in accordance with Parts 21.43. and 91 of the Federal Aviation Regulations. as appropriate, and the aircr t is registered in the United States 4111. DATE OF ISSUANCE FAA REPRESENTATIVE DESIGNATION NUMBER Replacement) 07-23-90 LEE H. Till GLO7 Any alteration, reproduction, or misuse of this certificate m. a bye froI exceeding S WO, or impnsonrnent not exceeding3 years. or both. THIS CERTIFICATE MUST BE DISPL THE AIRCRAFT IN ACCORDA CE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) GPO 892-804 EFTA00277822 1 5 r .fr a e• ... 4 ili EFTA00277823 . . O - •- Form Approved OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION US Dew titija For FAA Use Only ca-ortp«vmAl - (Airframe, Powerplant, Propeller, or Appliance) ' Office dentification Federal Ariaflon I -P i ----7Z--40 ) u RUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model- BOEING 727—100RE 1. Aircraft Serial No. Nationality and Registration Mark 20115 N500LS - Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner NORTHWEST DELAWARE CORPORATION ggYIA4,DE. 1;899; 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME ....................... (As described in Item 1 above) .................„„,„,..... X • POEFIPLANT PROPELLER Type APPLIANCE Manufacturer • 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. X U.S. Certificated Mechanic THE LIMITED INC. Foreign Certificated Mechanic IA301541619 4387 INTERNATIONAL GATEWAY Certificated Repair Station COLUMBUS, OHIO 43219 Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of Ihe ,. -,Eede rMigion Regulations and that the information furnished herein is true and correct to thei,,beq.of my-knowledge. 1 ;'• !.;e: :I .... i„ .3"L Date ii Signature ze-r 1 divi a • , . March 11, 1998 ' Richard K Cady II 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item wa inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is - t APPROVED O JE' TED FAA Fit. Standards X • her (Specify) Inspector Manufacturer Inspection Authorization FAA Designee Repair Station Person Approved by Transport Cana orthiness Group , Date of Approval or Rejection Certificate or Si natur of thorized I yid:al Designation No. . • - March LI , 1998 IA2185934 ,x-e T .W. RITCHIE FAA Form 337 riz-aa) EFTA00277824 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft compatible with all previous alterations to ass record. An alteration must& ure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach addition al.sheets. Identify with aircraft nationality and registration mark and date work completed.) REMOVED THE FOLLOWING EQUIPTMENT; 2EA. HONEYWELL DIGITAL AIR DATA COMPUTERSP/N 700 070 0--962. INSTALLED THE FOLLOWING EQUIPTMENT: 2 EA. HONEYWELL DIGITAL AIR DATA COMPUTERS P/N 7000700-662 WITH STATIC SOURCE ERROR CORRECTION CURVE INSTALLED IN ACC ORDANCE WITH AES DRAWING ,LIST NO. 97-727-500 REV. B, DATED NOVEMBER 3, 1997 PER SUPPLEMENTAL TYPE CERTIFICATE STO9364sc. FAA APPROVED FLIGHT MANUAL SUPPLEMENT, DAT ED OCTOBER 27, 1997 IS REQUIRED AND INSTALLED ON THIS AIRCRAFT. WEIGHT & BALANCE NEGLIBLE. COPY OF STC ST09364SC AND MASTER DRAWING LIST ATTACHED. CONTINUED MAINTENANCE PRACTICES INCLUDED IN THIS PACKAGE. END El Additional Sheets Are Attached *U.S.GPO:1991-0-568-012140035 EFTA00277825 ti THE LIMITED UR0859 RECEIVED . ... U.S /Department Form Apprptypdo c Irina OMB (p 1,01d2-0192196 of Transportation Federal Aviation MAJOR REPAIR AND ALTERATION For FAA Use Only Administration (Airframe, Powerplant, Propeller, or Appliance) CiffirAPPOALLAS INSTRUCTIONS: Print or type all entries. See FAR 43.9 SW05 , FAR 43 Appendix B, and AC 43.9-1 (or subsequent revis for instructions and disposition of this form. This report is requ ion thereof) ired by law (49 U.S.C. 1421). Failure to report can : result in a civil penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model _- ..-.,. Boeing 1. Aircraft 727-31 Serial No. Nationality and Registration Mark 20115 N500LS Name (As shown on registration certificate) Address (As shown on registration certifica 2. Owner te) Northwest Delaware Corp 1105 N. Market St Wilmington, DE 19899 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME —---— ----- — --------------------(As described in item 1 above)--- ------ --- PRATT & WHITNEY POWERPLANT Turbo Fan Engine JT8D-7B P654373 X PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated Mechanic Greenwich Air Services - Texas, LP Foreign Certificated Mechanic 9311 Reeves Street RAI R445K .. X Certificated Repair Station Powerplant Class 3 Dallas, Texas 75235 Manufacturer Accessory Class 1,2 and 3 D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described have been made in accordance with the requirements on the reverse or attachments hereto of Part 43 of the U.S. Federal Aviation Regulations furnished herein is true and correct to the best of my know and that the information ledge. Date Sign e f Authorized Individual /0 r 3 O --n 7. Approval r Return To Service , Pursuant to the authority given persons specified bel w, the unit identified in item 4 was inspected in the prescribed by the Administrator of the Federal Aviation Adm manner inistration and is _ X APPROVED [1 REJECTED FAA Flt. Standards Other (specify) Manufacturer Inspection Authorization inspector BY • Person Approved by Transport FAA Designee x Repair Station Canada Airworthiness Group Date of Approval or Rejection Certificate or Signa f Authorized In ividual Designation No. / or _3 O - 9 4 RAI R445K f-AA Form 337 (12.88) EFTA00277826 EFTA00277827 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Engine S/N P654373 was removed due to "SERVICE BULLETIN COMPLIANCE." • Engine was disasembled, inspected, repaired as required in accordance with Pratt & Whitney JT8D Engine Manual (P/N 481672), and Greenwich Specialized Unit Repair Workscope which are data approved by the Administrator. Inspected/reinstalled Combustion Chamber Outer Case P/N 542155, S/N 243, T.T. & T.C. Unknown, in accordance with P&W Alert S/B 6228, Part I and Part II and AD's 87-11-07 & 95-08-15. Ps4/Drain bosses require reinspection within 6000 cycles and at each Engine shop visit. Rear flange requires reinspection within . 12000 cycles and at each Engine shop visit. Case meets inspection requirements of Part III of P&W ASB 6228. Continue timed combustion chambers. Complied with P&W Alert S/B 5729R2 and AD 87-14-01R1; immersion ultrasonic inspect C2 fan blades. Complied with P&W Alert 6038R5 and AD 94-20-01; corrosion inspect high pressure compressor disks. Complied with Pratt & Whitney Alert S/B 6196R5; #5 bearing seal assembly. Improved oil return & compartment sealing configuration. Complied with P&W Alert S/B 6110 and Alert S/B 6131, AD 94-20-08. This terminates -reinspection requirements for P&W Alert S/B 5913R6, AD 93-06-05. Engine was preserved forshort term storage IAW Pratt & Whitney JTSD Engine Manual (P/N 481672). Engine was subjected to a test run; a post-test borescope inspection was performed and Engine was accepted as serviceable. Engine TT: 32939.0, TC: 22557, TSR 00:00 CSR 0000. Pertinent details of this repair are on file at this Agency under W.O. UR0859 fl ADDITIONAL SHEETS ARE ATTACHED FAA AC 72-4906 Form Approved 0 . MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 uSDeporrpent atralwavarxxl (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Filderolita*Mms Office Identification Aderinharoftn a_FSDO-09 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Boeing B727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 N500LS • Name (As shown on registration certificate) Address (As shown on registration certificate) Northwest Delaware Corporation 1105 N. Market Street 2. Owner Wilmington, DE 19899 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME ......................".......; (As described in Item 1 above) ...............~............~........" X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. ST Mobile Aerospace Engineering, Inc. U.S. Certificated Mechanic 2100 9th. Street, Brookley Complex Certificated Mechanic MZAR013L Foreign Mobile, AL 36615 Certificated Repair Station Limited Airframe X Manufacturer D. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulat ions and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individ November 25, 1995 Clarence Spencer .r....---- e • 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is NI APPROVED D REJECTED FAA Flt. Standards Other (Specify) Inspector Manufacturer inspection Authorization BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. November 25, 1995 MZAR013L Christopher J. Hil FAA Form 337 (12.88) EFTA00277828 NOTICE Weight and balance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration rAust be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Installed DeVore Aviation Corporation tail flood light installation in engine pylons in accordance with De Vore STC ST09113AC dated 26 May 95. DeVore Top Drawing List #72700003DL Rev "A" dated 5-30-95. Installed Valsan Winglet Modification in Accordance with Valsan Master Drawing List #VA000007, Rev uN" dated 17 April 1995. STC SA5938NM. Aircraft Inboard and Outboard Aft Flaps and Ailerons rigged to endure functionality and conformity. Aircraft weighed after modification. Weight and balance data provided to customer. Aircraft total time = 31,197 hours. Total cycles = 21,345. END ❑ Additional Sheets Are Attached *U.S.GPO:1990-0-588-012/40004 EFTA00277829 FAA AIRCRAFT REGISTRY CAMERA N0. 3 DATE: die/ fr Se— •••• •14fiS • ••: • •-2. ; • • 9.: m.44. • ;• 4.4. .4 • •4444.4•444 of Fc.rm Approved • • OMB No. 2120-0020 0 MAJOR REPAIR AND ALTERATION uSOtowirrwre For FAA Use Only or laracianomn (Airframe; Powerplant, Propeller, or Appliance) i t5IdenNication _„ 6- 0 7 I said asionse ' isaverawiesies •• . •• INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 03 Appendix B. and AC43.9-1 (or subsequent revision thereof) for instructions E •1:4 «. and disposition of this form. This report is required by law (49 U.S.C:1421). Failure to report can result in a civil penalty not to exceed 51,000 y; : for each such violation (Section 901 Federal Aviation Act of 1958); Make • Model S. aiE7N6- 7.Z7 -- /,‘Z) 1. Aircraft .. . • . . Serial No. ' Nationality and Registr,ation Mark c; o d C . • , N5-6,04.5 : . Name (As shown on iegistratiqn certificate) Address (.4s shown on registration certificate) . ' , . • /vagazder. 44D/4/6 Oieft-P. .. te)..an-k -7435 • a. Owner .. V/(14),(16few ..7)e: /912)5 3. For FAA Use Only • :: . ;I: • f: :. • r . • .• .. _ .• ...::.1 - •&i • ‘ V. '',\ S ce • c •.- 7/.:45:: I. %J.: ... ._ . , , . , .. . ., _ . • .• ••• • • • 4. Unit Identification 5. 'Type ... /•• . Unit • .. . ' ', ••'', Model • - ' Serial No. -• Repair Alteration : . : P :. AIRFRAME _ (As described in Item 1 above) • I -.. • , . POWERPLANT .-......., . r. . . , •- • • '-: ._ - • • .. . . - ' \'. .\• •• -/I:'+IV '..".-'• 'i• 1.•. . - - PROPELLER - • Type i : • 24-s euntgar .' PA) • N APPLIANCE Zia/6 00 - 90c l ; 97405 '-e°3 e i i • Manulpoturer _ b. 6714/ra, (.1,OD. 6-) > l< • 6. 'Conformity Statement ti. . A. Agency's Name and Address . B. Kind of A enc • C. Certificate No. f. U.S Certificated Mechanic • --rief Ziliire3 -fink ..tvc_ , mt. 4. Foreign Certificated Mechanic y3e2 Certificated Repair Station 1 -04...))e S-93tZ . • • Co i_i,f6tri , osielt.o 5132. pi' - Manufacturer D. I certify that the repair and/or alteration made to the un i(s) identified in item 4 above and described on the reverse or attachments'hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my kno -- . --- Date S natur of orized Indivi • . 7/i/9 41 - - ;rt. 7. Approval for Return\o Sonic* ••• • Pu suant to the authority given persons specified below• the Loch identifieo'in item 4 was inspected in the manner prescribed by the ••• Administrator of the Federal Aviation Administration and is APPROVED O REJECTED FAA Ft,. Standards •N . (Specify/ • Inspector Manufacturer Inspection Authorization ' .. BY Person pprov by Transport FAA Designee Repair Station Cana Airwo hives recap • . Date of Approval or Rejection Certilicate or Sig lure of uth t zed Individulther Designation No. . /9/9 (1/ - -. 1.14-a ,acci-w , FAA Fors 337 Ia.'s) • 4. 1 • • • : if . •• • • • ri eft • 4 •i• 4 :••• .1, •.‘ •4 .1 • ,• airman ail2Si • • . onor a,. soiwarr•Iina.se,,,,,,iggilia 16* t il t ' 4 Ofifigam • ffs EFTA00277830 • j Weight andbalance or operating limitation changes shallbe enteredin the appropriate aircraft record. An alterationmustbe compatible with all previous alterations to assure continued conformity with t Description of Work Accomplished the applicable airworthiness requirements.. (If more space is required, attach additiOnal sheets. Identify with aircraft nationality and registration mark and date work completed.) NOTICE .I••• /: .......i • . ... ••. • • •...• I ' . • •• -e. of. .!•1 • . . I i • • neile ... aPee,47›,e-z• To 4 -71v Vo66o/0.-' 4964 . (fien).- a.) "By •,xletreAcrearver , Nits/ere-a_ . sla 41°660/6 - 34i ertir&041-67) AI> 9st - o/-041 4.-.. npic.c#&,_ 4(4.49-7eme,A./ ..cs 2),Exa-ivr. :...._. ,.Sy nrit /6Z-I 3(60 oPetkriernhild/ 04?"-e--20 eloo.Zo/D adNeo. TevZ .?4,-75,> c-1- 41sie • 4),/,c hi- Vi Er •AV 4-eargrAig ,ec- ve6-.•idg rE73/ 2,4-.4) • ..?,00-6.edsoht , air ,49.14P 90-a -oV Afro. 39 -- 878Lr .. -6,zagot - 23(?)..,-erbe -7116- Aril &Al AZ • v3771 V,Lti - e c.c% • 74)40ee,oi_der-77A.?6-. a- am/ of s stn. AD. 4;;,/ riierwr /111-Ahnot -Warsqc re" 477-Xedieb riehtf- lerre;- ,c krfirlerc-zdue,. <ale Affigenak_ Av MeroAr oc , .. ......; L• . __J .:. , -:... :. • .: • -. --- 'i . . .. - I. "‘ b14•• .lain til'ArtemoD :t . ... • - I J.4.10. i'••:.! . x•,•nk;ilh 1G hill?' c ' - . ee•Yd.rd: bi 4 • --.. 831•1,. r• • .." • •— -••• • -•• • Oint,n;T: • "Yanlei, ;;• ;01.•• • f-mt...o'R • "''• CV C. CA NC., rc...1‘J • • -• now • , • • . • -• • . r- • el r Itei P.,:i .-; :fle ;".:::; 410 to•lovin erlInlibm1I14: 4i.4150r. -•••. " ,..:.1..! •- 4:1•..! 4 ki 14e.itil.:;L: td.(E).1i.loeti.tol SbsIn (*ifZ.1'31 ' GIO‘tine• itbiitt ro.t,iF. , • :. nc,14:71iC-;:i. Mit :KM brilt 4....41.-.461:4;•.r.:11•' ,IlbivA ;it i•,•;•, : it 1.I.;.;-•Ilo a')'iL'•13.11•17in.4telsiitiro!,•• -pt;1 milt . • b'...nnelysi...i.a epi store r• $ r ; g.,.. • , • ' . i .: &'.... :/ it \b '1 t 0 JZ6d.erif ci! Jr.:alio.; t)4:::. ,:... d zi nir.brv.' 1 • • - • • ............... • ..%•• . ...... m• ••••••• d.;,.•• . '''' ' : '"•••• • J., • ..m.....m. •••• A.. I:Mi. . • . ••• • =4 .. . . . • ... I i'a iV i tit il 46 ‘`: i i c ' ; . P. 4t 1- g ?tc l‘ i) ; 14.: ; 7. i • I . k • . . • • . •. • •' " raiviDE2O.T.ot; i.: ' • *:•••! 4, . • • • • • c.r!S vc! tiC•dittiz 1(1,1r.ittittrii ,i:tirill Loitz;ttitril otiw 1%. ratili rii !...:•Iiiii,; ,i., Si: : t i. 1.'.. .... ‘.••1:.ki.t.soli:•••.)cli e:norisr;, • .)*'1, :! vinc...0.;44P., Urn Vi. I714;,::‘• "•;..• •.. I) rti3lan t.1 • (tvtior,:t...:-..,•'? ,.i i.,:tt Ii0;10:1041,:t,.;11::- nc•it,.:-.6•A ;•7•.p.i..i.:k.",t•IA.10 mlitt!imiltsn. ' . v ._ ...... (X‘V.11::.1?. iVil:51 . . - . - r . . . • . . I. . . . • ;;.... tt 1: : : !. i < 71'.: L.... 5. t t; i :•:• -• . : , itglli!:10".:,..1,0a •: 2.*'.11•‘triate- 107• 4344,,,i1.rAZI . 1 . •. • l '• • • • • — . : i'diti:dir.47 yd b loi.;';i lc:521.)g! • :- - - • • ' .. . Mdiehriv3r4in lowilm is.e4.9.•,.. , • . fIC;Irlc. lif191............ i...:-. ..‘Octize!..• A Al ..._.... • ...•+...•.••••..... • ea .. aft ••••••••••••. .• ' ••••.••••=••••••••••1 •••••••••dmmini• •••.... ir••••• •••••• •••11,•••••••,.. ••• : , ••••••••7 .7 ...... , ... • • • • itii iivitini . bt..1=0,4 lo 0,Lpap.. eta 1 . - ..,t incl.,01D, . ritri)34,40,y., •:....,vzi.V, , A t. i , •i . i•i • . • ...0.,110,. .1..,7.,• ,,r1.:Et...?-, \-,-:-O kddillo I ShilailicA6 Atiecheid .0';•Cr-')Ot •cL,:..477;:. • • :, :. • s,- ;,.:..•. .:, . • " • ... "I: • • 'a' •• • jti •fat, • • I a' • EFTA00277831 FAA AIRCRAFT REGISTRY CAMERA NO. ,3 DATE: -41e/Ife/fY USDemamment TRANSPORT AIRPLANE DIRECTORATE ottranSpa-tation i AIRCRAFT CERTIFICATION SERVICE • C ; LOSJANGELES AIRCRAFT CERTIFICATION OFFI o • Federal Aviation (,. (3229 EAST SPRING STREET %."7.-:•4- AdotinistratiaA • / LONG BEACH, CALIFORNIA 90806-242S VAR CI 144 Honeywell inc. Air Transport Systems Division ATTN: Mr. F. W. (Bill) Lynch 21111 North 19th Avenue 7, • Phoenix, Arizona 85027 References: a) Honeywell letter, dated Feruary 17, 1994 b) Honeywell letter, dated March 1, 1994 Dear Mr. Lynch: Compliance " ' Approval of an Alternate Means of , our review of the data submitted fp response to your letter of March 1, 1994 fivsupport of a proposed alternate means .of compliance with paragraph C. of AD II part No. 4066010-901, -90R 94-01-04 regarding Conversion of Honeywell TCAS G), has been completed. and -903 (Any Mod) to part No. 4066010-904 (Mos revised Service Sullitin We concur that method and procedures outlined in yourprovides an acceptable 1994 4066010-34-SW16 Revision 1, dated February 17, 1-04 Docket No. 93- of AD 94-0 level of safety in accordance with paragraph C. NM-68-AD; Amendment 39-8786. If there are any further question, please contact Mr. Abby Malmir at (310) 988-5351. Sincerely, ,‘ r"— -w.-c, • 7-/f Alan T. Shinseki Manager, Systems and Equipment Branch Lt.?: • , .• 4. • F.-; 1 tt • .4, a_ ‘.. --ze;&,,,„6.smru.lua _s=2 t • EFTA00277832 •MAKT:2131115; ;;„.(4(.1114 110124AST 33114W. ?./.1 TIARanZA,. ria3Dre)Ctritni "i'40 PPIT ;:•INI.751"A • .2.:1317T4A. .• 1'. 47Utr; °Muni! moitctiyA , tatt. . • 4.1 -•• tr;nriTtz:nia.;:.71.. •• Aflinirrlie3-:4(jkls ¢. :iii. I f r. •C tr-H IQ ( iS) .1. . •7;4 ;1.110;4 111.1f: •t.Stfija .r.nosNA :;'-;Co'3110;:i• f ••••vivetno!f ;I T. r ±rib • •.• t ioa t r• I ; V:• • •j:• ;. 0 i2 •• C• ••'• -ray • 0`;) s..1100::f. • • TV.4q •t • AO gr 5:00 a tau?-Of0600:2W4 11::4N.3ro10 6 :golzssiVriorpiiii)21-415.1 ry thri/cOla0 M/Vie-.0103Y214;;69-,,V7Ap cOM. - 3f.lsifun • . • -iec v . !mg Fiu6. ztriu.i.tboini•Ina. Itorifee,pr ;$35:30v.../31- ; M0rfIce.):::)c, ;10tio(J.j10--!.4.7-411i) Olt, 1.15 ,‘.1 •dirriEti-NrAz aiNz-fsc-oluaboA, 'i.:}•zi's.;v1 71' • f. • • .. ft Ottieit* •'i$ 4-8a4;;;: ti •••••1 '" • • zfff.:15 .2.v.2 *i.ert,;%tr,;. EFTA00277833 FAA AIRCRAFT REGISTRY I CAMERA NO. 3 DATE: y1/4y/f5— • •' •, • • • • • eN1 I It/ •/. • • .• . • • ' grakehigko& . • ,• . . • 't • • •- . , . • • , .• • . .• •• . • • t :••••••• 1.1. .. • '-'•• • • • • . • ' ..1 AIRWORTHINESS DIRECTiVE U.S. Depastrberd FUGHT STANDARDS SERVICE of Transpottation ;: 4 REGULATORY SUPPORT OMSION • . • . •, Federal Aviation • P.O. BOX 26460 Administration OICLAHOMA a-ne, OKLAHOMA 73125-0460 ; " ' ' flecsiodoaa east a *Plan a skint Th• Icameno te....,en••• Cara Sued by ea Fa A.td.r asatinieteent Si esimmes eel the eieplise• et reimnd sCs sod SO Picamlbale gnat fora losallcOm areka Yom •••• as " air " . ioulloos you Nonni' •441•Ianal Asinswrearts Pao a _it. "sal d ..'" Ilinseraren 01realre ••••••••S M Alrailla Oat* sp apasame •••••caml RS re p.•. , wary tarn Si sistrellIntioli •...bomet 3•1.4. . .4/ 04-01-04 HONEYWELL: Amendment 39-87843. Docket 93-NM-68-AD. ?•:' computer units; part Applicability: Traffic Alert and Collision Avoidance System (TCAS) II following almlancs. numbers 4066010-901, -902. and -903; as installed on. but not hatted to, the certificated in any category: A340 'scales Airbus Industrie Model A300-4300. A310-200. A310-300. A320-200. and airplanes: 747-100. -200. Boeing Model .727-100 and -200: 737-100. -200. -300. -400. and -500: -300. -400 and 747SP; 757-200; and 767-200 and -300 series airplanes: s' Citation III and. VII 1 • Cessna Citation Model C550 and C560 series airplanes. and Cessna series airplanes: Canadair Challenger Model CL-600-2B16 and -2Al2 series airplanes: iJ I British Aerospace Model 125-800A: Gulf:stream Model Gil, GLIB. GIII. and GIV series airplanes- • -1 2.0"4, Lockheed Model L-1011 series airplanes; and -444;It s McDonnell Douglas Model DC-9-10, -20, -30-, -40, and -50; DC-10-10, -15..30. ,. . MD-11: and DC-9-80 series alrplazics; and Model MD -88 airplanes: . Dassault AV/S.111On Model Mystcre-Falcon 50 and 900 series airplane s; • Short Brothers Model 503-60 series airplanes; „ de Havilland Model DHC-8-100 and DHC-7 series airplanes: ' •Ri • '-; I .011 • Fokker Model F27 series airplanes; and Corporate Jets limited Model BAe 125-800A and EiAc 125-1000A series airplanes. A ra • Compliance: Required as indicated, unless accomplished previously. the TCAS II To prevent collisions or near misses caused by incompatibility between : processors and the current air traffic control system. accomplish the {allowing hs •(aiel) +and (a) Before December 31. 1994, accomplLsh the requirements of paragrap 16. -dated (aX2) of this AD in acconiance with Honctywell Service Bulletin 4066010-34-S* ' December 20, 1993. • (1$ Remove existing Honeywell TCAS U computer units, part numbers incorporate updated 4066010-901, -902, and -903, and replace those units with new units that i, 1 collision avoidance system (CAS) logic, identified as Version 6.04A in Mitre letter F046-L-0069. • dated September 21, 1993. r united r.t. (2) Modify the computer surveillance logic on Honeywell TCAS U compute odate Mode C part numbers 4068010-901, -902, and -903, to ensure that these units accomm coordinated by altitude input of 100-foot Increments and that the system will be tracked and • • Intruding aircraft when the Mode S transponder CA field Ls set at CA.7. tidal? (b) WPrior. to further -after accomplishing the requirements- of paragrapir (al- of :AFM- SupiiIement by • either .+ AD.—revise the Airplane -. Flight Mniiunl (AIM) ' • paragraph (bXI) or (bX2) of this AD; the aP13ropriate Revise the Normal Procedures Section of the AFM to include • • (1) • this AD, in TCAS operating characteristic relative to the modifications required by paragraph (a) of Certification Office accordance with a method approved by the Manager. Los Angeles Aircraft (ACO). FAA. Transport Airplane Directorate. Or the following! (2) - Revise the Normal Procedures Section of the AIM. to Include this AD. TCAS operating characteristic relative to the modification required by paragraph (a) of This may be accomplished by Inserting a-copy of this AD in the AFM or AFM Supplement::7 • -••! ! - . • • • fr ,': a,. 4 -• • •• • • • 0' • 41 • • I! • •!• • • ' • . 1. e :4i .• et: ,. ere_ 4,4, C • 3 T. . . . • 'Ijk• 4. -0: 41'•;•-• • jsr, k.••;.Att4 7‘.• • EFTA00277834 FAA AIRCRAFT REGISTRY CAMERA NO. 3 DATE: -y/r/i - 2 94:0144 messages am ' • CM) aural ground level (AGL) 'All Resolution Advisory (RA) and Traffic Advisory inhibited at a radio altitude of less than 1.100 feet above less than 900 fed AGL descending.' t of the corap liance time that climbing. and compliance or adjustmen Nianager. Los Angeles Aircraft rtattve method of the (c) An alter safety may be used if approved by Operators shall submit their • acceptable level of Directorate. comments and provides an Transport Airplane Office (AC01. FAA. Avionics. Inspector. who may add Certification Principal through an appropriate FAA requests Los Angeles ACO. • . approved alternative methods of Maruager. existence of then send it to the txtncerning the ACO. NOTE: Information obtained from the Los Angeles 21.199 to this AD. if any. may be accordance with FAR 21.197 and compliance with In a.coomplistux:L Special flight permits may be issued requirements of this AD can be Honeywell (d) whore the accordance with location done in operate the airplane to a and modification shall be This incorporation by reference The replacement 20. 1993. (e) December and 1 CFR 4066010-34-SW16, dated with 5 U.S.C. 5.52(a) Service Bulletin Federal Register in accordance Group, Ar . the Director of eel Commercial 14-light Systems was approved by Honeywell Inc-. Copies may be inspected may be obtained from Arizona asoss. Part 51. Copies Division. P.O. Box 21111. Phoenix. SW., Renton. Washington: at the FAA. Systems Avenue, Street. Transport Airplane Directorate. 1601 [led Certification Office_ 3229 ,East Spring the FAA. Traiasport Directorate. Los Angeles Aircraft 800 North Capitol Street NW.. Transport Airplane Federal Registers California; or at the Office of the • Long Beach. Washington. DC. on February 4. W94. suite 700. This amendment becomes effective (f) . .. INFORMATION CONTACT: ' Transport FOR FURTHER Equipment Branch. AMA-13216. FAA. Street. ErIginCer. Systems and 3229 East Spring Aerospace Certification Office, Abby Nialn Aircraft 988-5210. Los Angeles Airplane Directorate, 90806-2425; 988-5-%51; fax (310) telephone (310) Long Beach. California Flights Date Aircraft Aircraft/APU Hours Gilt GIV GI GII ode No. NOT APPLICABLE COMPLIED WITH • -• - DEFERRED UNTIL,. - E ABOVE ITEM IS DUE ON THE ITEM IS COMPLIED WITH. H. LEASE COMPLETE THIS FORM AND SEND IT IN WHEN •.- • . : 5 t..it1 _ :t ; ::::::15.:ir.ii t'.' I.'111.1: L:,l, .“.• v 1:e'iilii:t2,'.;. Z:5 4.2,,t z .. rnr.. • u: .ti—', 1..1:;.! sc. ', .t.:: :1-.;z:-...'„•7, .i:.ti t:.r: 1. liwez . JSOlil.Diltritt: 1 J)trird f"!. a :1••7••11,. ii:).3 tr:/5?:.) . ,. • tti : ••-oh• +34K .Jr. silt t• ....Lc.), : • • t •., . , •.); • , li f" r. tit 1, cp :341:le 01 troll. :1;g-iFl. Itro: 1 r t; ?7)v; U•1Vi T.: '..1 -... i>ttioft I. ,_A I CA ,;1117):"1 r.Pikr.t.:1"1::!t-strb Mr?. (*--.11,11ae: _101.?1:.0:11X.11.9 • •t: Cr. 'grit 'to vr it .; ;,• matht• tztt 13•;71-.:tqrtr., •. tv: C:Uq• • f. , a -anOnftilwls EFTA00277835 -FAA AIRCRAFT REGISTRY CAMERA NO.i it/ DATE: /0 -1R-94 • ( •••••• ••••• Form Approved OMB No. 2120-0020 r a MAJOR REPAIR AND ALTERATION • us Department For FAA Use Only nr frolsooncmcn . (Airframe, Powerplant, Propeller, or Appliance) riderdAriation ,- (1)ffiC.Alrang.0-15 AdrintenstIon INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 NSOOLS Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner NORTHWEST HOLDING CORP. 1105 N. MARKET STREET WILMINGTON, DE 19899 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X N POWERPLANT • . I. PROPELLER frft tP Type APPLANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated Mechanic PAGE AVJET CORPORATION Foreign Certificated Mechanic 9809 TRADEPORT DRIVE 0S4R425M X Certificated Repair Station ORLANDO, FLORIDA 32827 Manufacturer •1 it D. I certify that the repair and/or alteration made to the un't(s) identified in item 4 above and described_on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S Federal Avia egulati and t information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Indi dual t2. 056-4-17 /996/- 7. Approval for Return To Service • .7! Pt. suer: to the authority given persons specified below, the unit identified in item 4 was' inspected in the manner prescribed by the F. ..rnrhistrator of the Federal Aviation Administration and is at APPROVED O REJECTED 1 Other (Specify) FAA Flt. Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Canada Ai rthiness Group . Date of Ap royal o Refection Certificate or Signatur Aril Authorized ivid Designatior• No. / 9 Ii-r/ CO Affte/ 709,1) g 0S4R425M Ati ti . ...t-C4-7.---7.-. 2 -4 FAA 'Form 3 1t2.88) A • ttii4Ty • No ......Viecte •PC "rot. e l :ki t 14;: a aA11 1 Aff:1,,a , Ina Or - ;et.•. , • EFTA00277836 NOTICE be Weight and balance or operating limitation changes shallbe enteredin the appropriate aircraftrecord. An alteration must nts. compatible with all previous alterations,to assure continued conformity with the applicable airworthiness requiteme • 8. Description of Work Accomplished . (If more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed:) . . . 1. INSTALLED A DORNE & MARGOLIN EMERGENCY LOCATION TRANSMITTER (ELT) SYSTEM IN ACCORDANCE WITH PAGE AVJET REPORT PR -91-22 REV. A, DATED 8/15/94 AND MDL- 91-02 REV. B, DATED 8/10/94 AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339, DATED AUGUST 16, 1994.. PROVIDED WEIGHT & BALANCE UPDATE. EQUIPMENT LIST UPDATED ACCORDINGLY. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OTHER SYSTEMS. STATION ALL PERTINET DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR 0S4R425M UNDER WORK ORDER 60298, DATED SEPTEMBER 2, 1994. . . .. . . . .. ••• ;:ot ; •• . .1 :1; • • EFTA00277837 -FAA AIRCRAFT REGISTRY CAMERA N0.3k DATE: /0-/a- *L____ Form Approved OMB No. 2120-0020 4".• MAJOR REPAIR AND ALTERATION For FAA Use Only wspepartnem . of Tronspc- - or . (Airframe, Powerptant, Propeller, or Appliance) OfficeAtyfittro_ 15 fekleterof A;dorkan Adnitrekstration and AC43.9-1 (or subsequent revision thereof) for instructions INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAB 43 Appendix B, Failure to report can result in a civil penalty not to exceed $1,000 and disposition of this form. This report is required by law (49 U.S.C. 1421). for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Boeing 727-31 1. Aircraft Nationality and Registration Mark Serial No. 20115 N500LS Name (As shown on registration certificate) Address (As shown on registration certificate) . 1105 N. Market Street Z. Owner NORTHWEST HOLDING CORP. Wilmington, DE 19899 3. For FAA Use Ority 4. Unit Identification .5. Type Model Serial No. Repair Alteration Unit Make • AIRFRAME .....~..................~..ww.... (As described in Item 1 above) X POWERPLANT PROPELLER ' Type APPLIANCE Manufacturer 6. Conformity Statement B. Kind of Agency C. Certificate No. A. Agency's Name and Address U.S. Certificated Mechanic Page Avjet Corporation Fore.gn Certificated Mechanic 9809 Tradeport Drive OS4R425M Cer,iticaled Repair Station Orlando, Florida 32827 Manufacturer er t(s) identified in item 4 above and descri on t everse or attachments hereto D. I certify that the repair and/or alteration made to the un d that the i ation Federa Aviatio egulations have been made in accordance with the requirements of Part 43 of the U.S. furnished herein is true and correct to the best of my knciwiedge. Date Signature of Authorized Individ I £ SEPT-6496E-2:- 1993 /4 06g/ere-L-4 - -3491(C) 7. Approval for Return To Service - identified in item 4 was inspect in the manner prescribed by the Pu suant to the authority given persons specified below, the unit IX APPROVED O REJECTED Administrator of the Federal Aviation Administration and is Other (Specify) FAA Flt. Standards Manufacturer Inspection Authorization Inspector Fl" BY Person Approved by Transport FAA Designee X Repair Station Canada orthiness Group Certificate or Signet of Author d Ind ual Date of Approval or Rejection Designation No. .,Sgy te.___CgotoPtiztrA,1 2 SEPT: 9 1/ OS4R425M al -4y ) ere—ter:7r e EFTA00277838 -FAA AIRCRAFT REGISTRY CAMERA N0.3,V DATE: joria- rJyC ,-•“Iffet•t. NOTICE Weight and balance or operating limitation changes shallbe enteredin the appropriate aircraft record. An altelation compatible with all previous alterations to assure conti must be nued conformity with the applicable airworthiness requireme nts. • . • . 8.- Inscription of Work Accomplished (If more space is required,,attach additional sheets. Ident . ify with aircraft nationality and registration mark and date work .- • completed.) . 727-31 S/N 20115 N500LS REPAIRED CORROSION ON THE LOW ER FORWARD CORNER OF THE AFT DOOR BEAR STRAP IN ACCORDANC CARGO E WITH PAGE AVJET E.O. NO. 02838 DATED 8/11/94 AND APPROV 53- 30- ED PER 8110-3 BY DER MARION SO-339/ DATED AUGUST 22, 199 SHIN, 4. 2. REPAIRED DOUBLE DRILLED HOLES IN B.S. 940 MOD KIT'BRACKET ACCORDANCE WITH PAGE AVJET -E IN .O. NO. 53-10-02839 DATED 8/1 APPROVED PER'8110-3 BY DFR MAR 0/9 4 AND ION SHIN, SO-339 DATED AUGUST • 1994. 22, SUMMARY: 1. ALL PERTINENT DETAILS OF WOR K ACCOMPLISHED ARE ON FILE AT REPAIR STATION OS4R425M TIND THIS ER WORK ORDER 60298, DATED END • • • • g • • • .• . • E. .. • - • .t: :•• "P- • '•`- ;•• :de. • ! .r • . 1 • . 0 .• I. 4O; •. . • . • k • - •• • 1:‘'? • • 4 • D Additional Sheets AreAttniched .U.S GP0:1991.0-S8&012140035 • EFTA00277839 i -FAA AIRCRAFT REGISTRY CAmFRA N.i. :A/ DATE: 1O-1a- *it fi., • Form Approved • OMB No. 2120-0020 z, MAJOR REPAIR AND ALTERATION lis Department For FAA Use OTh cc tronsocconon (Airframe, Powerplant, Propeller, or Appliance) offiASIOrtESDO Fedora Aviation Admintoanion (or subsequent revision thereof) for instructions INSTRUCTIONS. Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC43.9-1 to report can result in a civil penalty not to exceed $1,000 and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Boeing 727-31 1. Aircraft Nationality and Reg .lion Mark Serial No. 00LS 20115 Name (As shown on registration certificate) Address (t i so_ivn on registration certificate) 5 N. Market Street 2. Owner NORTHWEST HOLDING CORP. Wilmington, DE 19899 3. For FAA Use Only 4. Unit identification 5. Type Model Serial No. Repair Alteration Unit Make (As described in Item I above) ---- AIRFRAME X POWERPLANT PROPELLER /14 Type APPLIANCE Manufacturer . 4 6. .Conformity Statement B. Kind of Agency C. Certificate No. A. Agency's Name and Address U.S. Certificated Mechanic Page Avjet Corporation Fo-eign Certificated Mechanic • OS4R425M 9809 Tradeport Drive X Certilicated Repair Station Orlando, Florida 32827 Manulecturer on the reverse or attachments hereto . D. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described ation gulatt and that the inf have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviatio t furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Inc:livid ,ial (2, S EPrE/Y)8Et /99 SZ 744a 7. Approval for Return To Service 4 was inspected in the manner prescribed by the Pu suant to the authority given persons specified below, the unit identified in item LI REJECTED Administrator of the Federal Aviation Administration and is ' . g1 APPROVED ..._ Other (Specify) FAA Fit. Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Canada • • orthiness Group Certificate or Signal . of Authorize ndivid Date of Approval or Rejection /Wirfi ge-4/ itfin At) Designation No. WFAA Form 337 it2.ettn 9' OS4R425M Ccht; ../A—,---A--; ,----> -- • • l• • •I • EFTA00277840 - PAA Al.cICRAFT REGISTRY CAMERA ?il DATE; . NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more spaco is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 727-31 S/N 20115 N500LS 1. RELOCATED ACCESS PANEL FROM B.S. 1183 TO B.S. 1350 LH AND RH BETWEEN STRINGERS S4 TO 57 IN ORDER TO FACILITATE ACCESS FOR FREQUENT INSPECTION TO TERMINAL FITTING IN ACCORDANCE WITH PAGE AVJET E.O- NO. 53-30-02837 DATED 7t'28/94 AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339 DATED AUGUST 22, 1994. SUMMARY; 1. ALL PERTINENT DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION OS4R425M UNDER WORK ORDER 60298, DATED 2.8,EPT934 --3-END • • • . • • ..... . • . — . . . • • • • - • • ..• • • • • • • • ❑ Additional Shoots Aro Attached * U.S.GPO:19 91-0-568-01 2/4003 5 EFTA00277841 FAA AIRCRAFT REGISTRY CAMERA NO, DATE: 0-1 - 93 Form Approved OMB No. 2120-9020 0 MAJOR REPAIR AND ALTERATION For FAA Use Only us Deporrmtt erifonteconeon (Airframe, Powerplant, Propeller, or Appliance) Office Identification Feigned Aylation Administration S0-FS00.15 (or subsequent revision thereof) for instructions INSTRUCTIONS: Print ortype all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 to report can result in a civil penalty not to exceed 91 00O and disp osition of this form. This report is required by law (49 U.S.C. 1421). Failure for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Boeing 727-31 1.' Aircraft Nationality and Registration Mark Serial No. 20115 NSOOLS Name (As shown on registration certificate) Address (As shown on registration certificate) .,. 1105 N. Market Street 2 Owner Wilmington, DE 19899 NORTHWEST HOLDING CORP. 3. For FAA Use Only 4. Unit Identification 5. Type I Model Serial No. Repair Alteration Unit Make AIRFRAME (At described in Item I above) X . , POWERPLANT PROPELLER Type ' APPLIANCE • Manufacturer 6. Conformity Statement B. Kind of Agency C. Certificate No. A. Agency's Name and Address Corporation U.S. Certificated Mechanic Page Avjet 9809 Tradeport Drive Foreign Certificated Mechanic 0S4R425M Orlando, FL 32827 _X Certificated Repair Station Manufacturer on the reverse or attachments hereto D. I certify that the repair and/or alteration made to the un t(s) identified in gem 4 above and described Aviation Regulation s and tat the information have been made in accordance with the requirements of Part 43 of the U.S. Federal furnished heroin is true and correct to the best of my knowledge . Date Signature uth•rized Individual 4 ,, f7/45,, -1/ V. 4:09.e.c..v/ • .4.e.u,. e.7 • itict.5/1.5 7. A for Rota • Service item 4 was inspected in the manner prescribed by the Pu suant to the authority given persons specified below, the unit, identified in Administrator of the Federal Aviation Administra tion and is R.) APPROVED O REJECTED Other (Specify) - FAA Flt. Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee x Repair Station Canada Ayryrorthiness Group Date of Approval or Rejection Certificate or SIgnatu e'of Authorized Individual Designation No. ‘f/ey / .1• go")/e , enwr r c2S- ? 3 0S411425M •7 2 /CAAin EFTA00277842 PAA AIRCRAFT REGISTRY CAMERA NO. 1 DATE: //'/- 93 Weight and balance or operating limitat NOTICE ion changes shallbe enteredin the compatibli with all previous alterati appropriate aircraft record. An alte ons to assure continued conformity ration must be with the applicable airworthiness req uirements. ?f-PLIZI 8. Description of W rk Accomplished (If more space is required, attach add ; itional sheets. Identity with aircraft nationa lity-and registration mark and date wor • k completed.) B727-31 -N5OOLS I. INSTALLED HONEYWELL TCA8i,II SYSTEM IN STC SA3094S0. ACCORDANCE WITH PAGE AVJET CORPORATION SUMMARY: 1 AIRCRAFT WEIGHT AND BALANCE UPDATED ACCORDINGLY. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. ALL SYSTEMS INSTALLED OPERATIONALLY CHECKE OTHER SYSTEMS. • D AND DO NOT INTERFERE WITH ANY 4. ALL ENGINEERING AND WORK ACCOMPLISHED AT PAGE AVJET C_ORPORATI STATION UNDER WORK ORDERS 7492, 8112 AND .ON_ REPAIR 9301. 5. AIRCRAFT TEST FLOWN BY FAA FLIGHT TES T ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORD ANCE WITH APPLICABLE DATA. . • • I:0: . ; .• • , is tlr,i ll Ic, : 1"i .".: • ; . • •: . . . • • . .„ . i•;.••-gz.:,••••6 f•..,:,-, • .i,:f l t .',!,, \• - ' •::.. ‘‘ ''‘‘. \;:!". I • . .. . ...ft..... .......:......,. ...!. ... ../...... ......! .: 30....:...a...... --.....-- ......-- .); nth:A I 1'. .. .• ::12.1::4 l'c . • :. '...:7 Pi l'n •.:), Pil..n. .6 .v i :n • j 1.1 t."-I:el• •I ...•.1 •)r•si sz.:•: -..! ;,:l. • .1.: rn:;..t...; '141.2....10./I 1 . 0 .r. Oil is.: 1!-I .t: P. -. ••• 0.!.. .. ..t.k;ft •-...:: it-p.i.j •,:. .,,,•.• ... nt,.41,9:.:t) • • . . !. i i • rtNi ,.:xlIzi.14,A rioibo.lardi I .. ...);,74 gg.i-..: . 2.,,LA.••• ' .. .: '' ‘1% ; • . . ... • I I I,. c.:;.;,.- i,' : d ' . •';'.".i.,.A .\ . ,ivt:./i •.: ...::::,,..e.A ..rtoe 'll..li .,....„ ., • .....k: , ......:.i„f.: ,i,...)...4•; • • ..1 •:. .t.,.:••••:; ct 1: • `t .' .. • %. i . \ littif..'11:110 i. ..•-.;ri‘t .1 •;%•..•••.71r>.k M., 4) ..'‘, l • .;, .. . \. ." . t:'• . •‘‘' . . , `,. .• • . . i e• ''.• . - O •Addllional.Sheit ..... . i Are Attiched ...,:2i: -.;..:c!.;.. ; . *U.S. GOVERNMENT PRINTIN G OFFICE: 1892-719-012/60 157' • . a" ..":•; l d . • .. • ' • • EFTA00277843 V. FAA AIRCRAFT REGISTRY CAMERA NO. 5r4DATES P - 4 - 9a e• • .• . • .. . • • ". .. e•-t • •• • I r r• '• • • d - 1 • • Form Approved • . OMB No. 2120-0020 .MAJOR REPAIR ANDcrALTERATION OS Depot imeni ,• ei bcnseorioi.on (Airframe, Powerplanl, Propeller, or Appliance) For FAA Use Only ....Aviation Administronon . '. Office Identilithoysli o is INSTRUCT IONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix Band AC 43.9-1 (or subsequent revision thereof) for instructions and disposition ol this form. This report is required by law (49 U.S.C. 1421). Failure to report can result In a civil penalty not to exceed $1.000 • for each such violation (Section 901 Federel.Aviation Act of 1958). t - Make Model 1. Aircraft Boeing 727-31 Serial No. , Nationality and Registration Mark • .1 20115 N500LS Name (As shown on registration certificate) Address (As shown on registration certificate) - i i= . • 2. Owner Northwest Holding Corporation P.O. Box 7138 • Wilmington, DE 19803 3. For FAA Use Only ' _ . • • 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration •r • AIRFRAME (As described In Item I above) ' ' • X POWERPLANT PROPELLER . - 1 ype .r., • ‘ i - APPLIANCE Maimlaciui ei - , • 6. Conformity Statement A Agen!.....y's Name mid Address B. Kind ol Agency --. C. Certi icate No. • U s Certificated Mechanic I Page Avje't Couporalion Furin9it Certificated Mechanic 9809 Trade-TWA_ Wive X Certificated Repair Station . 0S4R425M Orlando. Florida 32827 - - .. Meintilacturer D I 'Aoki ) h int ilicieravi .milk). oil...Limon made to the ini i(s) identified in item 4 above arid described on the reverse or attachments-hereto, !ed..; hem, mom: rk it, „woo,i, e with the requiremoids of Part 43 ol the U S Federal Aviation Regulations and that the Information umrushed rivrem is um: arlij ‘Ollad W the best ol my knowledge. • 22 !hire I ' • Signature ol Auth i d Individual 4 AMC, 4 : 447 4 .90 --- 7 .3- -1 I/ L11.2 9_12_5. ..... + . . lac (---- 7. Aoki:oval for Return To Service Pursuant to lily at/Viunty ii.er tau auirs specified below, the unit identified in item 4 was inspected in the manner prescribed by the AdillitirSilaWl Ul the I tide' di A.I.Illuil Administration and is • El •APPROVED 0 REJECTED ••• ". - • • I AA I. It Sidnjoids Other (Specify) inspector MoilltlidditilUI ' Inspection Authorization • UY — _ , . ' FAA Desynee itemui Station Pelson Approved by Transport . X Canada Airworthiness Group Date ul Ai provid or illittClivil Gelilk:Me or Signature of Authorized Individual a_a i d Lictzl -zn-4.-f s4vth g Designation No. .. 2) Luc ' 4( 5 t . OS) OS411425M "• I" tstrima' • EFTA00277844 • • • FAA AIRCRAFT REGISTRY . • CAMERA ND. 3 AiDATE. // 70 - 9a • • • . . lir.. • . • • ". .. • : •• Weight and balance or operating limitation changes NOTICE shall be entered in the appropriate aircraft record. An compatible with all previous alterations to assur conti alteration must be e nued conformity with (he applicable airworthiness requi rements. 8. peeccIplion of Accomplished firmara japcali required. attach additional sheets. Ident 1 ity with aircraft nationality and registration mark and dale work completed. ) D727-31 5/N 20115 N500LS • 1. MODIFIED SECOND BATTERY SYSTEM PER PAGE .AVJET CORPOR STC SA3092SO, MASTER DRAWING LIST MDL-91-37 1 REV. ATION- A. 2. MODIFIED ED44-805 EFIS PER PAGE-AVJET CORPORATION STC MASTER DRAWING LIST MDL-91-44, REV. A. SA3085SO, 3. MODIFIED FMS-800 FLIGHT MANAGEMENT SYSTEM PER PAGE CORPORATION STC SA3089S0, MASTER DRAWING LIST MDL AVJET REV. A (NZ-9112 SOFTWARE). -91-43, SUMMARY: 1. PROVIDED WEIGHT AND BALANCE UPDATE. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. el 3. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OTHER SYSTEMS. 4. ALL PERTINENT DETAILS,Or% WORK ACCOMPLISHED ARE ON FILE AT PAGE AVJET CORPORATION UNDER WORK ORDER 9286, DATED AUGUST 31, 1992. • END • 0 ••••••••• •• • • i • . • • _ • . - • • - • .. - • - ,•. ! ! . . : t. • • rt..; A II • • • • ••••• .• ••• • . . . • • I r • • '• • • •• ❑ Additional SheetiAre Attached • 411Serirt- OrOnMalal • • - • i EFTA00277845 FAA AIRCRAFT ' CAMERA NO. bi DATE: th _ Qom, • t. Form Approved 0 OMB No. 2120-6020 usorpcsimens • MAJOR REPAIR AND ALTERATION ' For FAA Use Only cr Ircesoorvorm (Airframe, Powerplant, Propeller, or Appliance) Office IdentWcation redone Aviation • . ediminisfrotion 30-f300-15 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR.43 Apkndix B. and AC43.9-1 (or subsequent revision thereof) for instructions and dispoiition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1 Make Model Boeing 727-31 • 1. Aircraft I Serial-No: Nationality and Registration Mark 20115 N500LS •1 Name (As shown on registration certiiicafe). Address (As shown on registration certificate) 2. Owner Northwest'Holding Corporation P.O._ Box 7138 • •• . ' Wilmington, DE 19803'" . 3. For FAA Use Only . si. • . • , . . ..• , I 4. Unit Identification 5. Type . ?. • Unit Make Model " * Serial No. Repair • Alteration •• • AIRFRAME ..--- _ - (As described in Item 1 above) ' X . • • • . " POWERPLANT - • PROPELLER , - Type • • , APPLIANCE Manufacturer . • 8. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certilicaled Mechanic Page Av jet Corporation Foreign Certificated Mechanic 9809 Tradeport Drive X Certificated Repair Station OS4R425M. - Orlando/ Florida 32827 Manufacturer D. I certify that the repair and/or alteration made to the un I(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S Federal Aviation Regulations and that the information - furnished herein is true and correct to the best of my knowledge. Date • Signature • A izer :' idu 2 J O i-f r ) It: 14 Lt, ire (\.) 4- 7. 'Approv !Return To Service ••• Pursuer I to the authority given persons specIlled below. th nit identified in item 4 was inspected in the manner prescribed by the Administi ator of the Federal Aviation Administration and is KI APPROVED O REJECTED FAA Fli Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee X Repair Station Person Approved by Transport . Canada Airworthiness Group Date of Approval or Rejection Certificate or SI enure of Authorized Indi dual Designation No. alt() . Zs JAL) PAA'Form 317 II; net i 5 OS4B425N_ . .hil-U/1) H L-Fr1 nil tqa--- EFTA00277846 NOTICE must be Weight and balance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration nts. compatible with all previous alterations to assure continued conformity with the applicable airworthiness requireme & Description of Work Accomplished • Of more space Is required, attach additional sheets. Identify with aircraft nationality and registration mark end date work completed.) INSTALLED SUNDSTRAND MARK VII WINDSHEAR DETECTION/GROUND PROXIMITY WARNING SYSTEM (GPWS) IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3133SO. ALL WORK ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION AND IS ON FILE UNDER WORK ORDERS 4784 AND 8112. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. 003.4122044. EFTA00277847 FAA AIRCRAFT REGISTRY CAMERA NO. IN DATE: — q 9v2 - 'tar ••• • er e • Form Approved ..• OMB No. 2120-0020 CO MAJOR REPAIR AND ALTERATION For FAA Use Only USE/ewer:erg Appliance) (Airframe, Powerplant, Propeller, or Office Identification okinfosnorym Federal AvIcalcin so--Fs110-15 Acentrkstratton on thereof) for instructions s. See FAR 43.9, FAR 43 Appendix El, and AC 43.9-1 (or subsequent revisi INSTRUCTIONS: Print or type all entrie in a civil penalty not to exceed 51,000 of this form. This repor t is requi red by law (49 U.S.C. 1421). Failure to report can result and disposition Aviation Act of 1958). for each such violation (Section 901 Federal Model Make -31 727 Boeing 1. Aircraft Nationality and Registration Mark • • Serial No. N500LS • 20115_ Address (As shown on registration certificate) II • Name (As shown on registration certificate) • 2. Owner • Northwest Holding Corporation ! P.O. Box 7138—_!... .: Wilmington, DE 19803 3. For FAA Use Only . • C. , ... • . • . . S. Type 4. Unit Identification • Serial No. Repair Alteration Make Model Unit ' - (As described in Item I above) a X AIRFRAME .- . POWERPLANT % . PROPELLER Type APPLIANCE • • Manufacturer • 8. Conformity Statement C. Certificate No. ir B. Kind of Agency A. Agency's Name and Audi ess • • U S Cerlilicatee Mechanic Ft:feign Certificated Mechanic :1 ' Page Avjet Corporation OS4R42514 X Ceitilicated Repair Station 9809 Tradeport Drive Manulacluier Orlando L_Florida 32827 or attachments hereto repair and/o r altera tion made to the un t(s) identi fied in item 4 above and described on the reverse D. I certily that the and that the information made in accor dance with the requir emen ts of Part 43 of the U.S Federal Aviation Regulations have been knowledge. furnished herein is true and cot rect to the best orsity Signature of Authorized Individual i4Afral.5 r. Writ* Jr. • Date I ?9r? 7. A r I for Return To Service er prescribed by the Pu suat I to the authority given peMbna speci fied below, the unit identified in item 4 was inspected In the mann 09 APPROVED O REJECTED Administrator of the Fedora) Aviation Administration and is Other (Specify) i FAA Fit Standards Manufacturer Inspe ction Authorizatio n Inspector BY Person Approved by Transport FAA Designee X Repair Station . Canada Airworthiness Group Certificate or Sigr lure of Authorized Individual Date of Approval or Rejection • Designation No. it er:.6.4 a0D. 3,ti-r) fici a QS4R4a5EL Ds v11) bi 2.417/472#2 inn rum, 337 I I,girt c- • • EFTA00277848 FAA AIRCRAFT ' CAMERA NO. /A./ DATE: 6 ) _q_ NOTICE O Weight and balance or operating limitation changes shallbe entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requireme nts. 8. Desalpilcin-otWolfaccomplished (If more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) 0727-31, $/N 20115 1: INSTALLED,EXECUTIVE'INTERIOR.IN.ACCORDANCE.WITH.PAGE AVJET CORPORATION.STC.SA3137S0. 2. INSTALLED HONEYWELL EDZ-805 ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS) IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3085S0. 3. INSTALLED MODE "S" TRANSPONDER IN ACCORDANCE WITH PAGE AVJET CORPORATION' STC SA3095S0. 4. INSTALLED JAMCO SMOKE DETECTORS IN ACCORDANCE WITH PAGE-AVJET CORPORATION STC SA3132S0. 5. INSTALLED DUAL HONEYWELL AA-300 RADIO ALTIMETER SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3087S0. 6. 'INSTALLED HONEYWELL PRIMUS 870 RADAR SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3086S0. 7,. INSTALLED HONEYWELL FMZ-B00 FLIGHT MANAGEMENT SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3089S0. 8. INSTALLED DUAL COLLINS PROLINE II COMMUNICATION AND NAVIGATION SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3090S0. 9.. INSTALLED HONEYWELL TCAS II SYSTEM PROVISIONS IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3094S0. 10. RELOCATED FIRE "T" HANDLES IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3111S0. 11. INSTALLED FAIRCHILD II PARAMETER FLIGHT DATA RECORDER IN ACCORDANCE WITH'PAGE AVJET CORPORATION STC SA3091S0. 12. INSTALLED DUAL 40 AMP HR NICKEL CADMIUM BATTERY SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3092S0. 13. INSTALLED DUAL HONEYWELL ADZ-800 DIGITAL AIR DATA SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3088S0. •i 14. INSTALLED AES AUTOPILOT INTERFACE UNIT IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3093S0. El Additional Sheets Are Attached • *U.S.OP0:1989 a 803•17t • EFTA00277849 FAA AIRCRAFT REGISTRY CAMERA NO. At • .DATE:' - PAGE 3 OF 3 - . • . INSTALLED HYDRAULIC ACOUSTICAL FILTER IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3136S0. . INSTALLED ESSENTIAL POWER SELECTION SYSTEM IN ACCORDANCE WITH .PAGE AVJET CORPORATION STC SA259(T!:. SUMMARY: 1. AIRCRAFT WEIGHED AND NEW WEIGHT AND BALANCE COMPUTED. 2. .'EQUIPMENT FURNISHING LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS INSTALLED. OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. 4. ALL WORK ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION AND IS ON FILE UNDER WORK ORDERS 4784 AND 8112. , . 5. AIRCRAFT.TEST FLOWN BY CUSTOMER AND ALL SYSTEMS CHECKED NORMAL. 6. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. END • . 0010404411'. 77,77:,.1....4;b, EFTA00277850 4. W Sta . , •• 41wartentwasintemam - ~~rt1ZR EFTA00277851 3:71r 'n • FAA AIRCRAFT REGISTRY t;;Palt retir CAMERA NO.3 N DATE: 9 - 27 - 91 0 ' . -,• • • US Derainlent • APPLICATION FOR •INSTRUCTIONS —Print or type. Do not write in shaded area. or Trompoisoico • AIRWORTHINESS use only. Submit original only lo an authorized FAA Represen s; these are for FAA space is required. use an attachme tative. II additional FederalMotion Admirilownion 500 L-9 CERTIFICATE II and VI or VII as applicable. nt. For special flight permils com plete SeCtiOns 1.REGISTRATI immt Z it t 0 • N Sb St .. 2.AIRCRAFT BUILDERS NAME 'Boet IQ 6- • (Make? 3. AIRCRAFT MODEL DESIGNA TION 4. YR. MFR FAA CITING r 5 C' 5. AIRCRAF e 1 -6 1 '... 3I . - /96/ 3 F Vo / o ..,. cc u Ma — 0 • a 0 iis- 6. NGINE BUILDER S effint iiimey AME (P.LiAw 7:3ge/ /TEL Dc.CeTIOtria$0 / 6. NUMBER OF ENGINES 9. PROPEL/En BUIL LA S NAM E /Maker ,17-3 b - c3-19C Carta 10. PROPELLER MODEL r 4, C53 C OR A/ iv 4- . cIGNATION vi :4 11. AIRCRAFT IS rChecA ii app4seaDiel APPLICATION IS HEREBY MADE FOR: (Check andfiCable 4lenis l i IMPORT A i X STANDARD AIRWORTHINESS CERT a IFICA TE !Indicate category) I !NORMAL I [UTILITY I I ACROBATICD1(1 TRANSPORT • B SPECIAL AIRWORTHINESS I [GLIDER CERTIFICATE (Chock appropriate ?Sem I [ BALLOON i? 2 LIMiTE05, o . . 'Ai ai s. 5 PROVISIONAL Widmer. Clan; 1 CLASS I O i3 W cc 1 CLASS q AGRICULTURE AND PEST RESTRICTED fIndoCale OporatiONS CON TROL 2 AERIAL SURVEYING Z 3 r 10 3 AERIAL ADVERTISING 0 be conducted; 4 FOREST; Wildlife conservflione r:. s PATROLLING 6 WEATHER CONTROL < 7 0 CARRIAGE OF CARGO 7. 0 OTHER (Speedy( 1 RESEARCH AND DEVELOPMENT cc . 4 EXPERIMENTAL (Inciter* opers 2 AMATEUR BUILT W to to condo:WO borest 4 3 EXHIBITION U • RACING • s CREW TRAINING MKT SURVEY . . 0 70 SHOW COMPLIANCE WITH F AR 1 FERRY FLIGHT FOR REPAIRS. ALTE RATI ONS. MAINTENANCE OR SPECIAL FLIGHT PERMIT ihrdic STORAGE ale 2 EVACUATE FROM AREA OF IMPE AA e oporet,ort lobo conducted. Wen NDING DANGER n. complete Section VIM VII as 3 OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKEOFF WEIGHT apphcablo On serene sycliN 4 6 DELIVERING OR EXPORT • r5 I I PRODUCTION FLIGHT TESTING CUSTOMER DEMONSTRATION FLIG C 16 I MULTIPLE AIRWORTHINESS CERT HTS IFICA TE (Check ABOVE 'Rest(t led Oper ation and 'Standard' or • L.noled A. REGISTERED OWNER (As show as turr,cabie r n on certificate of anCiall registration) NAME IF DEALER. CHECK MERE d e+c, ADDRESS /may VOVZICOEST" 6 10 4.2)./A)Ce B. AIRCRAFT CERTIFICATION BASIS (Gncc* anplitable Wachs arid COmp fetv items al indica ect) e. - icAwerin, zfraiku4-( 6-- /Foos rev Cg ,a> R, . ti(ne 4 /Ss ,i4 1Jfr S AIRCRAFT SPECIFICATION OR TYPE CERT IFICA TE 1 a p and Revision Nal DATA SHEE T /Give No .3 C AIRCRAFT LISTING (Gov pego 3 nontoellell AIRWORTHINESS DIRECTIVES latest AD No )4 O9O X,IPPLEQNT AL TYPE CERT iCtioca;a/ai:esvereabte AD s complied with 4) ._ and gar g IFICATE (List numb er of earn S TC incorpcua /O A loc0 15 C. AIRCRAFT OPERATION AND MAIN TENANCE RECORDS t /14 8 l itifri !Twee/ 623./ /990 CHECK IF RECORDS IN.* TOTAL AIRFRAME Nouns • 0 COMPLIANCE WITH . , FAA 91 173 . EXPERIMENTAL ONLY r r-I 'ICI vans D. CERTIFICATION — I hobby cs, 94/4./ .. . 51000 lass cVIII f; Cale ;5504.41 co reneiree4 Cellily ItiAl I III the iegislesed Admonish/Ilion an accordance with owner (penis agent; til the aricia Suchen 501 cil the Federal Mullion ll deathbed above. mar 1/00 ancia airworthy and eligible for the airworthine ALI 0119511.atin applicable Fede l1 is iegisleted with the Federal ss ter Oman: rem •' rid ral Avialion RegulattoiLs.tusd Thal *rialto° .... ... . . . 1110 RIICIall has been inspected and is DATE OF APPLICATION E AND TITLE 4,07— 40. Ttroir-- • - \ 774-4/ 0, 3 / 990 - HUM It % (di. . SIGNAT UR A. THE AIRCRAF I DESCRIBED ABOV I IAS ([LEN INSP ECTED A D FOUND AIRWORTHY BY (Con yl (-c-, nr.thsptcrio FAR PART 121 OR 127 CERT n/few ;h... •••. .oti only if FAR IFICATE HOLDER (Give 21.1671( I onseaf '" Cerrthesto No 1 CERTIFICATED MECHANIC (Girt. AGENCY 3- Cartrircale NO. I — - - - • CERTIFICATED REPAIR STATION 6 (Gat Certificate No 1 • AIRCRAFT MANUFACTURER ;Grre veRincemot name of font? 4. • —— - t _. . I DATE TITLE .. .... . • .. ..SIGN.ATUR . E ' _ Whets ALL ,ipplicablo blocks in dents A a dB) A. yawl dial die anciall described in Secti THE CERTIFICATE REQUESTED on I or VII meets retarireinenis for. 1. Z AMENDMENT OR MODIFICATION r. 0 B. Insociclion lot a special High: peed OF CURRENT AIRWORTHINESS CERT under Sect. IFICATE to g vats conducted by. .. . 'FAA INSFIECTOR . ... ... . lr-„. • —.. AA DESIGNEE g a DATE c > iv w DISTRICT OFFICE . DESIGNEE S SIGNATUR RE A 1, : CERTIFICATE HOLDER UNDER: FAR 65 [ FAR 121. 127 or 135] 1 FAR 145 _I . ._. __ FAA INSPECTOR'S SIGNATURE ki c U **ID AI\ e ..• % 1Vvi . . • D2. ... F 5 .' NrIl • .. : ' .' • EFTA00277852 FAA AIRCRAFT REGISTRY CAMERA NO..)) At DATE: 9 - 27 - 97 *U.S.CPO:1989-241473/90913 S • A. MANUFACTURER. . .. . •• - . .. . _ •- ADDRESS . NAME - .. • . , . .VI• PROOON B. PRODUCTION BASIS (Check applicable item) - PRODUCTION CERTIFICATE (Give reduction COW:Cato numbs') FLIGHT TESTING UCTI TYPE CERTIFICATE ONLY • .. . .. ........ .... .. • APPROVED PRODUCTION INSPECTION SYSTEM C. GIVE QUANTITY OF CERTIFICATES REWIRED FOR OPERATING NEEDS SIGNATURE DATE OF APPLICATION NAME AND TITLE (Prop or typo) • A. DESCRIPTION OF AIRCRAFT ADDRESS • ' REGISTERED OWNER • ... s •• MODEL: • BUILDER (MAW . • ' . • ,. REGISTRATION MARK . SERIAL NUMBER . . - • . • . .• • STONER DEMONSTRATION FLIGHTS l 0 jebeea d abolicabiel B. DESCRIPTION OF FLIGHT • "•- . FROM, • •• TO • .. .. .. .. . • ... . .... ,.. ... .. .. .,.. • .. ... . . .. ,... Mt SPECIAL FLIGHT PERMIT PURPOSES'OTHER THAN PRODUCTION FLIGHT TEST DEPARTURE DATE DURATION VIA •. .. . . . .. . . .. . . -. • . . : • \ C. CREW REQUIRED TO OPERATE THE AIRCRAFT AND ITS EQUIPMENT.: -- • I PICOT COPILOT NAVIGATOR • OTHER /Speedy/ NOT MEET THE APPLICABLE AIRWORTHINE SS REQUIREMEN TS AS FOLLOWS. .13. THE AIRCRAFT DOES . ,. . . .. . . • .. . • ". - ' ' •• . . . ... . . .•• .• • .'. . _ . .... . . ..,.. _.. _ _ ........ . ....... ..... .. .. . . - •- ._ . . . • '. -.. • ..... . : "- -...‘. '.., CA:: • c •'' • : '` - i . „ : 7:i-: •• .. . . • s `.. ., -. 5.‘11.2.•,- . V i•-• • .' ..i.*:•• • • • . .. . - . . ..- • .. • .. .. •. . . . . . . .. . . .. I , r- , -• . ,' • . • •• ii .; • . • .... .":•• OPERATION ruse effacement ,0 necessary; ; • . . E. THE FOLLOWING RESTRICTIONS .ARE CONSIDERED NECESSARY FOR SAFE . ! i ; .. ...„ . .. -. - ....-....... „..--- - . . i I . 3 ' -- • • •, . • •• •,..... r" ... .. .. -..... . - -.... . ... . -. •- .. ; s! ..•r•:•: • c •• • :,• • ,, ., ; . : • : 1 I •.* I ,• .. . , .... .: •.'; •:.* • Ir•l"••••: . .. . . . _ : • .4.. .. .. • • '. I .. ' . . % : .:.. : ; r.I.V:r.I.• Cr" ? . I Y i • 1• . 7. t : f.ol a.:. a •c.. ! • :••: i : . i I f .. ._. . .-., ., • • i. ..; - • \• • • • • •• • •• •• . . • • !6 1 . .. .:i.. • .. . • . . - • .- • . FederalA.O1UP% Adm satiation tn ...v. registered owner tor nia agonbollhaerallalssarawslabove.IntIlwaecransregaleravalhan • • f. CERT IFICATION — I hereby certilythell ant the and that the Nara Ins been Inspected and is airworthy for Ins high) .. Federal Avestan Regialront . . • accordance with Section 501 of the Fetleral•Avialion, Ad of 1958, and imitable . , described . - .. SIGNATURE • _ . . OAT C . [NAME AND TITLE (Thint of typo) . ., . • . •. .' . .. i.. O..Slidstalent of Com o i mily. FAA Form 01304 (05(tath when require**. A. Operliting Lunations and Markings InVriniPtuinirilelin FAR ' . VIII. AIRWORTHINESS 91.31 as Applicable ' •• • . .- H. FOllfieriiiilifOtihtn!“ Cerhi;Calion. the fritpOri Airafal— . • ... --- •-••.:: • 1 ... . . . .. • }Aback when toZhatedl ".%''C t . % • • D. Cimeni Operably Limilolions Attached :• - • ••• l.':_•.1 • . "`. " 1 - DOCUMENTATION • • I. Previous Auwonnin ' Cgical lis . cadres willi::. C. We. Drawings. Pholographs, etc. (iitlachechen toquiredi•'. ' 1• FAlit73 - (Oligtnal Allacht(11 D. Current Weight and Balance InlosmatiOn Available in Aircraft . (FAA use only) J.Current AnwortAiness 1 1 nificat I's in Accordencesvah . . .. . . . V E, Major Repair and Alteration. FAA Forni 337 (AlraehWhen iiquoitcli FAR :2 11 .. 1 . ) • /Copy inched) [ V F. This Inspecah Racurded f M etall Records . , .. ; , . • ' ' EFTA00277853 • FAA AIRCRAFT REGISTRY a. CAMERA NO.3 N DATE: 9 - 27 - 91 4 Ot.kr", it.'421 : . s•• • • . • • • • • 'a . • . ' ••.' • • 9 • . . •• •• ' - . • . •• .• • t . . • UNITED STATES OF AMERICA , DEPARTMENT OF TRANSPORTATION—FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE, , MANUFACTURER AND MODEL 3 AIRCRAFT SERIAL A CATEGORY 1. NATIONALITY AND 2 REGISTRATION MARKS NUMBER •„ N505C BOEING 727-31 20115 TRANSPORT 1 ••••• • , • • ' . . • 5. AUTHORITY AND ETAS S FOR ISSUANCE the •• TNsainvorthiness certificate is issued pursuant to inFederal Aviation Act of 1958 and cenif es that. as of the date ol issuance. • aircraft to which issued has been inspected and found 10 conform to the type certifteme Therefor, 10 oe in 'condemn for sale • 'r "....•• r • ••• as . . operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code provided by Annex 8 to the Conventionel. Iniernabonal Civil Aviation. except as noted here" Exceptions' ' •• • . NONE . . • ••••• • .- • . 6. TERMS AND CONDITIONS by the ACImintSlialOr. Ibis '.. ...?.... .. Unless sooner surrenclerea, suspended. 'evoked. Or a lerthination dale rS °MM.'Se established are performed in ... .,,l airworthiness certifies', rs effective as long as the maintenance. pievenlative maintenance. and anerabons le. and the aocran is leg:Ste:ea .ntrieUnitecl ....; . .• , accordance with PartS21. 43. and91 of theFederal AviationRegulations. as aPPI States DESIGNATION NUMBER , • DATE OF ISSUANCE DAR-41-FS-NM - .•-• • •, • 7/23/90 ot exc ng if 000 0 imposonmena erCeerbng 3 / , . . •.... Any alteration. reprOduCliOn. Or M. use of this certificate may be purushableoy 8E . DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL I: . .:• • • •• • • years. or both THIS CERTIFICATE MUST ' . ' • • • . AVIATION REGULATIONS. . . . . GPO si2•e04 FAA Form 8100-2 •• (8-821 • a 0 IP • - • • • •, • I. ••• •• • • : • 0 • •7 : • • ....N..— •—•••'. - • • .. • x. • -rm. EFTA00277854 FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 21 EFTA00277855 • • t t 4 ' .•• •Ah.: 0A • • • • j • . ..• in , A . • • . •• • r • • rr• - • 1 • ." • . • . • . r 0 . uS dearnmenr . MAJOR REPAIR . Form Approved or TIXISDOefOriOn ' • (Airfram A N D A LTERATION e, Powerplant, Pro OMB No. 2120-0 Act.wwwAv icnien ROCIOCOI 020 wwton peller, or Applia Gk nce) For FAA Use Onl y INSTRUCTION Office Identificatio S. P n and disposition of rint or type all entries. See FAR 43.9 this form. This re , FAR 43 Appen for each such violation (Section pot t is required by la dix B. and AC 43.9-1 901 Federal Avia w (49 U.S.C. 1421 (or subsequent re tiOn Act of 1958 ). Failure to repo vision thereof) for ). rt can result in a instructions _-, M ak e ci vi l penalty not to exceed 51,000 1. Aircraft BOEING Model • . Serial No. 727-100 20115 ' Nationality and Registration M Name (As show n on registration ce ark. rtificate) N505C • 2. Ovine'' Address (As sh own on registratio NORTHWEST HOLD 1409 Foulk Roa n certificate) ING CORPORATION d, P.O. Box 71 Foulkstone Pl 38 'Wilmingt aza, Suite 102 on, Delaware 1 3. For Use Only 9803 - _ Unit 4. Unit Identificat ion Make . S. Type Model Serial No. - AIRFRAME Repair . Alteration (As described in Item 1 above) POWERPLANT X PROPELLER V ___ ___ _ ___. _ _____. _____ Type t{FPLIANCE Manufacturer . -- _ A. Agency's Nan 6. Conformity akend Address Statem ent North American l B. Kind of Agenc A Rockwell Inter ircraft y national Corpo U. S. Ce rti fic ated Mechamc , C. Certificate N o. 2825 E. Avenue ration I Fo re ign Ce Airframe Class Palmdale, Ca. P m ficated mecna I X I Certificated Repair Stat mc 4 93550 ion Limited Powerp D. I certify that I Manufacturer lant the repa ir and/or altera Class 3 have been made tion made to the in accordance with the require unit(s) identifie NXAR6B8K furnished herein is true and correc ments of Pal 43,0 d in item 4 above and described Date t to the best of my knowledge. 1 the U.S. Federa l Aviation Reg on the reverse or attachments he ul re ations and that to -th e informatio I Signature of i :,. n Authorized Indi / / July 20, 1990 vidual I • D. A. Perazzo Pursuant to th T. Approval Col Retur /14.- Administrator of e authority given -persons specifi n To Service . .— , the Federal Avi ed below, the / ,......1,.../ " ation Administratio un it identified in ite n and is CD APPROVE m 4 was in f FAA Fit. Standa D spected in thez rds 1 - L 7i REJECTED manner prescrib InsP i M an uf ac ed by the BY tu rer 1 Inspection Auth I Other (Specify) orization FAA Designee 1 x Repair Stat ion Person Approved Date of APProv ai or Rejection Canada Airworth by Transport • Certificate or iness Group n Designation N Signature of A July 20, 1990 o. uthorized Indi vidual . I1 NXAR688K • • , I FAA Fo rm 337 • U. A. Perazzo' ' II V t • I— • EFTA00277856 r. _ hr:::1.1 tit .• • -•.; . • . • :, . • t...; ••, , I EFTA00277857 FAA AIRCRAFT REGISTRY CAMERA NO.9 DATE: 9 - 27 - 91 • ti • • 4 • 4." ' • NOTICE • must be ll be ent ere d in the app rop riat e airc raft record. An alteration itation changes sha iness requirements. Weight and balance or operating lim ass ure con tinu ed con formity with the applicable airworth • rati ons to compatible with all previous alte ed mark and date work completed.) 8. Description at Work Accomplish additional sheets. Identity with aircraft nationality and registration (if more space is required, art • - ial MUm ber 201 15, in accordance with supple -10 0 , Ser A. Modified Boeing Model 727 363NM, amended September 1, 1989 as follows: mental type. certificate SA4 ng Doc ume nt VA0 000 01, Rev ision F, dated January T. Valsan-Boeing 727-200 Re-eng ini 's• • 15, 1990. . eri ng Ord ers (E WS ) are in addition to the gs and eng ine 2. The following drawin aboVe document: g. NOTE: "VA" denotes Valsan Drawin a. Chapter 24 ELECTRICAL POWERical System Initl. - Strut E.O.: 003A, 101 . VA240000 A • Electr Pan el- Loa d Con tro l Cen ter Mod ification E.O.: 003A, 004, 005, 0240007 E & 006 , STRUT b. Chapter 28 FUEL SYSTEM INSTALLATION Strut Feed Thru E.O.: 100 VA280001 B Tube Assy - Fuel c. Chapter 48 MISC t. 48-727 E.O.: 101, 102 VA481100 A Pressure Buldhead Reinforcement Sec VA481200 C Frame Assy Sta 1263 E.0.:.101, 103, 116 VA481300 C Fuselage Skin E.O.: 106, 114A, 114 A 1243 W/L244.39 E.0: 106, BST VA481324' NC Intercostal Assy - BSTA 1223- to A 1243 W/L234.06 E.O: 105 VA481325 NC, Intercostal Assy - BSTA 1223 to BST URE d. Chapter 53 FUSELAGE STRUCT t Weight Installation E.O: 100, 102 8 Ballas VA6.30001 las t Wei ght , Sup por t Str uct ure Ass y. E.O.: 002,100 VA530003 C Bal 360 E.O.: 002, 100 • VA530004 - NC Ballast Weight Instl. STA 312 - e. Chapter 54 NACELLES & PYLONS Assy (Sh. 1, 2, & 5) E.O.: 003 VA543000• C Main Strut D Fir ewa ii Rib , Sid e Engine E.O: 36A, 003A -VA543100 f.' Chapter 71 POWER PLANT, nt Ins tl. - Eng ine Pod V727RE E.O.: 002, 105B, VA710000 NC Pow er Pla 110, 003, 111, 006A 109, 108, 001A, 104A, 005A, 004, L g. Chapter 73 ENGINE FUEL AND CONTRO eno id Wir ing Dia gram E.O: 002(Rev L), . VA732301 .K App roa ch Idl e Sol 002 (Rev. M), 003(Rev. M) Rel ay Ins tl. - App roa ch Idl e Solenoid E:0.:. 103, 003, 100B VA732303 0 Swi tch /IN D Lig ht Ins tl - App roach Idle E.O.: 002, VA732304 0 .: 103 A Swi tch Ins tl. - Nos e Gear Position Approach Idle £.0101 - VA732310 ots Ove rhe ad Pan el E.O .: 100, 002, VA732315 NC Relay Ins tl. Pil h. Chapter 76 ENGINE CONTROL E.O.: 00ZA VA760000 A Engine Controls Instl. - Strut 100, 101 VA760014. A Drum Instl. - Eng. Controls E.O.: .: 105 VA760015 A Bracket Assy - Pulley ESTA 100 E.O ched (1§ Additional Sheets Are Atta • U.S.GP0,1989.0-663. 11 EFTA00277858 FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 91 EFTA00277859 FAA AIRCRAFT REGISTRY CAMERA NO2 A' DATE: 9 - 27 - 9/ . - r DESCRIPTION OF WORK ACCOMPLISHED 1ContinuedY •• , Serial No. 20115 .Chapter.77. ENGINE INDICATING VA771005 NC Indicator:Engine,?ressu're Ratio EPR, E.O.: 001 Chapter 78 ENGINE EXHAUST , • a VA780000 . • B Engine Strut Controls Instl. VA783010 E Fit Deck -Indicator Ihstl. T/R'Sys': E.O.: 003, 004 VA78301I- F, Thrust Reverser System Wiring Diagram E.O.: 002 (Rev VA783013 D Support Bracket Assy - T/R Control Valve•R/S E.O. . G) - VA783017 J Placardi E.O.: 007, 008 : 100 (Rev. E . VA783024 B Relay Instl. - Thrust Reverser Control E.O.: 003 VA783028 A Mixer, Exhaust - Instl. 727E E.0:: 100 VA783101 C. No. 2 Engine T/R Wiring Deactiviation E.0.: 002 ° k• 'Chapter 91 CUARTS• VA910002 ' A Instl. - Electrical Wire Harness E.O.: 003, 004, 005, VA910008 NC Wire List V727RE E.O.: 001, 002, 003 006, 007 • *NEW DRAWINGS ADDED TO MODIFICATION P. Boeing 727 Service Bulletin 727-53A0171, dated December 14, 1989 SUbject: Fuselage - Station 1182 • Pressare Bulkhead web, . Crack Repair and Preventive Modification • C.. The aircraft empty weight and center .of gravity . , was revised in accordance with Boeing Weight and Balance Manual D6-21100. Weight and Blan attached. ace Manual Supplement, VA-CR279 is . ... D. VA000003, Rev. A, Dated 4-4-90 is equivalent to VA000001, Rev. F, dated 1-15-90. END Sri EFTA00277860 r, FAA AIRCRAFT REGISTRY CAMERA NO3 DATE: 9 - 27 - 97 • EFTA00277861 FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 27 - 91 pa,5649-tioat PARTS A THROUGH D. N/A L INIT IAL EAC H ITE M IWT HE APPLICABLE BLOCK FOR THE CHECK LIST WIL i. PERSONNEL ACCOMPLISHING TO A/C BEING WEIGHED. BLOCKS NOT APPLICA BLE RATIONAL CONDITION. O2, H20 ) SHOULD BE IN NORMAL OPE 2. ALL BOT TLE S (02C ECTOR OR HIS DESIGNEE: S LIST MUS T BE COORDINATED WITH CHIEF INSP WILL CHECK & SIGN FORM BE• 3. ANY DEVIATION FRO M THI FOR EMA N/LE AD MEC HAN IC OR ASSIGVED INSPECTOR THROUGH D THE 4. ON CONIPLErION OF PARTS A ING. DIN G WIT H WE IGH Checke FORE PROCEE . Ch ecke d By ti9 FLU IDS pV • 1. FIL . L ENG . OIL SYSTEMS & TANKS FULL VI.4-1- k." 7 6. LAVATORIES CLE ANE D & VAC UUM ED ' Q S & SEAT BACK ke 4. 0,,,. ...r ALL MAGAZINES, NEWSPAPER DRA IN . OVE D 2 ALL FUEL TANKS DRAINED USING 50•7. , 7< LITERATURE REM %43%d PLUGS WI (H AIRCRAFT LEVEL ERS 0 1: 1 IR COV KS . -PROTECTLVE ENTRY, AISLE & STA DRINKING di 1e)ASH WAT ER TAN B REMOVED ' - ‘i‘ • 3. ED 1... i - .. DRAINED EL FILL W V , TY & CLEAN \ • 9. WINDSCREEN STOWAGE EMP 4. HYDRAULIC SYSTEMS FULL ! • •\ . & AFT. LAV. .iitV e<74-2;" ..in• • STOWAGE COMPARTMENTS ON FWD QUANTITY cr ei -•• — . BULKHEADS EMPTY 5. TOILETS SERVICED TO NORMAL le/4yred- G FLOATS SEAPLANES: DRAIN HULL & WIN . • 6. r;2- . COMPLETELY . _ •. 0 CONTROL CABIN POWERPLANT J D. CARGO, LANDING GEAR & - . • .<, TE 1 a c 1. ALL INSTRUMENT PANELS COMPLE ?:)11iA • D kt b r BOOKS, 1. ENGINE FIRE BOTTLES CHARGE i 2 ALL MANUALS; CHECKLISTS, LOG IAL REMOVED CO/ 2//f WR ITTE N MA TER FORMS & OTH ER & 4,er 2 ALL ENGINES COMPLETE I.E., ACCESSORIES, e H SEAT BELTS ALL CREW SEATS COMPLETE WIT PLUMBING, ETC. •- '3. HARNESSES INSTALLED .1//f & 7..riew,' ALL COWLING & PANELS IN PLACE & FLIGHT ENGINEERS TABLE EMPTY i SECURED 4. AN EXC EPT FOR STR ETC HER KIT CLE D. ..r.A. ..- . X 4. 4 BRAKE AIR BOTTLE CHARGE 7 • C. PASSENGER CABIN -P, KS EXCEPT ALL AVIONICS EQUIPMENT INSTAL LED 12• REMOVE ALL ITEMS FROM HATRAC UNT ED OXY. S. , MO 1. • MEGAPHONES, FIRST AID BOTTLES, DEM POUCH O OXY . KIT MAS K & LIFE VES T IN 6 FWD, & AFT, CARGO COMPARTME & CLEANED • NT EMPTY SI. -a` 71, 4"- MAIN OXYGEN SYSTEM SERVICED • 2. ALL PASSENGER SERVICE EQU ' IPMENT REMOVED Xis A 7 ' FULL 7 7 •:' -Not ) FROM GALLEY D • a MAIN BATTERY & AUX. BATTER Y (IF USED) , ,t.). q...N ALL SERVICE EQUIPMENT REMOVE INSTALLED _ 3. FROM FWD. & AFT. LAVATORIES & .-6-.:- : _ & • a CARGO DOORS & FAIRINGS CLOSED . ALL GALLEY AREAS CLEANED . LATCHED ce7:: 4. VACUUM ED nb; ING LL TIRES INFLATED TO OPERAT , 00-- UUMED 10• A PRESSURE ' -9)114-v PASSENGER CABIN CLEANED & VAC &,A) 5. ING _AIRCRAFT READY FOR WEIGH alo , as Ariz Aiil ica 4 h ?VERSO% ISO AIM •••• • • . -•,1/4 • EFTA00277862 4•1w,:‘' FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 27 41 •1 ; .0 • -a :; . ; •• ". . ' .• ' •17 •i'.. -••:14.1:1::S. • ." . • '. •• ••.:- . .. . • , • '• !I ,;•".?.• • • '7. ' . tt• -: ' .i .„ • : ;en,. r.••,;1•:-....c. •• . r '• .r. :.• . .• • • .cr t 4 -e41-4‘ vrk.:-%peroler.44t4;,*. EFTA00277863 Nt h —zwiw awainicmaaTiCOn4041, -r.L. I FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - 27 - 91 • AIRCRAFT WEIGHING Eliereeeen ) MODEL SCALES: MAKE CALIBRATION DATE 5 3 - 9 .0 SERIAL NO. 10(e? • -"FIRST WEIGH CALIBRATION CELL DRIFT TARE NET WEIGHT REACTION SCALE READING CORRECTION LEFT ML INGge 4 7 7 3.5 - -2o -e0- -62- 1/ 7715-- RIGHT "L INGO ° - SO ---662- - - iiY75-0 l igg0 q 3 55- OS AIL Ya 93 `S +10 NET WEIGHT TOTAL 10O1 2T2O 1 / CIRCLE REACTION USED SECOND WEIGH CALIBRATION CELL DRIFT TARE NET WEIGHT REACTION SCALE READING .CORRECTION LEFT MLG 11-7 750 -5-O -79- 41 417 9'OO WING RIGHT MLG ‘//741.0 +10 -69- -re Ile 120 Lt 3(O-5- WING a 6 3 '69' NOSE/TAIL l 'i3 5- NET WE GHT TOTAL 1 00/ CYST th 1 / CIRCLE REACTION USED i 1. WEIGHING COMPLETED Foreman/Lead Mech. Or Inspec 2. WITNESSED & ACCEPTED 0)1444.4-d ICt4.421,4- Chief Inspector Or Designee ROL SECTION. BE ACCOMPLISHED BY THE QUALITY CONT NOTE: PART F. AND SUBSEQUENT PARTS TO NET WEIGHT AVERAGE _ MLG MLG NOSE/TAIL LEFT RIGHT VVING WING FIRST WEIGH 117 715- Li F75-0 1-1-355- SECOND WEIGH 91900 qa'Li 20 113425- TOTAL 956 IS 91/ 7O X72O AVERAGE q 7Sac ggs-75-- 4t3tho CHECKED BY PAGE 2 OF 3 ' EFTA00277864 FAA AIRCRAFT REGISTRY CAMERA NO.3 4/ DATE: 9 - 27 - 97 .6.6. 4 nl . • . . ,,.• . • •, • . . . . EFTA00277865 FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - 27 - 97 DATE 7 70 REACTION MOMENT 11 CIRCLE REACTIONS USED. 2. ENTER AVERAGED NET WEIGHTS 45,4124,6e6.-5- FROM PART F. 41 360 b 200 7-3/, 2. TOTAL AS WEIGHED in.552,5" 925., 27 BEW ITEMS NOT ON AIRCRAF ATTACH SUPPLEMENT IF ADDITIONAL SPACE IS REQUIRED SUB TOTAL ITEMS WEIGHED BUT NOT TO BE INCLUDED IN DEW ATTACH SUPPLEMENT IF ADDITIONAL SPACE IS REQUIRED SUB TOTAL BASIC EMPTY WEIGHT ISC1 CHECKED BY PAGE 3 OF 3 EFTA00277866 FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 91 ••••• • ..• .4, . .. .. If • , c. • •••• .•• _ • ••._t .• E. . • • I • 0 1 i • i ‘1 ‘ ‘ Z: • . • • . . . ... • ....gm ...Ob. • 1 ...E..... . • • 1 • I ; • • • 1 . ',. . • • 1 is . • t • •••••••• A : • ••• dm ..• ... .. ••••• ••• • .....•• • •• ••• ..... • i k . 3 EFTA00277867 FAA AIRCRAFT REGISTRY • CAMERA NO3 A' DATE: 9 - - 97 • t• • : • •• t. ▪, • , • ' • ▪ . . • N. • " • •• • : . .• . • , o . , •- OF AMERICA N Uan TED STATES MIAISTRATIO SP OR TA TIO N. - FE DERAL AVIATION AD AN DEPARTMENT OF TR NESS CERTIFICATE -SPECIAL AIRWORTHI " ' •-• , • PE RI M EN TA L pY / 0ESiGNA TION EX RVEY :• 1.. Y CA TEGO PL IA NC E W IT H FAR / MARKET SU A PURPOSE SHOW COM 3 NA M E N /A . .. _ , MANU- , N /A 6-. FACTURO ADDRES S . • N/A / FROM C FLIGHT N/A ., TO SERIAL NO. 20115, D N- 505C MODEL 727-31 BUILDER BOEING EXPIRY 08-01-90 90 RTIFICATE ARE A PART OF THIS CE -0 1- DATE OF ISSUANCE 05 TE 05-01-90 OPERATING LIMITATIO r NS DA FICE NC: . • ' • DESIGNATION OR OF E SIGNATURE qr F REPRE -108S i SEA-MIDO, ANM eding $1.000 or SON . ble by a line no t ex ce 'MICHAEL J. mi su pu nis ha se of this certificate IFICATE MUST BE DISPLAYED ma y be IN TH E AIRCRAFT IN du cti on or ENFrattOn, rep ro th. THIS CERT Any ceeding 3 years. boRAL AVIATION REGULATIONS. DE imprisonment not ex APPL IC AB LE FE DE SEE REVERSE SI ACCORDANCE WITH FAA FORM itiO4 (loam •z ,•• EFTA00277868 FAA AIRCRAFT REGISTRY CAMERA N0.9 N DATE: 9 - Z7 - A This airworthiness certilicate is issued under the authority of the Federal Aviation,Ac•t of 1958' v and the Federal Aviation Regulations (FAR). • • . '. . . . . This airworthiness certificate authorizes the manufacturer named on the reverse side to conduct production flight tests, and only production flight tests. of aircraft registered in his name. No B person may conduct production flight tests under this certificate: (1) 'Carrying' persons'or property for compensation or hire; and/or (2) Carrying persons notessential to the purpoie of ;'• ..' • • /14., the flight. ...... --.• 1 This airworthiness certificate authorizes the flight specified on the reverse side for,z‘rpo se C shown in Block A. . • • .. - - ' ( .. ' •—•••••••• - .. •. • • • cS,i This airworthiness certificatecertifies that, as of the date of issuance, the aircraft to W. ich issued has been inspected and found to meet the requirements of the applicable FAR. The aircraft does not meet the requirements of the applicable comprehensive and detailed airworthiness code as O provided by Annex 8 to the Convention On International Civil Aviation. No person may operate the aircraft described on the reverse sit (1)except in'accordance with the appliCable FAR and in accordance with conditions and limitation: which may be prescribed by the Administrator as the. special permission of that part of this cer. tificate; . , foreign country without . • - -.any (2) over country. • . ic • • • . . ... E Unless sooner surrendered. suspended, or revoked. this airworthiness certificate is effective for c the duration and under the conditions prescribedin FAR Part 21. Section 21.181 or.21217. . •- - 1.4 rs f EFTA00277869 7 2.Yety sktrir, nos ti r "'Yr FAA AIRCRAFT REGISTRY CAMERA 6,:)..3 iV DATE: 9 - 27 - 97 •4 •VW . " • ar . • . . • • • • .• • •••• . • • •• • • • . . gt. . 4 • 1. U.S. Department of Transportation Federal Aviation Administration Manufacturing Inspection District. Office 7300 Perimeter -Road South Seattle, WA 98108 May 1, 1990 EXPERIMENTAL -SHOW COMPLIANCE WITH FAR's/MARKET SURVEY •\ MAKE: Boeing . MODEL: 727-31 SERIAL NO. 201157: • REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: 1. No person may operate this aircraft for other than the purpose of Show Compliance with the FAR's and Market Survey to accomplish, • the tests outlined in the applicant's program letter dated May 1, 1990 describing compliance with FAR 21.193(d). Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). 2. All flights shall be conducted within the geographical areas described as follows: 1. Western United States of America bounded on the East by the Mississippi River, on the- North by the U.S.A./Canadian border, on the South by the U.S.A./Mexico border, dnd bounded on the West by no more than 200 miles from the West Coast of the United States of America. ! • A 2. Base of operations is Palmdale/Lancaster Airport, i Palmdale, California and secondary base of operation to be Moses Lake Airport, Moses Lake, Washington. 3. The pilot-in-command of aircraft must, as applicable, hold an appropriate category/class rating, have an aircraft type rating, have a flight instructor's log book endorsement or possess a "Letter of Authorization" issued by an FAA General Aviation or Air Carrier Operations Inspector. 4. This aircraft shall not be flown unless it is maintained and opera4-ed in accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. Upon changing between operating purposes of a Multiple Purpose Certificate, the operator shall determine that the aircraft is in a condition appropriate for the purpose intended and has documented that finding in the aircraft log. 6. This aircraft shall contain the placards, markings, etc. required by FAR 91.31. • EFTA00277870 FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 97 EFTA00277871 FAA AIRCRAFT REGISTRY CAMERA N0.3 N DATE: 9 - 27 - 91 • Federal Aviation Administration Manufacturing Inspection District Office Experimental - Show Compliance with FAR's/Market Survey, Cont'd Page 2 of 2 7. The cognizant FAA office must be notified. and their response • received in .writingprior to flying this aircraft after - incorporating a major change. as defined by FAR'21.93. . 8.• This aircraft approved for day/night VFR/IFR only. '"No operations shall be conducted over densely populated areas or in Congested airways except for takeoffs and landings, and when under.ATC control. :10. No person may be carried in this aircraft during flight unless that person is essential for the purpose of the flight while in the Show Compliance category. 11. This aircraft is prohibited -prom aerobatic flight; that is, an intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved by the cognizant FAA office. 12. If aircraft engipe.or propeller operating limitations are exceeded, an.appropriate entry will be made in the historical records. 13. After the aircraft has been re-engined, the pilot-in-command must make a log book entry stating the aircraft complies with FAR 91.42(a) and FAR 91.42(b). Mic ael J. son Aviation Sa ty Inspector (Mfg) SEA-MIDO, ANM-108S These limitations will expire on August 1, 1990. J1 EFTA00277872 -ti r cs '0. r. 4: kith- ••• • • .7, • ^ • .a.•••••:. •• .• _ EFTA00277873 , Form Approved • .. • OMB No. 2120-0020 uSDecianrrient MAJOR REPAIR AND ALTERATION of nomoonction (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Peen MiatiOn Office Identification Administration 7A/y gsad INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instruction s and disposition of this form. This report le required by law (49 U.S.C. 1421). Failure to report can result in acilejl penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). RECEIVE[} FAA Make Model BOEING 727-100- 1. Aircraft Serial No. Nationality and Registration Mark jUi 2't L-9.0 • 20115 N505C Name (As shown on registration certificate) 1/14Y 11;[)() Address (As shown on registration certificate) 2. Owner . -1409 Foulk Road, P.O. Box 7138 NORTHWEST HOLDING CORPORATION Fpulkstone Plaza, Suite 102 Wilmington, "Delaware 19803 3. For FAA Use. Only - - _ • . 4. Unit Identification 5. Type . , . Unit Make ' Model - Serial No. Repair Alteration — .. . AIRFRAME (As _described in Item 1 above) - X • POWERPLANT, - PROPELLER • • - -- .--- - ---- _ _ ___ • Type APPLIANCE Manufacturer • t - - - - • ' 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. North AHL.-ican Aircraft U.S. Certif cated Mechanic Airframe Class 4 Rockwell International Corporation Foreign Cen baited Mechanic LiMited Powerplant 2825 E. Avenue P X Certificated Repo I Station Class 3 Palmdale Ca. 93550 • Manufacturer NXAR688K • D. I certify that the repair and/or alteration made to the un t(s) identified In item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43.of the U.S. Federal Aviation,RegulatIons and that-the infornation furnished herein is true and correct to the best of my knowledge. i / Date Signature of Authorized Individual • . July 20, 1990 D. A. Perazzo kJ 7. Approval for Return To Service j Pu suant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the , Administrator of the Federal Aviation Administration and is cg. APPROVED :-.7. REJECTED !. FAA Fit. Standards Other (Specify) • Inspector Manufacturer I Inspection Authorization • BY FAA Designee x Repair Station Parson Approved by Transport Per (Th Canada Airworthiness Group i I l Date of Approval or Rejection Certificate or Signature of Authorized Individual i Designation No. July 20, 1990 NXAR688K U. A. Perazzo h . .' . .. ,..._. i- FAA Form 337 ti y Hsi t, t EFTA00277874 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. - - B. Description of WorteAccornplIshed (It more space is required, attach additional shoots. identify with aircraft nationality and registration mark and date work completed ) A. Modified Boeing Model 727-100 , Serial Number 20115, in accordance with supple- mental type certificate SA4363NM, amended September 1, 1989 as follows: 1. Valsan-Boeing 727-200 Re-engining Document VA000001, Revision F, dated January 15, 1990. 2. The following drawings and engineering orders (E0's) are in addition to the above document:: NOTE: "VA" denotes Valsan Drwing. a. Chapter 24 ELECTRICAL POWER VA240000 A Electrical System Instl. - Strut E.O.: 003A, 101 VA240007 E Panel-Load Control Center Modification E.D.: 003A, 004, 005, & 006 b. Chapter 28 FUEL SYSTEM INSTALLATION, STRUT VA2-80001 B Tube Assy - Fuel Strut Feed Thru E.O.: 100 c. Chapter 48 MISC VA481100 A Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 VA481200 C Frame Assy Sta 1263 E.O.: 101, 103 VA481300 C Fuselage Skin E.0.: 106; 114A, 114, 116 VA481324 NC Intercostal Assy — BSTA 1223 to BSTA 1243 W/L244.39 E.0: 106 VA481325 NC Intercostal Assy - BSTA 1223 to BSTA 1243 W/L234.0b E.0: 105 d. Chapter 53 FUSELAGE STRUCTURE VA530001 B Ballast Weight Installation E.0: 100, 102 VA530003 C Ballast Weight, Support Structure Assy. E.O.: .002,100 VA530004 NC Ballast Weight Instl. STA 312 - 360 E.U.: 002, 100 e. Chapter 54 NACELLES & PYLONS VA543000. C Main Strut Assy (Sh. 1, 2, & 5) E.O.: 003 VA543100 D Firewall Rib, Side Engine E.0: 36A, 003A f. Chapter 71 POWER PLANT VA710000 NC Power Plant Instl. - Engine Pod V727RE E.O.: 002, 105B, 109, 108, 001A, 104A, 005A, 004, 110, 003, l ii, 006A Chapter 73 ENGINE FUEL AND CONTROL VA732301 K Approach Idle Solenoid Wiring Diagram E.0: 002(Rev L), 002 (Rev. M), 003(Rev. M) VA732303 D Relay Instl. - Approach Idle Solenoid E.O.: 103, 003, 100B VA732304 D Switch/IND Light Instl - Approach rdle E.O.: 002, VA732310 A Switch Instl. - Nose Gear Position Approach Idle E.U.: 103 VA732315 NC Relay Instl. Pilots Overhead Panel E.O.: 100, 002, 101 h. Chapter 76 ENGINE CONTROL tA760000 A Engine Controls Instl. - Strut E.O.: 002A VA760014 A Drum Instl. - Eng. Controls E.O.: 100, 101 VA760015 A Bracket Assy - Pulley ESTA 100 E.O.: 105 g Additional ',.neets Ard Attached .U.SCIP(11989.0.600 71 y'` - • EFTA00277875 k -` • AAYft'GtA` t, • CANER!. 7 D. I.N DATts 2 g • Itt DESCRIPTIQN OF WORK ACCOMPLISHED (tontinued) :;"11 . i.- Chapter 77 ENGINE INDICATING - VA771005 NC Indicator Engine Pressure Ratio EPR, E.O.: co! Chapter 78 ENGINE EXHAUST VA780000 B Engine Strut controls:'Instl..E.O.: 002. . • VA783010. E )Flt Deck 'Indicator Instl T/RSys. E.0.L.003, 004 VA783011 F Thrust Reverser System Wiring. Diagram 002'(Rev. G) VA783013 D :Support Bracket AsSy:=:T/R'COntrOl Valve R/S 100 (ReV. E) VA783017 J' •Placards*E.O.:pp,0308 VA783024. 'Relay Instl.. -. ThruStReverter Control E.O.: 003': VA783028 A .:Mixer, Exhaust -‘ Instl..727E.10.: 100 • VA783101 C. • No. 2 Engine TM Wiring Peactiviation E.O.: 002 - k. Chapter 91 CHARTS VA910002. A Instl. ElectriCal Wire Harness E.O.:. 003, 004, 005, 006, 007 * VA910008 NC Wire List V727RE E.O.: 001, 002, 003 *New driwings added to modification. B. Boeing 727 Service Bulletin 72753A0171, *dated December'14, 1989. Subject: Fuselige - Station 1182 Pressure Bulkhead Web, • Crack Repair'and Preventive Modification . • C. The. aircraft empty weight and center of.gravity was revised in accordance with Boeing Weight and Balance Manual D6-21200. . Weight and Balance Manual Supplement, VA-CR279' •is attached. EFTA00277876 '“义〉: !! ， 一一一 r IIl Ik 榦攥私＞,} ：一． ： · 一 l I I. 討 一 I 一 F- r f - . 'l I EFTA00277877 29 1991 0.t" q. No.212J-0018 0 . , - -- APPLICATION FOR INSTRUCTIONS-Print or type. Do not write in 'laced antes: these are kr vs.,' use only. Submit Oulnal only to aniauthorized FAA Repreientalow. II additional us orpslinorr a lionwiu.ion • AIRWORTHINESS space is required.-usean attachment. For special fl ght porn. Is complete Sections Fecteral Mahon CERTIFICATE It and VI or VII as applicable. earrenraranon 5" 010't S 1.REG.STRA 2.AIRCRAFT BUILDERS NAME (Mew 1 AIRCRACT MODEL DESIRNATIOI4 - .ift 1 MA .• ttk I. AIRCRAFT I. AIRCRAFT SERrAL NO C. C 50 Eti U 6 . 6. ENGINE BUILDER'S NAMEThaikci 72 7 — Avaritspi,4-> /..i.3 I. ENGiNi .MODEL DESIGNATI - O. arc -tee_ . ❑ESCRIPT1ON 0 7. NUMBER OF ENGINES / /S. si ti fte IL) . O. PROPEL!, ER Still pr.11- AME AL .-; Br> .1-. .7 A - 9. *ROPE ..1.5 R MODEL 0ESiGNATION 21 et 10. AIRCRAFT iS (Crack ii SODiatit, _,..3 • all . ik._>I / I 'IMPORT APPUCATION IS HEREBY MADE FOR: (Cheek atftlicible iremsi. ' le. A V ' STANDARD AIRWORTHINESS CERTIFICATE Umlaute carvuo., . iit i•••••••O I jUliLITY ACROBATIC] 1 TRANSPORT 1 _1 GLIDER BALLOON L B SPECIAL AIRWORTHINESS CERTIFICATE (Check app. onique din!. \ 2 LIMITED .- 1 - - G.ASS I S PROVISIONAL (indicatekraal 1 2 . • -CLASS II • g 0 AGRICULTURE AND PEST CONTROL 2 AERIAL SURVEYING $ AERIAL ADVERTISING se CC . 1 . RESTRICTED/Indicate operehon(0 ID FOREST (Wareile conservahwq II WEATHER CONTROL • 3 PATROLLING : ' O Os co/Murat:ft • • - 1 • •• • . 7 CARRIAGE OF CARGO 0 OTHER iSpecdp/ ' • . RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT .3 EXHIBITION 1 i .. A EXPERIMENTAL (InditeM Operettor(s) to De ccoducted) - . .- . )itk RACING S CREW TRAINING N MKT. SURVEY •' bi TO SHOW COMPLIANCE WITH FAR d ' • • • - • 1 FERRY FLIGHT FOR REPAIRS, ALTERATIONS. MAINTENANCE OR STORAGE SPECIAL FLIGHT PERMIT (Indicate 2 EVACUATE FROM AREA OF IMPENDING DANGER • . operation to be conducted. then i c. OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKEOFF WEIGHT . • complete Section VI or Vil es. • — ' - i - ' • applicable on mites saes: • a DELIVERING OR EXPORT 1.51 I PRODUCTION FLIGHT TESTING $. CUSTOMER DEMONSTRATION FLIGHTS C 1 MULTIPLE AIRWORTHINESS CERTIFICATE (Check ABOVE -Restricted Opera)ion- and 'Standard' Or linuted.- as applwablej A. REGISTERED OWNER (Ar shown on cashier-aloof aircraft registration) IF DEALER. CHECK HERE I ... rat PCS-Vole PA4 VA 15 cale era,Ai? rater koAn NAM!, ADDRESS ... • • , ,s90 Cenp Ay on. N10 41-44650-61" ge,LAI Ws. ,( e • 61.6.lei 1I3t tor Lws W6-Tew beAsioa ilIo3 A. AIRCRAFT CERTIFICATION BASIS (Check applicable blocks and complete arms as indica ad) g - AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE DATA SHEET (Owe No. AIRWORTHINESS DIRECTIVES (Chock it all inviable AD's complied with end wee latest AD NO.1 P and Revision No.) 3 SUPPLEMENTAL TYPE CERTIFICATE (List number °I each STC incorporated) F AIRCRAFT USTING (Give page number(s)) I.0 C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS . • . I bi CHECK IF RECORDSIN • TOTAL AIRFRAME HOURS EXPERIMENTAL ONLY (Enter hours flown since lest certiliiiale COMPLIANCE WITH FAR 91.173 Pf gg'ie 2 •. . --., iF ilT ikkE issued or renewed/ /9, g 0. CERTIFICATION — I hereby Willy thal I m the registered owner (or his earl) Of me airalft desCribed abort that IN aircraft is registered with the Federal Aviation Administration In accordance with Section 50 of thefts:Mt Availed Act cal 1958. and applicable Federal AviatiorilleguLshons and thal I he Sucre II hes beer nine salld .1. . - . .. aftworthy and eligible (or the aliworthine se certificate raquesiat - -" • . DATE OF ORLI,. ATION . " NAME AND TITLE (Print or type) rue SI • Si/ 19 10 • I ....t • ... (02441.17- • / ?KA. 7 - A. 710 AIRCRAFT ESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Carnivore retie 'capon onty if FAR 21 183W) epphesl Z z 0 0 . FAR PART 121 OR 127 CERTIFICATE HOLDER (Try ai CERTIFICATED MECHANiC (Owe . - CERTIFICATED REPAIR S(Al-ION:6,n Ceihhcaiii 5 r; r 'Tr:7, Certificate Nal . . . (O Culibcito No.) Ar t No.) t 61 itli\ ° 0 C ! •€ I tili • XIPITRAFT MANUFACTURER/0Niahem* Of thin) i! i • DATE TITLE. i .,: . SIGNATURE • (Check ALL applicable blocks in items A end% .' 1 THE CERTIFICATE REO 'ESTEE, A. I find Om the aircraft described in Section I or VII male reiediremente lot, ot AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE • 1 ?.1 3 DATE g B. Inspection tor • special Mght pernalundir SectiOn VII -, was conducted bir . •• • ., i FAA INSPECTOR CERTIFFCATF HGIOER UNDER: FAA DESIGNEE FAR 55 I 1FAR 121. 127 0 1351 1FAR 145 . DISTRICT.OFFICE - " DESIGNEES SIGNATURE AND NO ., . . AA INSPECTOR'S SIGNATURE s g .' S EFIV" Altb0 ' • . . ' • a 45:61 49° ANAT .1649S .- 40 • . , 1 FAA Conn 81304 (1243) SUPERSEDES PREVIOUS EDITION ' . 74,..ite. • • EFTA00277878 &MANUFACTURER. NAME ADORPCS VI. PRODUCTION , - • - ` . . B. PRODUCTION BASIS (Chock epootabie hemp PRODUCTION CERTIFICATE (Gee prOducUon creficate number) FLIGHT TESTING TYPE CERTIFICATE ONLY , APPROVED PRODUCTION INSPECTION SYSTEM C. GIVE QUANTITY OF CERTIFICATES REQUIRED FOR OPERATING NEEDS DATE OF APPLICATION NAME AND TITLE (Print Or type) SIGNATURE A. DESCRIPTION OF AIRCRAFT T REGISTERED OWNER ADORES.) BLIILOER (Make) .. MODEL . • SERIAL NUMBER • REGISTRATION MARK ,:' •- • • . .. • N .. .... . • .• • . ' ,, . . • . I B. DESCRIPTION OF rucirkr.... • . ' “. ..._.. 4 &STORER DEMONSTRATION WORTS 0 tailor It sPOliceloW FROM ---• ...- VIA DEPARTURE DATE - • • DURATION , VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER THAN PRODUCTION FLIGHT TEST .. -_, .. '. C. CREW REQUIRED TO OPERATE THE AIRCRAFT AND ITS EQUIPMENT,. • I 'PILOT , I I COPILOT : I I NAVIGATOR • I I OTHER (Specify) • D. THE AIRCRAFT DOES NOT MEET THE APPLICABLE AIRWORTHINESS REQUIREMENTS AS FOLLOWS: • . - • ••. ..' .... . ... • • i . — . .. . . ..." . . . .. • ' -• " - " " •- •' • .. • - 1'1 " •"' -r _. . .. • .i .• : . • .. • •.. .. . . ..... .• • •• . • it . .... .. - • .. - ,. _ - .... . . .. , - . .- .. . . _ •• , -- - E. THE FOLLOWING RESTRICTIONS ARE CONSIDERED NECESSARY f OR SAFE OPERATION (use attachment il necessary) ... .. . . • . ... . . .. — . . - '•. - - .. . . • .. . • ' -• • • „. • - • r . . . .. . .,. . _ • .- . S ... : . . • • • • F. CERTIFICATION —1herebyceiThlty ItIM larrf the Ng'marathoner (Or Ms agent) of UmaIrcraft deseribidabovir.trail the aircraft la registered wishIh•Federal Aviation Administration In accordance with Section 601 of the Federal Aviation Act of 1956. and applicable Federal AviationFlegulations• and the Sircratt has ban inspected and Ii airworthy for the flight described. ‘, • • '• ' .• : • •• • . DATE •• , NAME AND TITLE (Pant or rypej: • N. SIGNATURE . . . . .. • .... Operating Limitatiora.and Markings in "replant, with FAR • CL,Stisteinent of Confcetnity, FAA Foim 11130-9 (Attach when required) V 2.„ 91. 1 as pUcable i I . H. Foreign Airworthiness Codification for Import Airc.A i ve B. Carron' Operating Wildfire Attached% i •• N. ' .. . . . --" .f Attach . . .when. required) . . "'--: t. i 4I I Pnnious Airworthiness Certificate Issued In Accordance with 3Ci ag 4 a/ C. Data. Drawing's, photographs. fit (Almon when foqukocl) . D. Current Weight end Balance Inlonnation Available In Aircraft ' ' • • E. Major Repair find Aberration. FAA Form 337 (hhech'When *end) • • 4 ' . FAR 2/. 191(b) •L Current Airsortinnere Certificate Issued i Accordance with CAR (Original Attached) F keir F. This Inspection Recorded in Aircraft Records . 4 • Fan 21.1910)) g n4 Q?) (Copy elisched) ' -prewar3`.11.,.. • • . • • EFTA00277879 EFTA00277880 .• . A This tirWrihlillieseterlikat° isisSbettlinderikaltitilti.6*ofthe FikieratAyifttiCal AO Of 1958 , ^ antl the Federal Aviation Regulations (FAR). • This alrworthiness certIficate authoreesthe fated* narittid On thereireMeS idet0 donduct production flight tests, and only production Ng 11631.1:61aircraft registered in his name. No ' B person may conduct production flight tests linderithIS certificate: (1) Carrying persons br property for compensation or hire; and/or (2) Carryingpersonsnot essential to the purpose of the flight. . - ' . . . This airworthiness certificate authorizes the flight speCifted on the reverse side for the purpose C shown in Block A. .ii—i ...... This airworthiness certificate certifles that. es of the date of Issuance, theaircraft towhich issued has been inspected and found to meet the requirements of the applicable FAR. The aircraft does not meet the requirements of the applicable comprehensive and detailed airworthiness code Es n provided by Annex 8 to the Convention On International Civil Aviation. No person may operate o the aircraft described on the reverse side: (1) except in accordance with the applicable FAR and in accordance with conditions and limitations which may be prescribed by the Administrator es part of this. certificate (2) over any foreign country without the special permission of that country. . % . • Unless sooner surrendered , suspended, or revoked, this airworthine ss certificate is effective for E the duration and under the conditions prescribed in FAR Part 21. Section 21.181 or 21217. 4•11 1. EFTA00277881 . Form Approved 0 M R. No. 2120-0016 a - INSTRUCTIONS — Pnnt or type. Do not write in shaded areas: these are for FAA APPLICATION FOR - J • on cmly. Submit original onty to an authorized FAA Representative If additional AIRWORTHINESS .- . 0 US Deponmere - SPaCetarteuired, use an attachment. For special flight permits complete Sect. 0ns at Ihrepcnohon -i CERTIFICATE • • 13 end VI or VII O applicable. Fedora kakilion Admisercassin - .. I.REGISTRATION MARX ZAIRORAFT GuiLoeyrs NAME WON . }AIRCRAFT momDESIWiATiON b..W4!' s.:. " — g I. AIRCRAFT iL) SV S e< . CSO Et.)06 • 727— )00 . Et. ENGINE BUILDERS NAME Wakes &ENGINE NODEL DESIGNATI , I. AIRCRAFT SERIAL NO. DESCRIPTION i. 0 / 15 Pee be.) - Ji ll 8M ) In' "sk 219 •-.:;":..:. ---- . 1. NUMBER OF ENGINES CPROPEU.ER ISUIL7A Ale MOW A PROPELLER MODEL onsGNATION. ok 10. AIRCRAFT IS rCoock it •orhcicv, IMPORT ..... APPUCATION IS HEREBY MADE FOR: (Crum solikeeDrit items/ - • A :I: STANDARD AIRWORTHINESS CERTIFICATE 'Masco re category(' 'NORMAL' I UT1UTY I 'ACROBATIC' 'TRANSPORT GLIDER i8At.i.00t4 8 `..P Y. SPECIAL AIRWORTHINESS CERTIFICATE (Check stonsonett MIM) LIMITED • L • it; cuss i •• . II. CERTIFICATION REQUESTED tri i PROVISIONAL /inmate clan) . at. III . • AGRICULTURE AND PEST CONTROL '::: AERIAL SURVEYING -;,3. AERIAL ADVERTISING z••• RESTRICTED (Immure operations to p66 FOREST (WSW ecoservamml .4: .. PATROLLING .e WEATHER CONTROL : 3- ., . „ y. De committed) tit i 'CARRIAGE OF CARGO . . ilf- OTHER (Speedy; j • RESEARCH AND DEVELOPMENT ...' B. AMATEUR BUILT .•- 3 EXHIBITION 9 • EXPERIMENTAL ihNOVIIO operation/ s i .:• ‘44I RACING 40 . CREW TRAINING X MKT SURVEY 4o PO cOnductodi • TO SHOW COMPLIANCE WITH FAR ' 1t .7. " 4 tit e FERRY PLIGHTFOR REPAIRS. ALTERATIONS. MAINTENANCE OR STORAGE '2 EVACUATE FROM AREA OF IMPENDING DANGER SPECIAL FLIGHT PERMIT ilndcalo °pew/on to be conducted illy.: ''.:3 OPERATION IN CXCESS OF MAXIMUM CERTIFICATED TAKE-OFF WEIGHT cc-nplele Sedan VI or VII as ti applicable on reverie idea B DELIVERING OR EXPORT .61 IPRODUCTION FLIGHT TESTING • .74.. CUSTOMER DEMONSTRATION FLIGHTS applicable.) C PS. I MULTIPLE AIRWORTHINESS CERTIFICATE (Check ABOVE liestnaml Oraranner end -Steislare or -Lveded. 'as ' J..; IF DEALER. CHECK HERE ----w- I "'t A. REGISTERED OWNER (As shown on certificate of welsh npistrstion) Foil tecs-Ries Pi-4?-4 1 WM kh1,11419 ;tentletAti NAME ADDRESS $ 1,g 1. On . NOttilAuti261 1401-0tOtr t 0-400 0rp iTiawns 41 .64Pti MT &.k IAA 1M6-7,P1 Wfrigintha irfff03 as in dicated) t B. AIRCRAFT CERTIFICATION BASIS (Cheek applicable blacks ana comps. AIRWORTHINESS DIRECTIVES (Chest 4 all amicable AOS merged WWI and give AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE Diri A sliEET (Give Na latest AO No.) g end Revision Na) . : . .t 9 SUPPLEMENTAL TYPE CERTIFICATE lbw rhimber OleeCh STC income/area. 14* AIRCRAFT LISTING (Give aga number(sc • 5 . C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS • d or EtPERI ,3A ..8j MEN ,sil.o.,..ince,„„cesid.coe 8„ / 76::::„ OINLY (E TALad tenn CHECK IF RECORDS IN TOTAL AIRFRAME HOURS 0 / COMPLIANCE WITH FAR 01.173 . . PI' .,gs-1, 2.: " the @naafi daunted above: MN the sworn tiered with the Federal Aviation D. CERTIFICATION — I hereby cattily that I am Me registered owner far his agent) Of Friferst Aviation Regurabons, and mat eve we has been inane and es Administration in accordance with Section 50 of the Federal Mutton ANY IEEE. rdappliCable .% . ' • &moiety and eligible for the einvorthinna madam reauested. . . - - • •• . • . DATE•OF APPLVATI0N / NAME AND TITLE/Penaor tysiN . 5/ / 7— , 9c• .:.- er-1 . tati4•41-7 ._, - eat..Owhen IV. INSPECTION A THE AIRCRAFT ESCRII3ED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY .{.1, FAR PART 121 OR 121CERTIFICATE HOLDER (Om Certificate No.) • % BY: (Complete Ma CERTIFICATED MECHANIC (One . Certificate Nat only it FAR 21. WWI Aghast • . CERTIFICATED REPAIR 5 ANON (Give Certificate Nal AGENCY trot rit AIRCRAFT MANUFACTURER (Give nem or Wm) VERIFICATION TITLE SIGNATURE s DATE - Niems .-"IeN • aw.. THE CERTIFICATE REOUESTE9 (Check ALL epplecebte Mocks In items A endial ' i. A. I lend that me aimreh described In Section I or VII meets (immanent* for. AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CEMIFICATE .7.>1 FAA DESIGNEE -a FM INSPECTOR, cs a. Inspection tor a special MgM permit under Section VII set i.8. conducted by: was CERTIFICATE HOLDER UNDER: FAR 6S , ' FAR 121. 127 a1351 1FAR tits . DISTRICT OFFICE DESIGNEE'S SIGNATURE AND NO. I- 1- AA INSPECTORS SIGNATURE 47 DATE • •. 2. i g SEA-Mtbc, . 4$ Jr • ri -4V. i Q5-6/-90 mmeic • ias .. FAA Form 8130.6 (1243) SUPERSEDES PREVIOUS EDITION • • •e z • I% e t-c=' ..- • 5'11•• /A' •` - y,Y A•St • r-. • - • ti . •r• A • EFTA00277882 老汹一d ．亡．- 一一：7 一： 一一 L3．一一・．一一c EFTA00277883 VALSitikkaktliEtts_:. . 3014 .Westcheiter :Averiue Purchase's, N.Y. :10577 ..• (914)":694-3600 I. May 1, 1990 FAA, `ANM"1085 . 7300 Perimeter Rd. Seattle, WA 98108 • :Dear Sir, '• Attadhed is FAA form 8130-6, Application for Airworitaneths ...Certificate, for adding "Market Survey° to the authorized operations of our Experimental Airworthiness Certificate. The aircraft is a Boeing 727-100 which has been retrofitted with P & W JT8D-219 engines on 'the POD positions and -7B in the center position. We have flown the aircraft approximately 17 hours under the presently issued Experimental Certificate.S We are requesting "Market Survey" so that we may take a TV reporter and cameraman from Paine Field, Everett, Washington to Grant County Airport, Moses Lake, Washington on 1 May 1990 for demonstration of the- Stage IIV Noise Characteristics:.. ' .The duratiOn of the "Market •Survey" portidn of this .Experimental Certificate :will be only. :for `the. one, flight' from Paine Field to Grant County Airport. The: certificate will then revert to "Show Compliance with FAR's" 'until expiration of the certificate on. ,1 August. 1990. • -ze EFTA00277884 V rr-re,ar,PKv-, a•ALL.... • • - EFTA00277885 -FAA. AIRCRAFT REGISTRY CAMERA NO. N DATES 02- gi 4,At,r14.,Ac:t USDepartment ;• , of Transportation ' Federal Aviation Administration Manufacturing Inspection District Office 7300 Perimeter Road South Seattle, WA 98108 May 1, 1990 EXPERIMENTAL- SHOW COMPLIANCE WITH FAR's/MARKET SURVEY MAKE: Boeing MODEL: 727-31 SERIAL NO. 20115 REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: 1. No person may operate this aircraft for other than the purpose of Show Compliance with the FAR's and Market Survey to accomplish the tests outlined in the applicant's program letter dated May 1, 1990 describing compliance with FAR 21.193(d). • Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). 2. All flights shall be conducted within the geographical areas described as follows: 1. Western United States of America bounded on the East by the Mississippi RiVer, on the North by the U.S.A./Canadian border, on the South by the• U.S.A./Mexico border, and bounded on the West by no more than 200 miles from the Wedt Coast of the United States of America. 2. Base of operations is Palmdale/Lancaster Airport, Palmdale, California and secondary base of operation to be Moses Lake Airport, Moses Lake, Washington. 3. The 'pilot-in-command of aircraft must, as applicable, hold an appropriate category/class rating, have an aircraft type rating, have a flight instructor's log book endorsement or possess a "Lgtter of Authorization"\issued by an FAA-General Aviation or Air CaYrier'Operations Inspectbr. , 4. This aircraft shall not be flown unless it is maintained and operated in accordance with .Boeing-Low Ut'Jlization Program, I/A/W FAR 91.169(f)(4). 5. Upon changing between operating purposes of a Multiple Purpose Certificate, the operator shall determine that the aircraft is in a condition appropriate for the purpose intended and has documented that finding in the aircraft log. 6. This., aircraft shall contain the placards, markings, etc. required by FAR 91.31. -st • '7 - EFTA00277886 , Federal Avia ti Manufacturing on`Administration Inspection Dis trict Office Experimental - • Show Com,plian • - Page 2 of 2 de with FAR's/M - arket Survey, Cont'd 7. The'Lcog '.received'in nizant FAA office Must'be .n o • incorporat writing prior to flying'th tified and their response ing a major c hange as defin is aircraft after' ed 'by:FAR 21. 8. This aircraft 93. approved f(* .i tair/night VFR/I • 9. No operation FR only. :or in congest s shall be'cond - under ATC c e d. a i rways excejy uCtid . over densely populat tfOr.takeoffs e ontrol. and landings, d areas and when ' 10. No pers on that person is may be carried in this‘airc ' Show Compli .essential for rait during fl ance category t h e p u rp oie of the. flig ight unless . ht while in t he '11. Thib ai rc intentional m raft is prohibited from ae an ro attitude, an a euver involving an abrupt batic flight;sthat is, an necessary for bnormal attitude or abnor change in the aircraft's normal flight ma Office. unless approv l acceleration not ed.by the cog nizant O' A 12. If aircra exceeded, an ft, engine or propeller op appropriate e e records. ' ntry will be m rating limitations are ade in the his torical 13. After the must make a lo aircraft 'has been re-engin g book entry e 91.42(a) and stating.the ai d, the pilot-in-command FAR 91.42(b).. rcraft complie s with FAR Mic ael J. Aviation Sa -t y SEA-MIDO, ANM- Inspector (Mfg) 10SS These limita tions will exp ire on August 1 , 1990. EFTA00277887 VALSAN PARTNERS . 3014 WeatcheAtet.Avenue Purchase,'Na.- -10 5 ' • . f914) 6943600' 77.. May 1, FAA,\ANM-74.08S.: , 7300 Perimeter:Rs:I.e.: .Seettlei:WAH 98108- AttaCiled is; FAA form 813076,. Application for Certificate for adding "Market . Su - Airwerthibeea. operations of our Expeii rV ey " .to the authorized mental Airuorthihess: Ce . rtifibate. . . . -• - The aircraft'is a Boeing • - • 727-100...Whibhhas been re P & W.JTBD-219 engines on trofitted with the POD pOsitiOnS•And -7 position. We have flown 8 in the center the aiicraft'AppiOximate the presently issued ly 17 hoUrsunder Experimental Certificate. We are requesting "Marke t Surveil." so that we may and cameraman from Paine take a TV reporter Fie10,-EverettOiashingi Airport, Moses Lake, Wash oeto'Grant County ington .Oa 1 May 1990 fo the Stage Noise Characteristics. .; rsaemenstration of s The duration c.of'the "Market Survey.". _ Certificate will be only of Experimental for the one, flight'fiom. Grant County Airport. Paine Field to The. certificate will'the Compliance with FAR's" un nrevert to. "Show til expiration of the ce 1 August, 1990. . rtificate. on: • Sincerely yours, EFTA00277888 诞 EFTA00277889 FAA. AIRCRAFT REGISTRY CAEERA ICO„ iN DATE: 2 — — et,..aar- 51 a .4 tia*. (FL st, t‘ 4:5'n YAtEstmmakibik 'DERARTmENToFTRANSPORTATION-FEDERALAVIAYIDNADMINISTRATiolt1 SPECIAL AIRWORTHINESS CERTIFICATE Any eh on, reProduction or misuse of this certificate ma exceeding 3 years, or tinik /table by a fmc not exceeding S L000 or imprisonment o THIS CER11FICATE APPLICABLE FEDERAL MUST BE DI LA YED IN THE AIRCRAFTIN ACCORDANCE WITH AVIATION REGULATIONS FAA FORM 0130-7 (7-70) USE PREVIOUS EDITION `Y:epterr'r let ter . • . - ••' EFTA00277890 EFTA00277891 Manufacturing bispection District Office. 16501 SherinanWayi—Suite 200 407 Van Nuys, CA .91406 . . US.Departant of Transportation Federal Aviation Administration February 2, 1990 EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's 3-4 MAKE:'Boeing MODEL: 727-31 SERIAL NO. 20115 REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft mustbe operated in accordance with the following Iimitations: No.person may operate•this .aircraft for--other than-the purpose of Show Compliance With the FAR's to accomplish the tests outlined in the applicant's program letter dated February 2, 1990 detcribing compliance with FAR 21.193(d),_Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). ' • 2. All flights shall be conducted within the geographical areas described as. follows: ' 1: Western United States of America bounded on the East by the Mississippi River, on the North by the U.S.A./Canadian.border, on the South by the U.S.A./Mexico border, and bounded on the West by no more than 200 miles from the West Coast of the United States of America. 2. Base of operations is. Palmdale/Lancaster Airport, Palmdale, California and secondary base of operation to.be Moses Lake Airport, Moses Lake, Washington. 3. The pilot-in-command of aircraft must, as applicable, hold an appropriate category/class r tin , aircraft tYPe rating,..have a flight instructor's --""166 -bboirentibitVme ss ss1"1:etter of Authorfiationft-issued'by an FAA General Aviation or Air Carrier Operations Inspector. ' 4. This aircraft shall not be flown unless it is maintained and operated in . accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. This aircraft shall contain the platards, markings, etc: required by FAR 91.31. 6. The cognizant FAA office must be notified and their response received in writingprior to flying..this aircraft after incorporating a major change as defined by FAR 21.93. . 7 This aircraft.approved.for day/fiight:VFR/IFR only. EFTA00277892 FAA, AIRCRAFT REGISTRT CAT:ERA NO. I DATE: 02. g s , "Fedelll AViAtiott AdidiAittiatia Manufacturing Iiiipectitid Oistrii*Offitt-- Experimefital - Show CompliaNdi'With cdntsd Page 2 of 2 % 8. No operations shall be conducted over densely populated areas or in :congested-airways except for"takeofft and landings, and when under ATC control. 9. No person 'may be carried ,ip:thisaircraft dUring flight unless that person is essential for the purpose of the flight. 10. This aircraft is prohibited from aerobatic flight; that is, in_ intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved by'the cognizant FAA office. 11. If aircraft, engine or propeller operating limitations are exceeded, an apprdpriate entry will be-made in the historical records. 12. After the aircraft has been,re-engined, the pilot-in-command must make a log boOk entry stating the aircraft complies with FAR 91.42(a) and FAR.91.42(b). bert Stagg R-48-AC-NM 'These limitations will expire on August 1, 1990. ;,..;••• ect.,:gm te**""r ...‘4!‘ '‘';'N"te.00.6frte4i0,44:'""--"- `: • EFTA00277893 FAA AiRCRAFT.REG1STEE CA? ELA WO. i. ,tr DATE: 2-21- 9 fd mow...—...a.,--... dir:ah. 0.••••••••••••.. • •- • •-• rt, . Form Approved 0 MAJOR REPAIR ALTERATION • OMB No. 2120-0020 as scruDortaucc LISIDevortinem . (Airframe, Powerplant, Propeller, or Appliance) For FAA Use On:y Pearce Aviation Acteriatishotion • • . . .... . . ' . • Office Identification ,S0 - Fs a 0 --/sr INSTRUCTIONS:Print or type all entries. See FAO 43.9, FAR 43 Appendix and disposition of this form. This report is required by law (49 U.S.C 1421)'land AC 43.9-1 (or subsequent revision thereof) for instructions for'each such violation (Section 901 Federal Aviation Act of 1958) . .Failure to report can result in a civil penalty not to exceed $1,000 . Make • Model . I. Alrcraft Boeing B727-31 Serial No. • • • Nationality and Registration Mark 20115 N5 0 OLS - Name (As shown on registration certificate) Address (As shown on registration certificate) Owner 2. • Vor.. thweS€ Holdin •• • • g •.Corporation - .. P.O. Box 7138 • 1. . Wilmington, DE 19803 3. For FAA Use Only - ‘ • .• - -- ;.•, . • .• - . ., . .. .-- .• . ,- : . . _ „ .„.. . ,.. • • 4. Unit Identification 5. Type • Unit • Make Model Serial N9. Repair Alteration AIRFRAME .... Os described in Item 1above) • • •• X POWERPLANT • - ., . \ • PROPELLER • s• ----7N • Type • • .: . • .. . APPLIANCE . - Manufacturer • ( -,._ 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated Mechanic Page Avjet Corporation . Foreign Certificated Mechanic 9809 Tradeport .13r4ye '. A Certificated Repair Station Orlando /a_ Florida 32827 . OS4R425M • _ Manufacturer D: I certifAhat the repair and/or alteration made to the un t(s) identi have been made in accordance with the requirements of Part fied in item 4 above and deicribed on the reverse or attachments hereto furnished herein Is true and correct to the bested my know 43 of the U.S. Federal Aviation Regulations and that the information . e. Dal.) • . • • . gnature of Aut Individual . .. .. 7. Approval for R urn To Service • Pursuant to the authority given persons specified below t, Administrator of the Federal Aviation Administration and , the ` nit identi fied in item 4 was inspe cted in the manner prescribed by the Is APPROVED 0 REJECTED • FAA Flt. Standards Other (Specify) • Inspector Manufacturer Inspection Authorization • By • • FAA Designee x Repair Station Person Approved by•Tranapart Canada Ainvonhiness Group . • • Date of Approval orRejection Certificate or Signar—obailhorized Individual / .. Designation No. •: lit 6E,Pr. 90 0S4R425If. ' . FAA corm 337 • iteAr8 d:41,,?! -.7n/Li.i etiaftZVotcesere.Lesz• scraslY -co;341- EFTA00277894 z -1.5t)c'er:k- fr,4-t t"\.- Jr ' ;G• . . - z 4Q Weight andbalance& operating limitat NOTICE ion changes stiell.be enteredin the compatible with all previous alterati • ons to assure continued conformity appropriate aircraft record. An alteration must be with the aPplicable airworthiness requirements. • 8. Description of Work Accomplishe d • fit more space is required, attach add itional Sheets. Identify with airc raft nationality and registration mark and date work completed.) B727-31 S/N 20115 1. -MODIFIED J:POWERPLANT-:-INSTAL PRODUCTION. FOR AIRCRAFT HAVINGLARETION :4).1-FACILITATE RE-ENGINE MOTE ENGINE OIL REFILL SYSTEM IN ACCORDANCE WITH' VA 71000, REV. .48 :,.. DRAWINGS PER DER'TH0MAS F. . tCUBRAN NM-a83, APPROVED BY-811 0 DATED SEPTEMBER 4, 1990. PERFORMED AIRSTAIR INSTALLATION :IN (STRUCTURAL SUBSTANTIATION. OF .EXTERN ACCORDANCE WITH REPORT. 442 COMPONENTS FOR INSTALLATION OF: FORW ALDOUBLER AND .MISCELLANEOUS (INSTALLATION INSTRUCTIONS, BOEING'7AR D AIRSTAIR) AND REPORT 444 27f00 FORWARD‘AIRSTAIRI AND 6 IN'ACCORDANCE WITH• 750 -1- BOYD SMITH S0-351. P00 2. DATED 94101990 BY D.E.R. • • PROVIDED WEIGHT AND. BALANCE UPDATE. 'EQUIPMENT -LIST UPDATED ACCORDINGLY.. ALL SYSTEMS OPS CHECKED AND DO INTERFERE WITH OTHER SY STEMS. •ALLPERTINENTDETAILS OF. WORK. ACCOMPLI PAGE, AVITETCORPORAT;Pki UNDER WORK OR SHED ARE ON FILE DATEP://ri/sJT:Ani(07,. DERS'4706.AND 6778, END ,,,,„,,agic„„iggetroiralt.‘aantatrra` EFTA00277895 EFTA00277896 Twvemqs7PapIlilvt%"=c- iTlA alECKAFT REGISTRY CA'r,ERA p0.7 N DATE: 12-21-90 31;sammi,spdpeammisMINIa • • • .;it••• • rat -1;1:jilt/Ilea r r _-zdaRatagec.-- EFTA00277897 Soscref&r.t.kirrs gicgorglict— FAA AlRCF.AFT REGISTRY C.UtIF.A N DATE: 12-41-90 .AL • •:'44 '• ••• UNITED STATES Of AMERICA DEPARTMENT OF TRANSPORTATION—FEDERAL AVIATION ADMINISTRATION ' STANDARD AIRWORTHINESS CERTIFICATE NATIONALITY AND 2 MANUFACTURER AND MODEL 3 AiriCRAL7 SERIAL REGISTRATION MARKS 4 CATEGORY NUm0E0 N505C BOEING 727-31 20115 TRANSPORT 5 AUTHORITY AND BASIS FOR ISSUANCE • ' • ' Trtsalmorthinefulcertilicela is issuedpursuanl toilleFederal Aviation Aci of 1958andcerfille s ai oftheMte of iisuance aircraft to which issued has been inspected and found to conlorm 10 the Ilse cenificale therefor lo be m cvochhon for salt operation, and has bean shown lo hysel the requer errant& of the applicable comnrenensive an detailed aimontimuss coot as provided by Annex a to the Convention ohIntematoonal Cml Aviation.excem as noted herein EaraptiOnt • NONE B. TERMS ANO CONDITIONS LIMN* 5004r surrendered. suspended. revoked. or a termination date us otherwise etlabhiliel tw.the AdmatflatOr ibis alnvorthincee certificale is ellimint N long as Me maintenance preventative maintenance and nitenitiort air perlotn*d In IccordencewithPerts21.43.andfll ol Huffed**, Aviation Regulations. estop, ate find the aircraft •iregistered itIll•ets• d Stets& DATE OF ISSUANCE FAA REPRESENTATIVE % \hosso ea% NUMBER DESIGNATION 7/23/90 WING C. CHIA. DAR-41-FS-NM Any attenition.feprohuclion.tx usa of CellibefratemaybeliontinITM nol exert 000.o implisd'imtolmilexerealmj 3 years. or boib. THIS CERTIFICATE MUST BE DISPLAYED IN THE_AIRCRAFT IN ACCORDANCE WITH APPLICABLE I-El:WAAL AVIATION REGULATIONS. FAA Form 8100-2' ore2) CPO ena•nt•4 i.cm..4 O.:my boa -;frial: 8. • • ••••• •••• Cfr• • •• ••=. - ..40;rs.g. -Nisi,lab t:•4; • EFTA00277898 a•74.1 ..J1V-r•-_ -"Wiii'illr.7. , .cam, , :,r; WASEA.I.TAMILle••=iliaWEi.rfcq ',..!gt• FAA AIRCRAFT REGISTRY .CA4TRA R0.7 N DATU R. . • ...c;4op• s • doittacaYom. P•46 .--•)4 • ear-t;s6--"aAl.:- tr•U•••_. vs' EFTA00277899 AA AIRCRAFT REGISTRY C RA NO. 7 N DATE: 8- 15- 90 N a . ireg r ., .a.t."' vow • - 1.0” . ....., . . 1 • .i t-- , *ty1)•10 • • Form Approved $,• I . 0.M.8. No. 2120-0018 I , APPLICATION FOR INSTAUC710NS -- PrInter typo. Do not wrlte in shaded areas; those Ultie . occirned AIRWORTHINESS • use only. Submti original only to an authorized FAA Representative. If are for FAA additional Space's required, usean attachme Federal ‘4311on mhastranon CERTIFICATE II and VI 01.VII LIS 440floa,b11).; nt. Forspeoial flight permits compleloSect ions ltREGUSTRADON MARK , 2.A1RCRAFT BUILDER'S NroCE (AEO I. AIRCRAFT N AIRCRAFT MODEL D SI NATtON 4, YR. WA I1S05C \ ,J - ‘ t\ FAA COOING 727-31 • •- - •• to-;ti 5. AIRCRAFT SERIAL NO. Boeing . 69 /3 ,gc70/0 • DESCRIPTION & ENGINE f3UI L DER'S NAME mak ; 7. ENGINE MODEL DESIGNATION i 20115 Pratt S Whitney - - JT8D-,76 I 8. ts'mBER OF ENGINES 3 • . 9. PROPELLER BUILDER'S NAME (Make) 10. PROPELLER MODEL DESIGNATION 5 ,k53 11. AIRCRAFT IS (Check it appttc•bio) l APPUCAT1ON IS HEREBY MADE FOR: -e, 1 IMPORT (Choc applicatninimu A I STANDARD AIRWORTHINESS CERT IFICATE (/rtcocatit cerog,try) I 'NORMAL I 'UTILITY 1 'ACROBATIC' El SPECIAL AIRWORTHINESS 'TRANSPORT 1 'GLIDER CERTIFICATE (Check appropriate il I I BALLOON .. `3 LIMITED inu) e .. PROVISIONAL (Indicate cl attl) 1 CLASS I . 2 CLASS II 0 a 1 RESTRICTED ffnetteste opershonE 1 ' AGRICULTURE AND PEST CON TROL 2 AERIAL SURVEYING 3 AERIAL ADVERTISING t)I0 F be conducted) 8 FOREST (WrAlloto consarvenan) ,, I pATROLLING a WEATHER CONTROL --, I CARRIAGE OF CARGO iB 0 OTHER (Specify) 4/ . RESEARCH AND DEVELOPMENT 4 EXPERIMENTAL (Indic nd ate operetiOn(a) 2 AMATEUR BUILT '8 X to a conducted) 4 RACING I CREW TRAINING EXHIBITION = MKT. SURVEY l TO SHOW COMPLIANCE WITH ei X FAR • FERRY FLIGHT FOR REPAIRS, ALTE 7 RATIONS, MAINTENANCE OR STOR SPECIAL FLIGHT PERMIT War AGE ta EVAC 2 UATE FROM AREA OF IMPENDING 3 operation to be Conducted. then DANGER complete Section VI or VII as I OPERATION IN EXCESS OF MAXIMUM a CERTIFICATED TAKE-OFF WEIGHT applicable on remise style) . 4 DELIVERING OR EXPORT a♦ - • • I I1 I PRODUCTION FLIGHT TESTING a cI MULTIPLE AIRWORTHINESS CERT IFICATE (Check ABOVE 'Restricted CUSTOMER DEMONSTRATION FLIG HTS °potation" and "Standard' or -Limtled. A. REGISTERED OWNER (As show - as applicable) n on ceittficale of aircraft registration) NAME IF DEALER, CHECK HERE ADDRESS 1 • Northwest Holding Corporation Foulkstone Plaza, Suite 102 B. AIRCRAFT CERTIFICATION BASI 1409 Foulk Road, P.O. Box 7138, Wil z S (Check applicable blocks and complete as indicated) darns mington,DE 0 AIRCRAFT SPECIFICATION OR p end Revision No.) TYPE CERTIFICATE DATA SHEE T (One Na AIRWORTHINESS DIRECTIV ES 1.9B03 all Appic ego AD's con)plied watt 5 A3WE West AD No.) and pare (Check it a r AIRCRAFT LISTING (Ciro X 90- 02- 19 €€ page numbs:fit ) SUPPLEMENTAL TYPE CERTIFICA TE (Cut number of each SIC ii Rev, 18 - Dated February 20, 1987 Incorporated) : C. AIRCRAFT OPERATION AND • i, MAINTENANCE RECORDS CHECK IF RECORDS IN TOTAL AIRFRAME HOURS Iii S COMPLIANCE WITH . . • FAR 97175 EXPERIMENTAL ONLY (Enter hours = X 29820 Hours - a issued Oe renewed) flown salts leaf carttficels D. CERTIFICATION — I hereby certIty tttat I em the /agitated owne (or -0- Administration In eccord•nce with r his agent) of the aircraft deacnbed above t•• Section 50 of tr. Federal Aviation AcI orrery:011y and eIrgitale for the mrworthine as certificate reatenfed• of 1958. end applicable Firtkra/ Avila ; that the aircraft is registered with :an RegutsIon : and that the aircra the Federal Artaticm ft has been inspected and rs DATE OF APPlICAT ION n oTIT I or I f Valsan .Program & SIGNATURE it- A. THE AIRCRAFT February 2. 1990 R.A. Braulik DESCRIBED ABOVE HAS BEEN naineerina Manager INSPECTED AND FOUND AIRW Z g e FAR PART 121 OR 127 CERT ORTHY BY: (Compite• tan seefron only-i f FAR 21. BT(d) applies) t t PA I Carolicat• No.) IFICATE HOLDER (One ' CERTIFICATED MECHANIC (Cl.. - CERTIFICATED REPAIR STATION 1 SI Certificate Na) g ..06 . (Give COf I,lc ala et c -.2 No.) AIRCRAFT MANUFACTURER (Dire nem* of firm) _ V .4 _ DATE TITLE e SIGNATURE J (Check ALL applicable blocks in items A and Ell t A. I hnd that the anctalt des/tithed THE CERTIFICATE REQU in Section I or VII Ibsen requireme ESTED nts for. .F p 0 B. Inspection tor a apecsal WI prive 4 AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS J Z t under SWIM WI ' CERTIFICATE CR was conducted by: • FAA INSPECTOR 3 3 .. . • -..1. FAA DESIGNEE >.1:4 SC DATE DISTRICT OFFICE -- CERTIFICATE HOLDER UNDER. _ FAR 65 i _ FAR 121. 127 or 1-...y r frAR 145 .N D ATUR --Ape . ..:::-.....- , • , N NO. AA INSPECTORS SIGNATUR 9A-- %pa not goo. . -2.• ‘,(01- 0‘ , Nay s E FAA Form 8130-6 (6.06) SUPE • • 7> -sr --.9 A.,ni 1 RSEDES PREVIOUS EDITION • :V• • "f• - "...... • EFTA00277900 FOR saFE OPEFIATIONJUI.datteChInent UneawFwri • . E. THE FOLLOWING RESTRICTIONS ARE CONSIDERED NECESSARY described ton. Mai the airalin is registered with the Federal Aviation Adminsbetion in • P. agamealsOpa- eats demaymui am In reCettered Ores iahsa9.nU Oi Me*wall the Mod of lelle, end oppaceete Federal Aviation Regulations. end Mat the Wenn has been inspected and is airworthy for itCardenitlitvilh Elect100 al 00 the Feeterel Aviation Act tesic W.= EFTA00277901 ,. UNITED STATES OF AMERICA •• .. DEPARTMENT OF TRANSPORTATION - FEDERAL AVIATION ADMINISTR . ATiOt, .}- i, SPECIAL AIRWORTHINESS CERTIFICATE BATEGORY/DESIGNATIONri ,A-Zrel - If6t denr A PURPOSE ijalAret, . .B• MANU- NAME FACTUFIER ADDRESS ifh• _7 I" FPON1 Atg $: 'C FLIGHT • ... . To 4,4 arta NmAcc isof SERIAL NO. Z e.tr . D BUILDER MODEL "77:-.0„,/,' DATE OF ISSUANCESOffrar t /4'99 EXPIRY zehery/f/InetV• OPERATI LIMITATIONS DATEDS04,09/475WRE A PART OF THIS CERTIFICATE E WO OF FAA ATM DESIGNATION OR OFFICE NO. . — _ r e ard ed i .. . A r 7 -4 Cbg0• -— ' Any alteration. repmduction or me 1 this carlificaer may be punishable by a line not exceeding 51.000 or Imprisonment not exceeding 3 yearn, or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA FORIIM30.7 me . CPC arl/FligF Ainr EFTA00277902 AA AIRCRAFT REGISTRY RA NO. 1 N DATE: 8- 15- 90 A This airworthiness cenificale is issued under (he autho ^ and the Federal Aviation Regulations (FAR). rity Wipe Federal Aviation Act of 195‘. . • • .. This airworthiness certifiCate authorizes the manu . production flight tests. and only production flightfacttiret named on the reverse side to conduct B person may conduct produ tests, of aircraft regist ction flight tests under this, cestfficpte: (1) ered in his narne.,Wo Carrying' persOns or prqperty for compensation or hire: and/or (2) Carry theilight. .ing persons not essential to the pitrpose of .•• , .• C This'aInvorthiness certificate authorizes the flight Speci c' shown in Block A. fied on the reverssside for the purpose .. . . . . . ,.. , .. ,.. • . This airworthiness certificate certifies that, as of the . has been inspected and found to meet the requiremen date of issuanCe, the aircraft to which issued not meet the requirements of the applicable compr ts of theapplicable FAR. The aircraft does o provided by Annex 8 to the Convention OnInternational ive ehens and detailed airworthiness code op .thaaircraft describedon the reverse side: (1) except in Civil Aviation. NO Person may operate in accordance with conditions and limitations which accordance with the applicable FAR and part of this certificate:.(2) over any foreign count may be preacribed by the Administrator as country. . ry without the special permission of that - . .r . . . . . .. • -. . • . . . • • . Unless sooner surrendered. suspended. or revoked. this F c the duration and tinder the conditions prescribed in FAR ainvo rthine ss certificate is effective for Part 21. Section 21:181 or 21217. .. . • • - EFTA00277903 1/ DEPARTMENT. OF UNITED STATES OF AMERICA • TRANSPORTATIO N -FEDERAL AV • STANDARD AIRWOR IATION ADMINISTRATION NATKMALITT AND TI ESS• CERTIFICATE • REGISTRATION MARKS 2. MANUFACTURER AN . AIRCRAFT SERIAL NSOSC , Boeing MOOT .• 5 Transport ; S. AUTNORITX AND BASIS FOR ISSU I 1 • This airworthiness dote of issuance, A certificate i the aircraft 'therefor, to be in con s urwont h issued 1 and certifies that, as 4 • cornprawnsive and ditio n 1dfe, opera of the t nform to the type cert • detaile ificate i Aviation, except os note d. f iwo /miss he s ;cements of the app • d lica Exceptions: n ntion on Internalionol ble Civil F. TERMS AND CIADIT IONS Unless soon*, sumndir this airworthiness redersu oltied,\ 61‘ artifice • is long os net toblished by the performed in accorda aircraft is registered nce w and 91 of t. f Administrator, pints:mance, and alteratio ns ri In I nil I *lions, as appropriate, and or. 1 DATE OF ISSUANC the E FAA REPR Exchange 06 IV DESIGNATION NUMBER Any alatatio rep roduction, or misuse of prisonme of exceeding 3 yea certif.( o rs. ;skiable by a fine no ANCE N APPLICABLE FEDERA or both. IS CE TE MUST SE DISPLAYED exceeding $1,000, or :tn. L AVIATIO REGULA IN THE AIRCRAFT IN S. ACCORD. FAA Form 8100-2 (7-6n FORMERLY FAA FORM 5352 et . • v „ , • . . —tr. EFTA00277904 ">> >＂脚＾州＞哟阃 蝉蝉。 审川帅阀 6 '” 是。’ 鸿 °＞闩忡＂ 啪l 料动t 漶 ' ～ ＞ EFTA00277905 UNITED STATES OF DEPARTMENT OF TR AMERICA ANSPORTATION - FEDERAL AVIAT SPECIAL AIRWORTHIN IOArADMINISTR.,TION ESS CERTIFICATE A CATEGORY/DESIGNATIO PURPOSE uiTALN V rg TO SHOW CON CE watt, . Roes B MANU- NAME 65", FACTUR ER ADDRESS N •'4 :4' FROM 13Y _, n /-' C FLIGH T "-. ..y \ TO ttli 1 Y. N- 5456 I ..6- IRJ I L O ER Boeing l'S c ER* 0.20115 t i MODE 727- 1 DATE OF ISSUANCE Fe -t, 1 E OP IN 8/01/90" E St ae r0 M •TION %- cy 2 PART OF THIS CERT AA !F ICATE ORATION OR OFFICE NO B RT it • • ' . .- • . - Any ohm on, rtproclliCtIOD or misuse of this artificats OAR-48-AC-M way bo punishable by a fine . ezecerfing 3 yens, or both. THIS CERTIFICATE MU not tzenedina S1,000 or APPLICABLE FEDER ST BE imprisnntnent not AL AVIATION REGULATIONS. DISPLAYED IN THE AIRCRAFTIN ACCOR FAA PORM 6130-7 • DANCE writ l7-7P) USE PREVIOU .. . S EDITION SEE REVERSE UDE . 'zierta." EFTA00277906 A This airworthiness certificate is issued under the authority of the Federal Aviation'Am of -— 1958 and the Federal Aviation Regulations (FAR). . This airworthiness certificate authorizes the manufacturer named on the reverse side to con- ' duct production flight tests, and only production flight tests, of aircraft registered in his B name. No person may conduct production flight tests under this certificate: (I) Carrying per- , sons or property for compensation or hire; and/or (2) Carrying persons not essential to the - purpose of the flight. C This airworthiness certificate authorizes the flight specified on the reverse aide for the pm- "' pose shown in Block A. • ,. ' This airworthiness certificate certif161 that, as of the date of issuance, the aircraft to which' issued has been inspected and found to meet the requirements of the applicable FAR. The aircraft does not meet the requirements of the applicable comprehensive and detailed air- , worthiness code as provided by Annex B to the Convention On International Civil Aviation. ' No person may operate the aircraft described on the reverse side: (1) except in accordance with the applicable FAR and in accordance with conditions and limitations which may be prescribed -by the Administrator as part of this certificate; (2) over any foreign country with- out the special permission of that country. . c . - Unless sooner surrendered, suspended, or revoked, this airworthiness certificate is effective E for the duration and under the conditions prescribed in FAR Part 21, Section 21.181 or . 21.217. +t fo EFTA00277907 A 1.• rw ••••••• • • T• • Manufacturing Inspection District Office. 16501 Sherman Way, Suite 200 USDepairreor Van Nuys, CA. 91406 of Transportation Federal Aviation Aderdnismation February,2, 1990 p. EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's MAKE: Boeing MODEL: 727-31 SERIAL NO. 20115 REG. NO. N505C - THESE-`OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: • 1. too person may operate this- aircraft for other.than-the purpose of Show Compliance with the FAR's to accomplish the tests outlined in the ' -s - applicant's program —letter dated%February.2, 1990 describing compliance with FAR 21.193(d). Aldditionally, thit aircraft-shall be operated in accordance with applidable air-traffic and general operating rules of fAR 91, and all .additional liMitations herein prescribed under the provisions of FAR 91.42(4). . 2. -All flights. shall.be conducted within the geographical areas \• described as follows:. 1. Western Mnited States of America bounded on the East by the Mississippi Riier, on the North by the U.S.A./Canadianborder, on the South. by the U.S.A./Mexi,co border, and bounded on the West . by no more than 200 mileS. froM the West Coast of the United States of America. • 2. . Base Of operations is Palmdalettancaster Airport, Palmdale, 'California and secondary base of operation to be.Moses Lake Airport, Moses Lake,.Washington. f ' 3. The pilOt-in7command of"afrdraft must, as applicable, hold an appropriate category/class rating: have an aircraft type rating, have a flight instructor's. — log book-endorse:lent. of"possesi a "Letter of Authorizatton"-lssued by an -FAA • . General Aviation'or Air Carrier Operations Itspector. 'A. This aircraft shall not be flown Unless it is maintained and operated in accordance with"BOeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. -This aircraft shall contain the platards. , markings, etc: required by .FAR 91.31. • 6. The cognizant FAA office must be notified and their responge received in writing prior. to flying this aircraft after incorporating a major change as defined by FAR 21.93:. 7. , This aircraft approved for day/light .VFR/IFR -":1" rv$1777= "T-IlenialrgitykraMr-rce-- ?-4 • rf EFTA00277908 Federal Aviation Aftinistration Manufacturing Inspection District OffiCa , • ! - .:. • - Experimental -Shell Compliance.With FAN'S, Page 2 of 2 8. • No operations shall be conducted over 'congested airways except for takeoffs and densely:OnOulated-ardo or in, 1andings, and When,Under.ATC.O0tre!. . ••• . ',No persOri.may be carried in this aircraft duri -person is essential for -the purpose of the flig ng flight unlets that ht. 10. This aircraft is prohibited from aerobetic flight; intentional maneuver`involving an.abrupt -change in the' that is, an. attitude, an' abnormal attitude or abnormal accelerationait.craft's for:normal flight unless approved.by the cognizan not necessary t FAA office. - . . 11. .If-aircraft, engine or propeller operating . • an appropriate entry. will be made,in the hist limititions are-exceeded, orical records: 12. After the'aircraft hasImen re-engined, the pilo make a log book entry stating the'aircraft comp t-in-command must and FAR 91.42(b). lies with FAR 91.42(a) T6eieilimitati0nS:*11.1 expire on August 1, 1990. EFTA00277909 AnclAPT NEOISTAV CAMBIA NO. 1 N DATE: 8- 15- 90 VALSAN• PARTNERS 3010 Westchester Avenue. Purchase. New %TX 10577 .* • (914) 694.3600 Telex: 825379 VALSAN OF Marketing Office: Fax: (914) 694.6062 99 Washington Street. Norwalk, CT 06854 (M3)866-6051 • • Telex: 6714726 DALAV UW ADelawareLtavtedRinnemhip Fax: (203) 855-0362 Product Support Office: Febfbify 1990 3605 Long Beach Blvd, #205 Long Beach, CA 90807 Tel: (213) 424-2145 Fax: (213) 595-0920 Mr t Bud Martell, Manager • . . Federal Aviation Administration Manufacturing Inspection District Office.• In reply . .16501 Sherman Way, Suite 200 • refer to Van NuyS, CA 91406 * . 001020290 .Subject: Application fortxperiMental Airworthiness Certificate • (To'Show Compliance. withFA,Ri) .- • • Gentlemin: .• . This letter is toinfotii\You.thai- Valsan intends to operate Boeing 727-31 ,. Registration N505C, Serial #20115 owned by Northwest_ Holding COrporation,Foulkstohe Plaza, Suite 102, 1409 Foulk Road, P.O. Box 7138, Wiliiiington,Delaware 19803 in an experimental. flight test prograM. The flight test program is in support of the Valsan JT8D-219 Re-Engining:PrOgram TIA NM-100S-1320. / Terms and conditions of the. Experimental Airworthiness Certificate are as follows: •• • • Valid for six (6) months fromLeffeCtive date of the . certificate. 2. Geographic area:is the, Western United States of AMerica. 3. Operation of. aircraft'will be in. accordance with alt. , applicable F:AjWs and:F.A:A. 8130-6 (attached).. Aircraft to'be maintained in accordance with Federal Aviation RegUlatiOns Part 91.169(f)(4), a current inspectiOn program recommended by the. manufacturer (Boeing Low Utilization Maintenance Program). R.A. Broulik Valsan Program/Engineering Manager C/O - Rockwell International 2825'East Avenue P Palmdale, CA 93550 Attachment RAB:lg t•-•••**0.,.. .• . EFTA00277910 烤暮·儿黧 h亡 m EFTA00277911 US .DEPAPTAIDIT a TIVIONVOITIAT1ON FEDERALAVIATION ROINOSTRATION - .. ..---,• ..sai . Sadsaltriiii 'No. 04-11060.1 ., ' atiumt WHIR AND ALTERATION tPOD FAA WE ONLY . J i 4 (Airframe, Pewerplent, Propeller, or OFFICE ,IDENTIFICAT1ON Apptione0) '11F-PHX INSTRUCTIONS: Prin or type Ill for instructions and dispt osit entries. . See ion of this form. - FAR 43.9. F4/1 43 Appendix 8, sod AC 43.9-1 (or0 subsequen -FSDO s • ... . . •- t revision thels..1) AWE I MOOR - • BOEING I. AnKilAn Sing NO. - • I Z.21.7.31 • • 'NATIONALITY AND REGISTRATION MARK • . .4 0115 . ii N505C \ NAN& (As shown on nigistnation mirtificars) • iI ADDRESS (As shown.on mpildration 7. OWNEI • . FB TRANSPORT INC. • ionOcoto( 1 100 PINE ST 2.1 FLOOR I P RUNT . c i 2 SAN FRANCISCO. CA 941 21. • 1 MR FAA USE Min , . • . . ... • - • , . ... - - . . .. . , • . ... , • I. UNIT IDENTIFICATION . onto . -. 1 -. . S. net L ...----- Ulna NO. " *me- • . SPAS Anon AIIIPRAME IIMNIOMONOANISOMMIN (As thootn i a slim I oboe)me teen . . POirrEltPtAte - . . • • •: MOMS t • - .. roe APPLIANCE mAsanakras ; o .• • A. AGENCY'S NAME AND A. CINFOIMITY STATEMENT ADDRESS . R. KIND Of AGENCY ' , C. CERTIFICATE NO. • vs. Ceetiticatur Pi1Cooksic . .DYNAIR TECH OF ARIZONA. INC• : -. • rer.t.rO4cominweci micmanic .3737 E. BONANZA WAY ' CRS A07-36 p is o CeenrICATID RIM! Inaptis PHOENIX. ARIZONA -. 85034't • -AIRFRAME.IV •.. satiuMCWItt ' D. I certify that the rep air and/or alteration made ' •inachtnents•heritobave been to the uriiiIst identified in item .4 abo made in accardanie. with the ve and described on the and that the information furniihe requirements of Pan 43 of the reverie or d Stein is true and correct to U.S. Federal Aviation Regulat the best of my knowledge. ion! DAT E " - SIGNATURE OF AUTHORIZED IND IVIDUAL' . ' •, : . AUGUST 10 1989 ' KENNETH ROWBOTHAM—Wernenta.a 4AP •• I . 44 , ."-- 7. APPROVAL FOR INTIM TO SERVICE Pursuant to‘rba author peen - ity she Administrator of the Pt pers ons spe cifie d below, the -A' Aviation Administration and unit identified in item 4 ',rasa:edin the is ®APPROVED O RE) manner prescribed, by • 'AA Pit. suitopu its aaaWACNINI . IMPICTI0NSONOIWATION . OTHER aativ) It • . IAA Otteill CAHN:KAN OrMITOUNT - XXX illia. SUMO.. Or NAMPO., worecrot DOI OP AMOVAt a v.Xr RIIICTION . =ON OR SIGNATURE Of WM D I NO . AUGUST 10. 1989 CRS 407-36 DANIEL WEAR , .. . (1320) EFTA00277912 'F i.At8cRATT ItniS/RY CAMtKA NO. / 41 DATE: 8 • NOTICE iliWeight and balance_or operating limitation changes shall be entered-in the appropriate aircraft record. An reiteration.mitst: be compatible with all previous alterations to assure continued conformity applicable airworthiness requirements. with the 8. DESCRIPTION OF' WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify witIleircraft nationality and registration mark and date work completed.) 1. FABRICATED S INSTALLED REPAIR ANGLE ON LOWER EDGE OF FUSELAGE SKIN FOR NO. 2 ENGINE SIDE COWL AT FIREWALL BULKHEAD 'APPROXIMATELY FS 1455 PER SRM 5.1-40-4.. 2. REWIRED 'CRACK AT RH HORIZONTAL STABILIZER LEADING EDGE APPROXIMATELY STA 78.3- 88.3q PER SRM*55-10-3. 3. . REMOVED CORROSION. CUT OUT BULGED AREA IN EXTERIOR FUSELAGE SKIN, INSTALLED DOUBLER APPROXIMATELY FS 1157 AT STRINGER 27R PER SRO 53=30-3. : 4. REPAIRED FUSELAGE'SKIN CORROSION. DAMAGE BS -1166 - 1174 AT STRINGER 27L IN. ACCORDANCE WITH BOEING REPAIR MESSAGE NO. BPI423200D. it U.S. GOVSINSINIVIT PRINTING OCCICE: ISS6-689-121/43146 osspAltia-wft" EFTA00277913 ,____ ,,,,_ U.S DEPARDAINT Of TRANSPORTATION ill RA . ,. •. FEDERAL AVIATION ADMINISTRATION • Fine App. ed ,Bage t Pinta. N.. 04-Ito60.: . MAJOR REPAIR AND ALTE -• RATION . -- OFFIcrF07REt; 4fi ctictalltEop4ONLY (Airframe, Peworplant, Propellor - , or Appliance+ VNYF . SD; INSTRUCTIONS: Print or typsell 00/7 for instructions sad disposit entries. S.. FAR 43.,. F4R 43 Append ion of this form. ia D. end AC 43.9-I lot subsequen t revision thereon MAKE • . .REOEIVED.FAA !mote , 1. AllCitArf•••• Fib! EING ' • "1- SERIAL ' • •• 727-100 , 20115. . rA I y 0.• 1., 1990 'NATIONALITY AND REGISTRATIDN MA RK NAME Os shown on registrstion tortifi.cetiam . N505C v Fq..)0 ADDRESS (As shown qn reoistrotion 2.CIVINEI, . LIMITED INCORPORATED - • • -- ""- '7 -- - 4387 International G'atewcerr ay iScorto) - 'Col umbus > Ohio : 43219 • • . . • 1. fOR fAA USE ONLY ., ...... • • • .... .. ...._ . .. '•• . • •• . -.• .. . ..-. .. ._ .- • ,. . .,. . . .• . . . ; ... , : • ., , • . .. . . - 4. IT IDENTIFICATION Watt S. TYPE- Mont • f • • ' . Melia ' NO. Anti- IIIIPMII _. . .._ . • *Now AIRFRAME • esetweteneeniennotoe. (As thos • cree d m Ihom ) obovoineeenbaseenreevr aseem X • . . tantrum • , . - . . . ... . ' • . . .. X . . . PROPELLER . . .. . .. , ' . ern • APPLIANCE i sensusecuua • ••• • • • r . • •• . • • . . . • . . • • A. AGENCY'S NAME AND 4. CSINFORIIITY STATEMENT • ADDRESS S. KIND Of AGENCY ekr, North American Aircrat' - . -- - -- . ••• • C. CERTIFICATE NO. Rockwell International Corpor --- Y.N . tan nest** setetiaisse 2825 E. Avenue P . ation . foa m* . cestmcarto macmAwic flOt8WepSlAniant Palmdale, Ca.. . 93550 . . X "CIP IPIC AIT0 NMI' STATION. . Class 3 " . NXAR688K • Y O. I certify that threepall sad/or -a auireRIACTRATO . . .:• . lter attachments hereto Inve'been mad atitia-made to the unit(*) identified in item 4 above and that the information furn e in accordance with the requirements on described on the reverse of Part 43 of the or ished berein is true and cornet to the best of my knowledgeU . eral Aviation Regulation ,', DATE .• • SIGNATURE. OF AUTHORIZE INDIVID nigli ti ot7 jt . /0 9e) ; I .D.A. Perazzo • RETURN TO.SERVIC 1. APPROVAL FOR S d r. . Peasant to the authority jin - . • KW Administrator N St h& n ven om speciied below. the tink4enti6ed In ide Aviation Administration and is • Ste 4 was Impened In the manne r prescribed by I SY i IIIA Ott. b/IMG • WOWS suanatites APPROVED . ~toss saniatiwno•• REJEC , Orrin ISesehi i • • . IAA X Ilia PATCH • .cataa TRAgui NSPRo ORTmunatton 'Of . . DATE OF APPROVAL OR AISM. : .• • RAJ! CERTIPECATI 'OR SIONATUkt • ? MTH • ED INDIVIDUAL 4.4.199a DESIGNATION NO. • ' i • L. . a" ft 97 NXAR688K ' 4 • .....4.-frics) EFTA00277914 鞲 －口 EFTA00277915 .,„ " Weight andbalanceor operatinglimitatio NOTICE " altmition must be compatible with all n changes shall be enteredIn the appropriate aircraft record. An . : • applicable al/worthiness requirements previous alterations to assure continued conformity with the , 8...DESCRIPTION OF WORK ACCOMP Identity with aircraftnation4lity andregiLIS HED Ott amore. space is required, attach additional sheets. stration mark anddate wort con pletad,) A. Modiinalloqing Model 727-100 , Seiial Number 2011 ' mental' type certificate SA4363NM, amended•September5, in accordance with supple- 1. Valsan-Boeing127-200.Re-engining Document VA000001 1, 1989 "as follows: , Revision F, dated January 2i. The following dftwings and engineering orders above document: (al's) are in addition to the - • NOTE: - °VA" denotes Valsan Deaiting. a: `'Chapter 24 ELECTRICAL POWER • A240000 A Electrical .System Instl. - Strut E.O.: 003A VA240007 E -, Panel-Load Control Center Modification. E.O.,'10 1 : 003A, 004, 005, 006 b.. Chaster 28 FUEL SYSTEM INSTALLATION., STRUT- • VA280001 .. B Tube, Assy - Fuel Strut Feed Thru E.O.: '100 Chapter 48, MISC A481100 .A Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, VA481200 C.. Frame Assy'Sta 1263 E.O.: 101, 103 102 VA481300 C Fuselage Skin E.O.: 106, 114A, 114, 116 VA481324 NC Intercostal Assy, - BSTA 1223 to BSTA 1243 W/L244.3 VA481325. NC Intercostal Assy, - BSTA 1223 to BSTA 1243 W/L234.0 9 E.O: 106 6 E.0: 105 Chapter.53 FUSELAGESTRUCTURE A530001 B Ballast Weight Instillaticin E.0: 100, 102 VA530003 C Ballast geight, Support Structure Assy. E.O.: VA530004 NC Ballast Weight Instl. STA 312 - 360, E.O.: 002,002,100 — 100 Chapter 54 NACELLES & PYLONS - ,VA543000 C Main Strut Assy 2, & 5) E.O.: -003 VA543100 D Firewall Rib,.Side Engine LO:.36A,003A Chapter 71 POWER PLANT _ A710000 NC Power Plant Instl. - Engine Pod V727RE 002, 1058 • 109, 108, 001k 104A, 005A,.004, 110, 003, 111,1106A , Chapter 73 ENGINE FUEL AND CONTROL- . . . A732 301. K .App roac h Idle Solenoid Wiring Diagram E.0: 002(Rev 002 (Rei. M), 003(Rev::M) VA732303 D Relay Inttl. Approach Idle Solenoid E.O.: 103, 003 • , VA732304 . D • Switch/IND Light Instl --Ap , 1008 . proach Idle E.O.: 002, . VA732310_ 'A Switch' Instl. --Nose Gear Position Approach Idles-E. VA732315 NC Relay-Inttlf Pilots Overhead Panel E.O.: O.: 103 002; 101, Chapter 76 ENGINEIOTROl. ' • A760000 A .Eng)ne COntrols,Instl. - Strut-E.O.: 002A VA760014 A . Drum Instl. Eng. Controls E.O.:- 100, 101 VA760015 A . Bradkit Assy.:.- Pulley ESTA 100 E.O.: 105 EFTA00277916 EFTA00277917 DESCRIPTION OF WORK ACCOMPLISHED (Cf:iiitiPliel) • . Serial No. 201lt . Cha ter 77 ENGINE INDICATING * ! A771005 Indicator• Engine Pressure Ratio EPR, E.O.: 001 Chapter 78 ENGINE EXHAUST A780000 Engine Strut controls Instr. E.O.: 002_ VA783010 E. Flt Deck Indicator Instl. T/R-Sys. E.O.: 003,:004 'VA783011 F Thrust Reverser System Wiring Diagram'E.0:: -002 (Rev. G) VA783013 D • Support-Bracket Assy - .T/R Control Valve -R/S E.O.: 100 (Rev VA783017 J Placards E.O.: 007,, 008 - • VA783(et Relay Instl. - Thrust.Reverser Control E.O.: 003 VA784028:. •' • A, Mixer, Exhaust - Instl. 727E E.0::.100 VA781101:- No: 2 Engine T/R Wiring Deaetiiiation E:0 002 , - Chapter 91 CHARTS:. VA910002 A • Instl. 7. EleCtriCal Wite Harness VA910008 : NC : Wire List V727RE E.O.:-00.1,.002, 003 • 603,*4,-605, • ••: *New drawings added to: modification 127:SerVice:Bulletin 727-'53A0171, dated December 14, 1989... FUselage's., Station. 1182 Presture'Bulkhead,Weh: • Crackllepair.inCPreventiVe • Modification'. . • , . The aircraff.eiptY ueigtit.and center of gravity was .revised in accordance with Bbeing Weightand Balance Manual D6-21200.- . Weight and BalanCe Manual Supplement,'VA7CR279 ' is attitched • EFTA00277918 EFTA00277919 SCALE READING Left Outboard -Main 24402 Left Inboard Main 21865 Right Outboard Main 1 X23687 Right Inboard Main t - •4777%..14,4).% Left Nose Right Nose „4 :04T414,V.C .i4t ,4**-Kns. Subtotal (Nose) 883253 176804 Items part of Basic Weight 4WW0AnAPDTVREA5K- but not Weighed AIRCRAFT. BASIC WEIGHT gsctvxivw?;antfpk Au' ti,j1m4 44. 111.221 = (MI) Distance tram the jig point to the main axis Centerline 520.1 1 • (M2) Distance - betweinthe• lettilose axle centerline and the jig point. eie.nl e (N3) Distance bitween•the right nose axle centerline and the jig point. 330.101 • (RI) Distance fres the referent. dates to the jig point of the aircraft. 950.121 a (A) Nein LOS Reaction' 311.371 = (I) Nose 'Axle liaction. :Ti littt aeVeRgirtiitid6;:%irtrisi • REMARKS The aircraft was weighed in a level attitude and in an enclosed hanger. 2. The wing panel jack' point . .• 4k - was 3. This is the summation of'the used for the aircraft jig point. 4. Baseline Weight Results 3 weighings. - for Post Mod Flight Test, dated _- 4/10/RO. J EFTA00277920 •1 Y. rr_f', EFTA00277921 727 — 100:/ 200 Weighing Form Left Outboard Main Left Inboard Main Right Outboard Main Right Inboard'Main riffix• Left Nose Rightlifose Subtotal 89563757 part of Basic Weight Basic Weight but not Weighed 1 4.4?.. • AIRCRAFT BASIC :ijki?-77-r= .,504•`x i WEIGHT 1 . 96173 931.278139.33% tsrilfzt , CORRECTIONS „"tittiga, Items NOT weighed but night Basic Weight mEAsuREmEtrie 118.22) ..(.1)Distant, from thelig point to Vie gain axle eantenlin, 320.11 s (112) Distant* between the left-toss axle centerlinaand tha jig point. . c (M3) Distinta.batenn the right noel axle centerline and tha jig point. s (R1) Distant, froa Lb, referants data to the jig point of the aircraft. 950. 121 s (A) Main 'Rile Reaction A s .R1041 311.371 (s) 'sits•'ail Reaction II a R1-(1124443)/2 The aircraft was weighed in a level attitude and in an enclosed hanger. • • 2. The wing panel jack point was used for the aircraft jig 3. This is weighing 1 of 3 point. .4=447Awan,1147' EFTA00277922 潜嗨置鲢薄鬈鑫坚： EFTA00277923 JAL AIRCRAFT REGISTRY CAMERA NO. 1 N DATE: 8 75- 90 • .. .. ....::•7; i 727 - 100 1_ 200 • : . • C. • .• .. ..r. . • ••- '"t;..II ' WeigIving.FOrm c • -,: ' L *Alt.il ...fl. “;:ic._ .: Date 'Model . 18eriail Number Place Weighed' Technician Phone 4/18/90 727-100 10115 - N505C . •ALMDALE FOLEY (805)265-2151 . ... .. , REACTIONS'' . SCALE •'41.1• " ‘.TARE . NET • - ARM MOMENT . • READING it $ ... WEIGHT - • • *. I.7;! • xi ' • 1.qt :tot& 4 Left Outboard. Main- et. . ..2..::gi.19 Firei. Vt.; % • t• • ;;;;;.;.A .4.,*:::*;14., • ••••• \ 1.••". • !.. . 24402 *.:' r - 6 24408 >. Left Inboard. Main . .41 " . 21865 t. 2 21867 L. •:.:;;;2;.:444.4.!."211.11#•dia. •:.'ner&E,4:40.4,Fe ,4;;I:f .t'ite,:•:•.•.:.. l4/Y41:11, 1(tl':cliii:: is r, .....ip.bv..1-.... A .47:3;4 ". . . 3•1 %'•.I 1"i . •' • 4 ••••• -,..•: 8( 7 ...4.- ! ! . 1Wi " rt:" .... :Sri .: • ' -‘ ' " I !!! 31 174. -- gyel;..‘ 17... Ca •:. , ..„;..f.t ,:......g:Ca Right Outboard Main 23689 4 23680 ::::-..44:k..t412: ...Q..: .:.....,•• .. Tr .•! 0. • ..bP . 1) ... .h:il 'Cer ... %'.. . 81 ••• .!'t 4.• u •/, if Right Inboard:Main' 23381 f, r 3 23384 ..4. • "ran.... ktype ,... .....;:;:oA.;:•.i:-. 9 far 4.10, •...t..i,.5 ;.:. .:1.:44.%;.:. . n..f .......:.=:. ... 4 s.01 .5 .. i 5-ef-,4s .4. 8 Tiv....,. - ...:....04! . 4. so ...:0 12 C I.:nil" • ' .... ' 4 . .2 ' . 'C .175 ‘g`:r•••••••.:•:• Subtotal (Mains) 93337 e e i o. '" 7 93344 A - 950.12 . . ••' • 88688001 •2-: 7. ti 5 ik 'Men 4tPitir .:11 OA , r I ,, . . fairgiN9! • Left Nose •'. . 1338 i;V:Z -, t• . .".1.1,z44/P .‘ - na 1338 - • - zi I. 4,1' •:. it Right Nose - .- 1501 0 1501 --- •,,,, k2,F2 • v,..•-mts t... ..44.,KAcre. 1.-- . 4.:. . r: htili.5. 04.ekl rs.sranons•• i e0 .......•: 161 17 1 Subtotal (Nose) 2839 1 l'• r .• r ti. A e 0 .2839 us 311.37 ,t:if- 883979 “.... ' AL • ri Ze •;•• ... .iia"VV %at fier;":::!el :, TOTAL 96176 7 96183 931.27 e.- - 89571981 id,41. 4;i ,.... , . . ite rae liti at.t' ",..., e i•str -$7 YL AwAt 4,1.,41 , sIr..t.;!" •;514 • •• ! , 7 t 1: -AAc“..2 f .h. . E., t t a:1 .." ..! 5". f, 33C 7;;;:t.:•Ir .4 a " "k" • lt t aka Items NOT part of'Basic Weight o :)...e r, •o PLUS „.. t"4"717 R41411V-gitilVP.Vialt;01,3 Airefti:-.. 4 llilkin,?/•:gial-iR.; • A ..iml' Items part of Basic Weight,but not Weighed ofay sto '", • AN. • 0 pp •• -.J . •:.:• . ....tVrait % 4.; ••;•.: V % ••!..•:"•••• :: V& .• 34,41,1 Ltlit.142:::4:' ..:94..A., 0. A.M.S.< Arty r .1 gi'•ri: it.4.!”71. .11LX:Z4 itSC• A••• : diefk :.. .., u.ii . V2 — .4. :: f: •••• AIRCRAFT BASIC WEIGHT • 96183[ 931.27 39.33X 89571981 tlirlektspiflt r 1.9wA *"' laii h -. „ ,, - ir.• • 'clus‘'" 4t•Pc.C*11#7ite 0 11 - . s , 11'1. 22 14 •161"*".•a!"4(1•24#‘ K. rd frtrat trit: '4-.02."{ 4n;.2:- l. ••• 4 • CORRECTIONS s. C lr ,, a :,..:tit •• ts2... ..y:. :,.m: . Sq.. 4 •cit. •.1 .• ;A:t. NOT Part of r Items NOT weighed but Part of - Basic Weight Basic Weight Description Weight Arm Moment Description Weight Arm Moment 1 • . TOTAL ; 0 0 1TOTAL 0 , ..i.fi,-orritez.f , k-r.• .. .,:,16.4. .,..-Z2.4-,A.:.. -7. _W. l*:.,..*.e..:t . . .....,. t4.4itatift! .i..J.•r „ t 1)ilgzliii . err 4,- , . mustummurrs ‘ ,,,SS ;A— , : ,... .. i• ' '119.22 a Oil) Dieter*, fro, the. 310I point to the sain.axle .centerline 920.11 a (142) Distrito between the loft nose axle centerline and the jig point. 910.991 a (11.1) Distance between the right ;Se axle centerline-end the jig point. ilS0.901. a (R1) Distance fecal the .referenle data to the 319 Point -of •The aircraft. 950. 121 a (A) Rain Axle Reaction' Ori‘111011 . . 4 . 311 371 a Cal Sim Axle ...action a s R1-(112019)/2 . .. • • Elifiliiiit,:i*:2;.!t1;- ..ci,n ..lin.. 100,1i.:\Vitil REMARKS" 11:0F0Fit l.‘' '•-•.:.T.I.ty.i'vill: '•.141.9)! 4-'1474.4fi.L.i n . . • 1. - The aircraft . was' Weighed in alevel . attitude and in an- . enclosed hanger.' • .. • . .. • - 2_. The wing' panel jack point was used for the- aircraft jig ,point. • . 3. This is 'weighing' 2 of 3.: • • . .- • EFTA00277924 tIAA AaRCRART REGISTRY Mini WO. .1 N DATE: 8- 75- 90 • • •";-•'"7• • •a 4. u"ktin'ti EFTA00277925 6 24407 2 21864 Items NOT part of Basic Weight PLUS 1 771',iS :14:;!:r AigligteieiT:tra$5ZitiMil0.,4.6 Items part of .Basic Weight .but not Weighed ......7.. .;,„•:,Fc, i..,,,,,:i.:::a..491:4:;514.t. AIRCRAFT? BASIC -WEIGNZ 96180. 931.30139.35X 8957232 •i TrA43 114114-2 i;, ..1;!.P..1.51,c, ea'. fill• aictilfii • 4.:•• ••tilref•air ••••- • %'d :- • fisttel•• N.*, • s,,,w-Pirsi 34•tksz.srsta‘wt:ttiormike*A" alliq2:2:filf,f•O:z•• -':i.3rit;.-• Vci.14•::, 044Kiat• 4 I'i3„.. .ese4:71,*....:-6w:etonttit4,4ti -C"RECTIONS 6.,:04 10T.”44:1: %'?...1 59 5.:Tt2fritii11444( .. tifizeFitsic. NOT Part of • Items NOT weighed but Part of • Basic Weight Basic Weight Description a (MI) biltince tree the jig•point to the ;Pain axle centerline .•. el.( 12). 01ittence- betweeri .the.loft -nose•axle•centerline and the jig point: c••(Iii).Diatance•between the right mese axle' centerline and the fig point. (Ii1) Distance from the reference - ditue to. the 'fig paint of the etrcraft. (A) Hain Axle Reaction imam . " (II) joie Axle React/en aR1-(1424443)/2 • 4 , REMARKS 1.. The aircraft waa vieighid in a 1pvel attitude apd iri an enclosed hanger. The wing' pane1 . jaaki point:weis used for the aircraft jig point. 3. 1 This. fr ...weighing Of 3 . • • • • . . 1 • EFTA00277926 64'n, -4prer,liar#- - •— <ler L r'lvAr3414" 4241:44- .-4s-Aats 2 EFTA00277927 '• • war. Etir WnANDroaTATI0N pie tired FEDERAL AVIATION ADMINISTRATION - edger wean No. 04-R060.1 MAJOR REPAIR AND ALTERATION' - FOR FAA USE ONLY • (Airframe, Powerplant, Propeller, or Appliance) IDE TOO • INSTRUCTIONS: Print or type ail entries. - See FAR for instructions and disposition of this form. 43.9, FAR 43 Appendix -B. and AC 43.9-1 (or subsequent revision thereof) - Cy MAKE MODEL. 1. AIRCRAFT Boeing • '-727-31 SERIAL NO. NATIONALITY AND REGISTRATION MARK 20115 N5051 • NAME (As shown on registrallavontificate) ADDRESS (As shown on registration certificate) 2. OWNER Tenneco Inc. 16951 J.F. K. Blvd. Houston, TX 77032 • • 3. FOR FAA USE ONLY • • - • •Ninti: . ; ,..: -.4..1:.- -; •. • ...:•• -.J., :• •- , • • 4. UNIT IDENTIFICATION UNIT S. TYPE ;MAKE MODEL SERIAL NO. ALTER- REPAIR . ATION AIRFRAME ateweeentweenneetee (As described in ;tern T. above ) XX POWERPLANT • PROPELLER TYPE APPLIANCE MANUFACTURER 6CONFORMITY SlATFJAENT A. AGENCY'S NAME AND ADDRESS B. KIND OF AGENCY C. CERTIFICATE NO. U.S. CERTIFICATED MECHANIC . • Tenneco Inc. FOREIGN CERTIFICATED MECHANIC 16951 J.F.K. Blvd. X CERTIFICATED REPAIR STATION Houston, TX 77032 205-10 • MANUFACTURER D. I certify that the repair and/or altera tion made to the unit(s) identified in item 4 above and descr attachments hereto have been made in accord ibed on the reverse or and that the information furnished herein is ance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations true and correct to the best of my knowledge. DATE . . . • SIGNATURE OF AUTHORIZED INDIVIDUAL • 04-04-85 7. APPROVAL FOR RETURN TO SERVICE Pnrsuan to the authority given persons specif the Administrator of the Federal Aviation ied below the unit identified in item 4 was inspected in the Administration and is Ir4 APPROVED O REJEL. CU) manner prescribed by FAA R.T. STANDARDS OTHER (Specify) INSPECTOR MANUFACTURER ' INSPECTION AUTHORIZATION EY , CANADIAN DEPAREMENT FAA DESIGNEE REPAIR STATION ' OF TRANSPORT INSPECTOR X of AIRCRAFT DATE OF APPROVAL OR CERTIFICATE OR SIGNATURE OF AUTHORIZED INDIVIDUAL DESIGNATION NO. ....4/O RU1°1°01-04-85- 205-10 - - •• • iAT....- t- a tre • • ••`:—.. •' " "I ••:• '14.‘11•.'.44 • • • d • :•.;?:Ps_ ? ‘ "e' . j..: •••e . • I••••• ms•S • EFTA00277928 FAA AIRCRAF REGISTRY„ CAMERA DO. 1- DATE: '7 -....r.T•T • "." NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An atterotion' must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements.; 8. DESCRIPTION OF WORK ACCOMPLIShED (If more space is required, attach additional sheets. Identify with air- Craft nationality and registration mark and date work completed.) CREW AREA CHAIR INSTALLATION I. Re4ovecifolding,couch:from L/H crew compartment station 400. II. Installed (1 each) Tosington T1150M24 F/A AFT facing single chair on sliding rails from station 420 - tOTstaticih :380. • III. This alteration. was completed in accordance with Threshold Engineering Company of.San Antonio, TX, drawing #270 and instructions identified in report #259. IV. All engineering drawing and reports were drafted and approved on FAA Form 8110-3 by J. A. Dugelby D.E.R. .(designation number.SW.7 256) and are available. to the administrator on request. . • V. .All work performed utilizing acceptable methods, techniques, and practices per AC. 41i13-1A. .VI. )Aircraft weight and balance amended. ---END--- • ADDITIONAL SHEETS ARE ATTACHED , •• ••. • . _ ,. _ _ . *US. GOVERNMENT PRINTING OFFICE: 1977-771.021/344 EFTA00277929 I - contmea Of Tatuvonnou:: • in &tinned FEDERAL AVIATION SINISTRATI0N . • fistoWer Biroce No .04-R060.I . - NIAJQR REPAIR AND ALTERATION - (Aidrame,Weirerilent,'Propeller,.or Appliance) , . . . -• OFFICE FOR FAA USE ONLY IDENWICATION Sai-feloo • INSTRUCT ONS: Print or type all entries. See FAR. 43.9,•FAR 43 Appendix S. and AC 43.9—I Lot.inbsequent revision . . di • MAKE•• for instructions and disposition of thie,forta. Boeing. ' : . . - • MODEL 1. AIRCRAFT SERIA L 115 NO.20 r NATIO NALRY'EGISTRAT N505T ' MARKION- AND 72-7-31 • - -71. 2. OWNER • . NAME Tenneco (Asshcam on registration certificate) ---. CADDRESS 16951 • (As short on registration ceitificcrte) JFK Blvd. .• _ : Inc • : ... : • • , .Hotis t on , Texas 77032 . - • • - 3. FOR FAKIISE. MI • • • to dalatMeSian Identified herein complied with applicable airworthiness requirements and Is approved for the above described aircraft subject to conformity' inspection by a person authorized in FAR 43, Section 43.7. • • • .... . / 2:raCC • babe Signatur of F seeder ' - 4. UNIT IDENTIFICATION . I .5. TYPE UNIT . MAKE • . • MODEL SERIAL NO. . ALTER- • - REPAIR • . ATI0N AIRFRAME. •• - '• . • . • . .' • .7PIII•••••••••••••••In4 • • . " (As descited in item 1 above) . ' - .- XX POVIERPbOlT . - , • . • • PROPELLER : ..- . • - . . • TYPE .. APPLIANCE MANUFACTURER . .. , . A.AGENNAME CY'S ADDRESS t • .AND 6. CONFORMITY STATEMENT B.KINDOFAGENCY C.CERTIFICA NO. TE . 16951. Tenneco Inc JFK Blvd. Houston, Tx. 77032 U.S. CERTIFICATED MECHANIC FOREIGN CERTIFICATED MECHANIC x aunkuoui REPAIR STATION .• 205-1.6 • • • • MANUFACTURER - . ca. • D. i Certify that the repair and/or alteration made to the unit(s)• identified in item 4 above and described on the reverse attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation or - . Regulations DATE •• and that the information furnished herein is true and correct to the best of my knowledge. . - SIGNA IOF TUREC7 IN IVIDUAl. 7. APPROVAL FOR RETURN TO SERVICE Put uant to the •authority given persons specified below the unitfintified injtern 4 was inspected in the manner prescribed the Administrator of the Federal Aviation Administration and is' by APPROVED O REJECTED fg FAA RT. STANDARDS OTHER (Specify) MANUFACTURER INSPECTION AUTHORIZATION INSPECTOR • BY - CANADIAN DEPARTMENT DATE FAA DESIGNEE APPR OR , /lc OVAL DESIG WAN STATION CERT NATIO IFICA OR Of TRANSPORT INSPECTOR VACTION Of . TESIGNA NO. N TURE OF AUDIZED Of ARCIAFT I DWI UAL • I,2.- rb • .. 30-14 ,do s^ . • • _ .. .-.._ ." ::,e4;). •• • EFTA00277930 . NOTICE . .• . Weight•and balance o- operating limitation changes shall be entered in the appropriate aircraft record. An altiratiOn must be compatible. with alt previgus attetations to assure continued conformity•with the - .. applicable airworthiness requirements. • • • • • • 8; DESCRIPTION OF WORK. ACCOMPLISHED (if more space is required, oltach additional sheets. craft nationality and registration mark and date work completed.) • Mounted T.T.G. (Time to go).Preset•Unit forward of center console, below existing Radar Indicator: (.5# @ Sta 210) • IV. Meunted .D.I.U. (Digital Interface Unit) with suppliers rack on shelf adjacent to ATC-1 Transponder in A & E Bay, R/H Side. (8# @ Sta 463) Installed 2 amp klixon CB on:fetwara-end pf.#2'Essential Radio Bus CB .Paneli. • '.Left side. of cockpit. (Ste 261) • • • • Installed wiiing and associated hardware VII. Complete system installed, tested, and operationally checked, in accordance with the manufacturers manual #910600, Tenneco Inc. Interface Wiring Diagram . 011586, and acceptable methods, techniques; and ptactices per AC 43.13-1A Chapter 5, Chapter 11 Sections 2 thru 7, Chapter 15, AC 43.13-2A Chapters 1 and 2, • EFTA00277931 FAA MCRAE REGISTRY CAMERA NO. adell••• DATE: v i - g9 • -7"••• - • • • aW 4440%90 a AM /043-83 diseer 1PI WOO X Mt acts ets.sAse tur Att n. »s nit a - 1 -5 3 ••• v pc Gun awri--;-•? AIII.fR0W 1OO A Aso Ott/ VIC44'0 1444 0 r DC Revues POSAM Mus—ia — ;--W S ELIMINATE ALTE ran OCU ,GOWN. WAIT+ • (0101 Jfr 39,t R r/Pt MANSE. PEZ OCh LOG It 2S1 moms bre your- 4921/14 L4A I' -ist RIN+ PTIONAL CASE PER OW LOt S 29. RIN- 30Erts tea A CABIN c ~isn't* OM LOS s 36e It MY am OWN« CAMEL la OtS. 'Ear l 44 4- Ott ans. CONMOI. UNIT As RILay. loff..12 05iro4; 1:bukisr-teP05Iraesen:pstkeay.,! vipka - C (DCI4 WALL ortJ.E. fl CO To 1(42 Se 6170140 EZhAftV IS ON tilem. • 3 A nurse: conraot nkrPM30 Onal P142 49 GNO AND Ottio4W. MELDS MAT DISPLAY.. ) . YIEL DS 11413 OISILAY. Pnal OPEN AND AfA130 GAN 30 OPE N ALT S(NAYES OLSAI..11.e P44.29 OPEN AND PIN t.060 DISPLAY. • ~21 GINO AND fl y 30 0A/0 TIELOC. ts/ UNINSELT10A/ 115 /UM 4:*e. Okilla 371 CAns Atft£StmtE ~VECTOR Mea Dui . tria le %stir) . is eaWark, ami. tAM£ was 3P1 ØØ as TAW To OF es Z3 t• PORF OF --.Sicsonst_ Cs. ;pc irTERFA TC Or Wu AV AstA te: .1.64k6 J~/46‘7i2 1.1 MX ~W ED , _ /7 ø .1 C.44tutEt tan au in rJA te_setwout [ant Pea n(4 NEnalFFs/ NrA 1- 6 7t ooTA (Kr . tµYA our. 7 TS oisiN - 6-(1404b 8 jeCITE BEN/a1 7 a. Can Awe ors wag on s r-sr ant 54 ~NS .04/0 111r ) RN sr? insur VHS Z 241 BUS. noso fr otwrort. atones* twat (9 AM MUSIC 4/4/1 1- OVA/ AND le2 2.4V SVC 3 gasp DI AND 84 IDARIDD nor use stnei sneryz ARA•tC 414 IIPLIT . WOIE: AU-17110E ENCINO ann miIPUT1 ARE REG4ft£Q annee P/J- PLA Y W AR//AC 419 141 11/1: oersinEa P7104 ACOSTA fox REPEOXE roc osr" ohm AV Conifer 7S /4- 47 10 PIN 5, 22 SPERRY AZ-243. CCIPINECYOR • t3 47I4- 47 ro sin 4 IND 9J/4 -44 ro rain. ADS IF ‘ 24 2 fVK£ 010~ BE USED FOR DIGITAL 4,2 AR/NC ea- ast-is rsys ot one CONNECTED. art AC/NC CAM ITAL ADS nor asap- BV #2 INS Ode ONE a - DIG } I 17 YOKE Ow, 83331 2 WIRE AND t nS. TOC IALT a 4.11/K OUT /WY "OUP ar wswecreo IF AVADABLE.. 4. AVOID swore& cost WITH oraDIRJce IttaRAPT WO/N& LEAITZ MOWING. morn ~TM * • NAV E AVS ZDA TED "setter. ALL .11/1aDED Inter 117 rani 3. rn • 33 sinew: ro at atenfoco TO can-wa 45 RACA' END. • At MADAVID 100 D/D Ts team/re-4:os° ossners e «nu. 44 At AND At OZUI COVACC71X r>/OFTN. goat rot MAW» SE ta/C433 IN tan' sun 35 24MI, OPTS:WILL CSCEPT Ate aura /moor. B NOTEst: ream.ormatwin sPECUY 3 ED, : CONNECTOR. TABLE RET soarcedmom 1 acre-aszsre MAC P., W se LPL earnenzscuucu-oonrum 6/sole ' 2P/ Pr PrOGI - 43-15 PTOcc-S-÷s 625'00 8 0' 442.5- O/P _3 PI In 3 /24 F -I41-12.9 443 Il2E - /F-.7S 4250/7 49 in' i4S31.22E-444-/PS HS3 EISC tlut..c NO 625O/9 30 3.12 1/3/1i .94 ati • 34 Ls I ()MI COO( NC(I0 Offif MIA? 10F.PariNG IVA .i 140110CLATUINC ON OESCSNITON I • ' . PARTS UST SeNaNCO ' man NO ASPIC, MICORIOCA TED ~En OMONFSL Int ~MU . OISCatias 7211714 CA 421 SO ~9~a Me. HitfC MYFORD W. ~era otessios skails • APINON•45 OlfC = = ''t"..1amoretten larl13 1NTElittNAIECT WIRING u aiLDED AIRSHOW 100 WITH DC OLNY INC. FO. SM tom socsa so; 'fl. 910600 gvp . 9 20410 F e. D Ufa ON SEEET 31 IT.ccT / Of Nal 00 NOT SOU Oliastosa Ina 4.-- T APPIXATiON 3 2 _~.wi.-s. ea. . • . • 4 •1' • : C.:;;; .. •r •t .•1 • • 7 :•_7 2o.. Svc, :s>.•••:: • ..b. •-).:;•;if:. — nee, •• es •' plit;49•; • • 1 ••• • ' -• :“" •154„; EFTA00277932 et I PYDED our 75 al• oars •••• } az Argitoc 4141,14Z 9 O.47-A — 2•M/l% It REF AMEN TA 170,0C eft SIG .1. • r/HE't kr av Dosnm Com-Ro S16 - • . .- .' • -115%021.771 . •*.seiffirs ISMINItrrai sfaitW.-e-A-6ta _.• ;.- - • • , EFTA00277933 - FAA A IRCRAF REGISTRY CAMERA EO. • DATE: rtami /04J-03 Akre Dc is 0git -AGEg0 An0 arr.& r0-20431tate A Atin tsetil VOCa .,_ 12 ft-fil a," TERsaTE DLL COMV a GUIMINATE AL 2•I • trzonm toe DIAPMG PER ora22004 gott0 O W tot • 2.96 PE R D Gaol 164 30CTES 00,4 MYOPIA: 77 04 LO G a c LALIM EW If. »tor OMNI Ca M at SZ E tie M r.: in pa, O/LTLAT Powhtg 15 er.weE.23 1, OMma i4/ doFf- £7,. 15 Suoy1/Eli UNIT /i/ A L L 07 74 WO* INFO Mira. "'UK Iko ra Rd it le NAP it ON WIELD. &ROUND RETURN VCR • A agrater LL' ogro ,c9k u TAE ouPtiV. Gam AND ems° O PEN naps MAP DISPLAY. YIELDS INTO DIM «. -erf Ar Etm O PE N AN D Ft.W.30 6.40 ~3 0 OPEN ALTEci va re S D tsietny. D DISPLAY_ Ram?, OPEN AN 110 YIELDS L060 n 60 40 AN O Paa 30 4, R aV l. IMU 76 "(MO ba ab lt eCCOW CaUMEtT PROW 3S1 (ACM Atta 1 SW CAME won tiM E W ae 3F Ottitidels *3 tie r to l -nb r OF /KU cmar 23 t • ro a etc fetsonsL A enalar-S Ae«.0)14 e.g. TIE RF At t O FOC pericoic. Ot 43 marstrauct 7Y Assn ZáMfUlElt. mate« ItS,t3z font nm .: bescoutTOM Vat PE itérimmi MU AI OW JEte- ‘. 11,0.TA r.t 90617. OUT 3 ton air . • Z , rT DA TA Tra .m.NA 7 jct. ATE & W/NO ST S 61 0MMS ag FOt asmaCe rs wing at e I t.v / ta ut a z 241, BUJ. 2W 60.0 arli ermor ov et. 4031440 pi sw is le .4 to w n ~A er itmo az tita lia OO ~O a MillatCarf IN AP T av WHEN ~at 429 C VIDEO ammo Or gore: ~Iron ~D N S avato- Nor IWO .rpur pa irr re rra y. ire alarea arrrurr£ or PO T. f AR E 4 AW IL1 7: IN /AC 42 AIZILITA OW AR OBTAINED FROM T AY CONNEC POE oar . DMPL Pot REFERENCE: 77 IA - 47 TO PM/ 5, t CONINECMC SPERRY AZ-Zet 1-T14-44 TO rum. TO P/ N G IS O 7. TI A- 47 S IF FOR DIGITAL AD C 2 W itt tH OLICO BE VIED BE an t &In AR/N AtiNC CAN NNECTED. Art ED- IN S OR ONt CO DI GI TA L. ADS flOT US . OAV er BV si2 INS 04 G WIRE , to». 2 WIRE AnD LI\ roe • hut OR ow o AVAILABLE- PL IT .11 AR ILD BC convocre AXING •O UT orate ~CRAFT "Ne COAX win< a. AVM', /(01/7 CYLALiNTt. E PROOLICYN6, ewers.* AIOAT a JACKET . ico co m ar TO wave ~Are R SHELL 3. AL( .n wr CONV EC TO IMWACCO TO SMIELAT TV BE RACK EARS . i00 DILI AT ARTNOW AX. 04400ETER CO .caumee case a at Ant Ar mix 1654 name) ap m ee ra c IPLICED Av TO R WNW RUN 0/0, it POWER ~P OT. 7' 1. L EXCEPT fa 11 24 AIV O OP TIO NA ECIIII£0) runtrr omen's:Er EP LL "NW 0 E CON.VEC773A TABL *PAC P/N ON ALTERNATE C REF OU TZ IP TI LY-000ITZto) 61s-o/e In OI S7.1111PC7t3ZE 625008 Procr-8-+S 20/ RPTOL£--8-lS 625Die . 53 ,2 6F -1 0- ap 5.91 11 6250/7 IP S 33:12E -M-425 3I 22 E- /f- 3.01 nS 6250/8 20 aNC etxx HD -3JZ uslv 4g rain OR flll COCRIPTOI l iatioTcoor Mine I•1 • AIMS (Zr rev 410eC. ~tattoo ILI 20 CD. 77.137/N CA «WC 147F0A0 IRING INTERCONNECT W 1 0 0 WITH DCU A IR S H O W '910600 gEVP 920410 'parts • of: • : ,SHEETr 31 APPUCATION co NOT OAMMNS 2 r- EFTA00277934 • ORAIRMIDif Of VIANIPORTAVON ' • . .. • Fern t r ...vgat Bw4ei .... 'SPA AVIMIOt4 ADMINISTRATION t• • . .- -. wren No. 04-R06-0.1 FOR FAA USE ONLY MAJOR' REPAIR . ANO .ALTERATION, orna IDENTOF (Airframe, Powerplant, Propellers, ei Agi011arim) .‘ # • ak , - INSTRUCTIONS: Print or type all entries :Sri PAR 45.9* PAR 43 'Appridlx Di red AC 43.9-1 (or subsequeist revision tbeteci .: for lasaructions sad disposition of this form; -. ',‘ 1 . ; •••••.' • - ' -- - . _ MAKE • -_ • ' -46-MODS; ' • • '. ' HOF I NG - . 727-31., , 1. MAGNI SERIAL NO. . • NATIONALITY AND PROSTRATION MARK ...... , ann5 • - USA N51.15T . . HAW (Ais them, on. registration eartIllare) ADDRESS (As.showr on registration certitioste) • . .16951H3.F.K. Blvd. • .__ TENNECO INC. _ .1lottiton: TX 77032 fr A. (Olt FAA OFF ONLY >. , onvogru ilsoraibs rife.; • . imposorwasse ss. is scIt.to.itiiiip....rf:47:3364:r... irma .. id . t • , 4,11: IDOMFIGTIOIL 5. ME UNIT MAO .1 ,,..„. - MOM •• • .7 SUMS PIO. ALTelt- tiPAIR • .: - ATION e • . J. AIRFRAME werwanneoes•444.• iitt dirtErill; Orr' V aboar) mirOimistraus . ,. • . . • . X POWERFLANT - • - . . • .. • _ . , .- • . .. • ' • PROPELLER C ;-- • ' VIM APFLIANCE '` _ IMNIPACIIMIN ' ..- ' i. (OISMNITT _STAMM A. AGENCY'S NAME AND ADDRESS S. KiND OF AGENCY C. CERTIFICATE NO. G. C. Kolb el.t. CIETIPICAT19 MIOLANIC Tenneco Inc. POUCH OITOICATITS MICNANC • 16951 J.F.K. Blvd. X • FINTIOCATID SPAR STATION205-10 Si. TX . 771112 leNUIACTVIllt D. I certify that the repair and/or altrrittion made to the unit(s) identified in item 4 above and described on the mete.* or attachments hensto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulation, sad obit the information fratthiSiti herein is tree sad correct to the best of my knowledge. DATE SIGNATURE OF AUTHORIZED INDIVIDUAL • December 21, 1984 - _....e.... "LS _ 44 II 7. ifilliflU. FOP 1 TO SEMICE %neat to tin autheriey awnpasoes specified below the unit identified in items 4 was inspected in the manner prescribed by dr Administrator of the Mad &Woe Adarakaratier and is Etatinovw allijEc hp OTIS fliptin, -='-, M4 PLY,• IyallOS a MISS OWILIFAltiat 1141PICOON AUTNOSILATION BY CANALMAN CaUITMINT MA MOM X✓ WAS STATION Ot TIA14,041 !WC" a - fX ASSAM DATE OP APPROVAL OR CERTIFICATE OR SIGNATURE OF AUTHORIZED INDIVIDUAL • REJECTION • DESIGNATION NO. Dec. gat /940k - Baer-L>a . — . ..dies. - d..-- rce.er • • O. EFTA00277935 . . Weight and batons or Operating limitation changes shall Wintered in Otis appropriate aircraft record. .An altoratiOn:Must be'compaHble with all previous alterations. to assure continued conformity with the . applicalskainiartldnsise requiremeati.. O. DESCIPMOM•OFROMI A(f.OIRLIMED (0 more epos* is required, attach - identify with oil craft nationality and rogidrationinadt and data- work.000tplohod.) • •-•;V:" . . ,•• ' ' . 7 , 77 .7 t.;1 '7". I. Thermador Trash Compactor P/N TI4C-28B S/N 3060438, Having 6 AMP,,,; •,:,0 t.itenioved • 4 a • load, approved on 337 dated 9/19/83. • AL:- Installed:Montgomery Ward Trash Compactor P/N SBW-5235-c S/NT481100442,- 1. _ •AMP Load. Having.10 III. Unit ftinctiOn tested. iatisfactorily; unit operation does not adVersely - affect the safe operation of the aircraft. • IY Installation was same as previouslylpprOyeCoo:N505T 4/01/81'for - -- • -1 Aireseardh Aviation Co. , Los Angelei-, -CC-- 1See previous-weight and BilanCe 's Data Report 11C-3688;) V. Installation using acceptable meaies, techhiques, •andfirectices in dente With AC4313-1A Chapter 11, and Chapter 13. • •VI. Weight and Balance and Equipment List Revised I •_. , C t) iv e>•.- r.,•• • . • ;VI • I Viq',~.• . 71 , a • A ,.:144.0 • & •-••-• e • . tc: :Ism • -7,1•7ostip •., •:* •• rti -.• • • L. • - •••••:. : • • . • !- • .• - : . . . 1!.7 . t •• • . • • - . • EFTA00277936 a ll..... .. ....1.1. 4AIENT Of MANSPOIHATION Form Approved • . CEDE AVIATION ADWNISTRADON - , • Bud;et Buren No. 04-R060.1 ' • t FOR FAA USE ONLY . MAJOR REPAIR AND ALTERATION zjoarrgri i (Alrfromi,.Powtriitant,.Propollir, or Appliance)' . INSTRUCTIONS: Print or type all entries. See FAR 43% FAR.43 Appendix B. and AC 43.94 (or subsequent revision thereof)' for instructions and disposition of this Cos; . . . - - -- - • MAKE MODEL - .. • - Boeing 1. A11101411 SERIAL No. •. • - 77-31. .. NATIONALITY AND REGISTRATION MARK 20115 . • . . N505T NAME (As shown on registration certificate) ADDRESS (As shown on registration certificate) 2. OWNER' - •Tenheco Inc..-:.. ' ..-. . 16951 J.F.K. Blvd: i . Houston. TX 77032 3. FORMA USE Nu • . : • . • .. , . ignitionsIsmlilimIse is unklISIRIMP :• - tilleiteNMS and Is On/1W Ss. i - , ' Wiest to orkentay Is II •I • ., 13.7 D*). • : . :. 4l -• • • ' . _ , . ,...........a. ‘..... •:pra. . - k _ - " I. Will IISTIRCATION S. •TYPE *SNIP SERIAL :40.. AMA- MAIM • . • 4...L • • • ATION • . • AIRFRAME' . •••••••••••••••••••#14 ilestrist in item I abowderamma re••• • • : . . j(X POWERPLANT , • , -• " I .. -• • •• ' • ' .. . : ' -c.5 ;• , ..,.. • . . ) ! .• • . . . '...• . ,• . • , , FILOISLEILv. •.. . . . . ....•••••-• ' - - .. - . - .•' ..._ : . . .1. i :.• .; . • - •• . .- .. -. APPUANCI Lionisation t - ' .. ".. • . 1.i.,. ••. a : Jam - £ collethITI STATHAM • , A. AGENCY'S NAME MO Amens • t - y - IL. KIND OF AGENCY C. CERTIFICATE NO. • tit. COMFOCATID MECHANIC Tenneco Inc. •, MOO* anararto istamtc ... . . . 16951 J.F.K. B1vd . rTrinift- ' . • Houston, TX .' 77032 . ' • x. pumnommmmessmnom '205-10 • -. • D. 1 certify that the repair andinialteritiois• snide to the unit(s)•identified in Item 4 above and described on the reverse or attachments hereto have been oat in Scootalta with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the infortisatioo famished, berth ii was and correct to the best of my knowledge. - • i ... ' . DATE . •!•• ' .. : • - 1 '';' . • SIGNATURE IN • 8/3/84 ...!: •!.... : ,. ;.• .,- •:‘..", •'. - • ,. • . , 7. RIROVAL FOR IfIRM TO a Pursuant to the eutbarity given persons specified below the unit idendfied in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administradon and is'. AP/MOVED ORFJECM al Ls RT. stistacts . . spareast AIDNOINZADON IV ... . ... . . ...- .. . COMIX034 DEMITlect PM OWONft y CAM STATION Of CRAMPONS IMPECTOR %en • • • DATE OF AITROyAL. OR CERTIFICATE OR . .... . SIGNATURE. OF : INDIVIDUAL • REJECT107 g it DESIGNATION NO. 10 /14 ' ‘.7tir r ,. . rditiM; TA: - " 1Z-- . • • • • %I "flet. • ••• EFTA00277937 NOTICE Weight and balance or operating limitation charigei."shell be entered in the appropriate'aircraft record, 7 ' 'alterations to assure tontinUed canformity with the previous.alteratio An alteration-must be compatible with all previoa applicable airworthinessrequirements. •• I. DESCRIPTION OF WORK1KOMPLISNED (If more. space is required, attach addit I sheets. Identify with air- craft nationality and registration. •mark and dote work completed.) -- - • .1 VIDEO ICINITOR ND VCR -INSTALLATION ' . ,L1 ?P•41.1, . Revised -interior (which was preiiously installed and a "proved by Airesearth'; Aiiation Co.. Los Angeles, CA.:.4/7/01 on report. No..C-3588).as follows . Modified Coat Closet (Ft/H.Side"..Sta..814*t5) to.remive_moUnts f.01‘ . installation of the following: * • ;•••:k.r.;1; yipeo• Recorder -MitsubishiNS-33OUR:' it;;;Ithed.,PiOnttoi,,,: :,mit.;sithisht CM-1901 3. Infra-Red Transmitter Nady 1RT-200 -A: Altitude Cut4Ut Switch -.Anint 90500 ,5:.' Power Receptacle ;":7777K1 • ...,.: . .6. : Pewer:SUpplY..:AC4C: AdiOtehl':',:.NadY,I.A72420 ......:._:::: ,......: . • .i i Modification of coat clOset in accOrdence:With Structural Substantiation RepOrt NO: 243. and. Draividg-No. 266e submitted and approlied:on'FAA.fOrm.8110-3 by ..L A:. DOgel by.i 0.4.-. it::Ttirettutoleelglileering' ,Company, Sin Antonio, TX. : • Reports and drawings are available to the AdministratOr:on-request..: ' ' ,.. .• , .. . f A;;', Pei,oer Supply as follows: • A. 28V DC Bus No. 1,(Drain Valve,: Shower 3. amp CB, existin g). . .• B. .115V AC• 60Hi (Utilit y Outlets Aft .Cabin -: 15• amp C8, existing). • ... • . : .• • • • • • • • • .1 . ! IV.. 'Utilized existing !Altee..755E:Speamers:at.Sta....730.0_. _ : V. 'Systems installation is in aceordanee "N505T VAdeo* - System': dated -7/26/84. : " • _ VI. All work performed utiliii0g4CciOtable methods, techniques, and, practices '.0er AC 43.13-1A4.- Chpi.15:6:04C..43.13,2A -Chott.: 1t6._24.. , . • _ . VII: 'intiallation- waefoiktiohally Itettedat ground level. end at'altitude dUring -performance check- flighti;ihd:.operitedsatisfactorily -404tdid:hOt adversly affect the operation. of .anY'.1)thet:licsterifs-._ . . - Rircraft' weighed ' ileighnana BelanCe-a0d at amended. .. ... . " ' - • - • • •-- ••: • . • -• • /10 *MS.GOVEMIliata PRINT.04.4 OFFICE: 1977-77,421/2 ••• EFTA00277938 • • MEM OF montoitinnow - Ff00AVIATION ADMINISTRA110"4 MAJOR REPAIR AND ALTERATION • - Fitdpmeived Beiges Bureau Noi 94—R060.1 ' FOR FAA USE *NIX- . s ONA6DENTMSATION lAirfr amok. Pow•rplant, Propelkr, *r Appleana) INSTRUCTIONS: Print or type all entries.- See FAR '43.9,, FAR 43 Appendix 'and AC 43.3-1 (or subsequent revision -6,-17>e, for instructions and-disposition of this form. thereof) . MAKE MODS • • Boeing •- - I. AIRCRAFT • . 727-31 SERIAL NO. NATIONALITY AND REGISTRATION A' • • 20115 . . N5051. i NAME (As shown on registration certificate) - ADDRESS (As shown on registration °edifice* 2. OWNER 16951 J.F.K. Blvd. Tenneco Inc. • . . Houston, IX 77032 . '' . 3. FOR IAA USE An I. . . . . • .. . ' ' . . • : ___,....... . . . ... ... .— • .— -. - . / —. , • - .. 4. UNIT IDENTIFICATION- .:. 5. TYPE Witt . ,SERIAL NO. ALM- /SPAM Anon AIRFRAME memomennennamne (As dasaind in item 1 above) XX POWERPLANT _ • MOMS roe . . APPUAtICE ` NANVIACOMINI • 0....r. - 4. OINTORINTf SIATEMBIT _ • A. AGENCY'S WALE ANDaRESS. • , • fr K*40 Or AGENCY C. CERTIFICATE NO. U.S. Cternicana maawac Tenneco Inc. twins OVITMCATIO AtIOIANIC 1695! J.F.K. Blvd.,/ - ...I j.:-. •X Penman ammo station, Houston, TX 77032' - '''' :205-10. . bat - tififimpArmana D. I certify 'thin the repair andiot ii/Miatliali'Matitio the ank(e) identified in item 4 above and described on the reverse attachments bent* have been made inateardateee with the requirements of Pan 43 of the U.S. Federal Aviation Regulationors and that the information fissnisbaLhereits:le !tend correct to dri bs, ofmytemerledge. •. . . .• DATE `;'.., i ' ! i ; ' ;.i.'1.• =Wart Of. . -" . ., . 8/3/84 . - .• t • - - . ‘,,..- . .. - fa MINI TO SERVICE I.'. ' • isenvia • Pursuant to the authority given persons specified below, the unit identified io item 4 waszbasted in the manner prescribed by the Administrator of the Fedetal•Avistion Adsninistradot; and is igi pPROVED. QM PmIttelininsl. . aiiiiii veire.." :.". itelebtleata isitte:MIAllUile... :'c: .. °M _. 4 ._ . '..::.c. . . .. . Nub, ottitanet: - - x ISM ;SIMON Of 17.011f0t1 SIVE= d i .• ... Of EIMOKAPT - • •••• DATE Of APPROVAL. OR, , REJECTION ' ' ' ' CERTIFICATE 01 .. .; . DESIGNATION NO: SifirbiPmg. OF . UTK . ,M.04'...t.-: - •: - • - ••:• ` 4 ..040 • • . I ., '• ' ‘ • ...... 8/3/84 • 205-10 • •S s • • • .1 ••• • ••• : • S. • • • • • • • • • . • • . • . • •• • • • • • p • •• .15 ", • •••- : c.f . -'sr.t .‘ ,;:ri gtettn. ;.;-‘.. • . - • ---- ••..• ••••••••••• EFTA00277939 AA AIRCRAFT REG TR NO. ) DATE: , I. "e".!'•• • . E - Weield'and balance ar..ope ot.npp limit Lion chaeges,shisn be enter.e.d inlipe.appropriate aircraft record. An alteration must be COnqicitible with oil:preirioio.alterations to assorseentiOuod conformity with-thit applicable airworthiness requirements. L7, • • ;_ O. •DESCRIP1104 OF WORK ACCOMPLISHED• (if more ipaai is requires attach additional sheets: , identify with oir- croft nationality. and nigidrallon.:inadc. and dcd• work-annialided.) '". " • ... .• . • . - BODY STATION .950 BULKHEAD FORGING REPAIR • . • • .- • .; --• • Repaired left and right BS 950 foiging, lower Section, *in:accordance with • instructions• provided by Threshol d ,Efigineerinve.ompany Of :San Antonio, TX. Subject inStrUctionS..t.are identified, in,:i*.eports:K.• 242 and No. 244. Reports We're drafted and apprOved'on- J. A. Dii01 fp E .R and'. are.:avail abl e the"'Aihnf strator -on: request ' = • _II, All :work performed utilizing accePtahlk, methods;, techniques,- and practices . per..AC 43.13.61A. • --7, I I I .• Airctlift and' Balance aliendecl..h -:- • • •- - • - • • .. • . . ADOIT(044 SHEETS ARE TTACH6 •• • - • • • • . , • . .: ,.. . ..;•-•••• --•.• „..; 4 .0 . 411, .. ',':•X•V - •_.... , • EFTA00277940 • . (,- VITNERITOP.TRANSPORTATION . . COat Appeared • flittsif AVIATION AomimstRATioN Budget Bureau No. 04-Rollo.s • FOR FAA USE ONLY • MAJOR REPAIR •AND . , ALTERATION (Airframe, Powerplant, Propeller, or Appliance) , OFFICE IDENTIFI ATION ..8_7 ' • e. INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix ... . . . . . 7.4sub2s!quenr reeis•ioe,thatoe . B. and AC 4319—I. i ot for instructions and disposition of this form. I MAKE MQ0/1 727-31.. • , - ≤• ' . • I. AIRCRAFT Boeing ' SERIAL NO. 't ' NATIONALITY AND REGISTRATION MARK 20115 , - U.S.A. - N5051 — - NAME (As shown on registration certificate) Y. ADDRESS (As shown on registration certificate) . 2. OWNER 16951 J.F.K. Blvd. Tenneco Inc. • 1 ... a Houstor, TX 77032 • • 3. FOR FAA USE ONLY . • - ,.. , • •'-• •- 1 • SliarnsiereetsWoremaInloor Omit alre inie-- 1,-, i:.•,:. -: ,•>1 ., _ ISSIRSell 6 gMy for tho f 11&,•:.: .:!:...,. .t. • Ishitieboti , .. -.. Set IP ea* .. , . , ULM • .•- ' -7 619 • ' I - 4.•0111T IMMOLATION • S. TYPE UNIT MAXI • NOM • . MIA* NO. WEI- MAII ANON , . • - • -• AIRFRAME . 4****1•1•••••••••••••• AR deicamed in awn I abovounaroonekeenosee X FOV/EPPIANT • : t - • ! ::- . .. PROPELLER :...; " ' • - . Mt • .. ._ . . . -• • •. APPLIANCE •... ... : NANUIPACIall . • , .,... . - . - -• ' TY STATISM 6. .. c. A. AGENCY'S NAME AND RODEESS . & XIND.OF AGENCY C CERTIFICATE NO. *S. OIRITFCATED MIKKAPRIC . Tenneco Inc. .. 'MOON CRIMPIC.ATED NIGIANK • • :16951 J.e,..K. Blvd. Xparincaras RIPAJR STATION 205-10. Houston, TX 77032 . .• - LoArrusavate . . D. I certify that the repair and/or alteration made' to the-onii(s) identified in item 4 above and described on the reverse or a attachments hereto ban been made fits:cordate with the require:Senn of Pan 43 of the U4 Federal Aviation Regulations and thin the information furnished hereinh true and correct to the best of my knowledge. DATE SIGNATURE OF *mat= INDIVIDUAL r- • -.. 7/19/84 .; . . . . - ' ..• -- idi—. • ....,..rder ..:. F. APPROVAL FOR RETURN TO soma Pursuant to the authority given venom specified below •tbe•unit identified in item 4 was inspected in the manner. prescribed by the Administrator of the federal Aviation Administradon.and is •IEWPROVED ORM • . MA RT. PANDA= NANUTACTOOft. eistecnctrAunionrAnoii. Ma Seits) N. ONSPICTOS BY ---..- - . .... . MA .DISIONSI - eon STATION Of TITANSOIT INSPECTOt Of ANOWT • DATE OF APPROVAL OR . CERTIFICATE OR ., SIGNATURE. Of AUTHORIZED INDIVIDUAL . • REJECTION DESIGNATION NO. . . I • -7-0, 57- ay .72,os-io ,,, .....S • .• d Pr30. levaL.c. isj nr-- • • • !j sz ..; ;. • • id s *Pk: • •- tar/ eie 204 011 6f ; - • • : — 'sr e• , . . .• . . • • • • 1• ••• '-.• • • ...NIZIEL.:•••.w.......•.•••••••••=.•••••••• •••• ••••=immm:PA.momi: EFTA00277941 Weight and balance or operaing limitation changes AO be entered in the appropriate aircraft record. An alteration must ,be compatible with all previous alterations to assure continued conformity with the appliCable airworthiness requirements: • ' 8. DESCRIPTION Of WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify with air- craft nationality and registration mark and date work completed.) • .. . -. INSTALLATION_ OF 115 VOLT SOCKET .& HAND VACUUM WITH CHARGER BASE. Installed 1 each Cutler; .- Hamer aircraft electric safety socket - P/N1.777-Kl.in rear cleset.rleft hand side, station 1137. Wired new • • plim'itite-lititchtng.15/1i5r.volt AC supply from utility plug in vanity. . „K:n.7 rf.:1z; e: • ;;; The safety socket incorporates a switch, which connects the supply to the vacuum:.battery Charger-when the charger plug is inserted in the socket, and is protectid ,hy i'250-MA:fuse. .• _ Installedthe following Platird adjacent .to. safety. socket. . ,..:`. .._.....:' , • ::••••••• Asir me sage imusomom oricamotethavii,ants 40 . • ire, tnie0 IV. Installed-1 each Black & Decker cordless vacuum clearier with bittery :::charger base.P/N 680982=00. Thisziniit is Underwriters- Laboratories • - • approved- and has the following specifications: 120 Volts, 60HZ, 5 watts! -• -*7.2 V.D.C., 125 MA. The total voltage.draw from*thebpower supply will be approximately 1.06 MA::, ' . - . V. The charger base is mounted adjacent to the electrical outlet at station *1137 and.attached using AN526-8-32.screws, AN97073 large Area washers and AN305-8•,32 fiber:: lock nuts. . • • 4`F, VI. •Weight 6 Bilariee and EquiPrnent.Lisi intended. ADDITIONAL SHEETS AM ATTACHED . itus.GoverisoitmPRINTING OFFICE: 1977-771421/200 -11c.- • ,r•zrt, A ••": • • V • . EFTA00277942 DATE: yma? _K., DEPARTATIrk 4 - 1 TRANSPORTATION. : .' . I Form Approved . c ci Budget Bur.rau No..04-4060.1 . FEDERAL .A.ViaiN ADMINISTRATION • FOR FAA USE ONLY. MAJOR REPAIR AND ALTERATION ••"• IDENTIFI OFF a TION (Airframe, Powerplant, Propeller, or Appliance) /zor (-5Pitp0.3 INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43.Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. • MAKE MODS: • 1. AIRCRAFT BOEING '727-31 SERIAL NO. ' NATIONALITY AND REGISTRATION MARK 20115 USA N505T NAME (As shown on registration cortificatii) • ADDRESS (As shown .on registration certificate) • 2. OWNER • ' • 16951 J.F.X. BLVD. TENNECO INC. -,HOUSTON. TEXAS.. 77032 3 FOR FAA USE ONLY .. .., . . s. .. ., • • •-. .... - , .. •11- - . .... . -•• • ,• . - 4. UNIT IDENTIFICATION • S. TYPE • , MODEL SERIAL NO. ALTER- UNIT • MARE • i REPAIR - . ALT , . • C4 1-1 ' *or AIRFRAME iannatimeno•tanne Asderribird in 'item 1 above)' .x • POWERPiANT . ._., . ) ......... i . . . •. -.•• -• - PROPELLER I . . • I. r :I: i • 4 • • .., • - - TYPE ! ' " • -. • APPLIANCE MANUFACTURER' • • ..,' ., ... .. —. .. , , . . ‘. . - .". " 6. UNIFORM STATEMENT ." A. AGENCY'S NAME AND ADDRESS ' . •!,:• - • : S. IIND OF AGENCY . C. CERTIFICATE NO. G. C. Kolb . 'Li.. 4.- . .. : ..:..; :. iil it: . U.S. clISTIFICATE0 MECHANIC • • Tenneco Inc; : i 'i • il ' : :. : .0SEION tEETIFICATIO MECHANIC ! .A:+ • P 16951 J.F.K. Blvd.. - . . '• • CIITHICATED REPAIR STATION - 1337480 .s. ... ., Houston, Texas.:.,77032. . . -t. MANUFACTURER - . - . . •—••• .-. . . D. I ::ertify that the repair and/or alteration ;nide to 'the units) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulniuns and that the information' furnished herein is true and correct to the best of my knowledge. : ••• • ..• —• DATE - • 'Iri• .• 'SIGNATURE OF AUTHORIZED INDIVI AI. • ' •• •' il i•i-ii . • i '• • September 19,' '1983' • • ! 7. APPROVAL FOR RETURN TO SERVICE Pursuan tit the authority given persons specified helow the unit iilentified in item 4 was inspected in the manner prescribed by . the Administrator of the Federal Aviation 'Administration 'and' is 014 APPROVED 0 REJECTED FAA ELT, STANDARDS '" •• . -• • , • •0 , • : OTHER (SeA6601' ' I I . ' 3. .'; I I ' i z-- - • mmairicruieit: .. . . . . INSPECTOR • BY • CANADIAN DEPARTMENT • • • f AA DESIGNEE • REPAIR STATION • • : I OF TRANSPORT INSPECTOR ' OF. AIRCRAFT •-• DATE OF APPROVAL OR CERTIFICATE OR ..c... SIGNATURE•QF AUTHORIZED DIVIDUAL. • REJECTION ' DESIGNATION NO. ' • • •• • 'September 19. 193- IA 1337480 1 -. .:.. ./...--- • •• P •• • . • EFTA00277943 ... • . NOTIcE Weight and balance or operating tirnitcsiion ;banes shalt be entered in the cipOrOpriate aircraft record. An attoratialniuse be canspatible ., ,igs.ag.grOiaus alterations PO Waite continuedconformity with the appiicOble airworthiness requirements. . . B. DESCRIPTION OF WORR.ACCOMPLISHED (If more space is required, attach[ackiltional iheeti.; ' Identify with air- craft nationahty'and . , ,. registration mark and date work coinOeted.) i • ' • ,: • , If ! Removed Montgomery Ward Trash Compactor P/N SBW-5621A S/N 08D-00489, Hay.ing -10 AMP Load. . . Installed Thermador Trash Compactor P/N TMC48B'S/N 3066438, having -6 AMP ;- load, -sanielocati0n. . : bnitlfunetion tested satisfactorily; unit :operatien.does_ not adife'rsely affect `the safe operation of ,the aireraft : V. Initillation was, replacement of unit previciUslyrapproifed-447-81 for Airetearch Aviation CO., Los Angeles, Ca. (See, previous _Weight. and Balance 'Data Repiirt #C-3688.)• V. Instal ration using acceptable :Methods. techniques,* and ,praCticei dance With AC43-13-1AChapter ;11; and ChiPter.13::. VI. Weight :and Balance and. Equipment ListReviSed. 1 c411010:0•6%, • EFTA00277944 am" D OP TRANSPORTATION • FormApproved Budget Bureau No. 04—R060.1 FIDE WATI0N ADMINISTRATION FOR FAA US£ ONLY MAJOR REPAIR AND ALTERATION .. • OFFICE IDENTIFICATION (Airframe, Powerplant, Propeller, or Appfrance) . . • 414-4 f5i2 0 er c Appendix B. and AC 43.9-1 (or subsequent revision thereof) INSTRUCTIONS: Print or type all entries. See la 43.9; FAR 43 for instructions and disposition of this form. . . , . . . titalei • • .. MODE! •.10-31 c. • • 1. AIRCRAFT sittido.• .. . • • NATIONALITY 'AND REGISTRATION MARK . . .. . U.SA. 450ST re ;tertian certificate) NAME (As shoWn on registration certificstsj .. ' trekt shown Ina. • -• 2. OWNER TO ; 18C. . . • •• tea, Teas MOS • ... 1. FOR FAA USE ONLY . . -. , ... _ . • . . . • • . . ... ... . . , . • • . • _ • .... . 4. UNIT IDENTIFICATION - S. TYPE SERIAL NO. ALTER- UNIT .' • moon - ' REPAIR ATION ' • ' . - • . , AIRFRAME ' tnynonieisinns• (Ai described in darn I obove)eiNtenn eene X . • er • - . • . a POWERPLANT ;. . . • , - PROPELLER s. . • - TYPE .• ‘ APPLIANCE MANUFACTURER - • AA • O. SONORITY STATEMENT . A. AGENCY'S NAME AND ADDRIAS • . , p__ I,1.P4D PF SlocsENCf. _ r it. a .. CERTIFliATE NO. . AinseardsAvlatlea Ca. • .. . .. .. . . D.R.cORTIPICATED MECHANIC' ' • A/C CLASS 2-3-4 • i-z-& 4150 Donald Donlan Dr., ••..- • it• HAMM FRITHICATED MECHANIC • •4. RADIO CLASS '_ a_ 1 _ actitIPICATED REPAIR STATION kJ MITED IPSTR UM ENT Long Snobs CA ,. 90400.. ...: . • • . ".. .• ... t pANUFACTUREI ' • SioECIALIZkID SERVICE D. I certify that she repair and/or al • ion made to the unii(s) identified -inPart item 4 above and described on the reverse or attachments hereto have been made in accordance With •the requiremen ts of 43 of the U.S. Federal Aviation Regulations the best of My knowledge .' : and that the- infornistion furnished birein:is true and correct-to DATE 'di SI • TU OF.A , IVIDUAL .. p• • - . - APB .1: 7 1991: . ' ' • .- • • . 7. APPROVAL f R RETURN TO SERVICE Pu suan to the authority given persona specified below the unit identified in item 4 was inspected in the Lft) e .. manlp "egiptliy . the Administrator of the Federal Aviation Administration'and is "APPROVED ,CIRR)E OTHER (Sperify)' : ; ; SAY • - FAA KT. STANDARDS INSPECTOR . m•smunclutut • . . INSPECTION AUTHORIZATION • • . /98/ BY CANADIAN DEPARTMENT Of TRANSPORT INSPECTOR • - `GB Pane% FAA DESIGNEE X REPAIR 'STATION —‘ I 65 • • DATE OF APPROVAL OR • ,' CERTIFICATE .0*-, ' SI TURE AUT IVIDUAL • •• . ,...;..!. . . REJECTIONApR 1 7 1981 itt oidgiN NO. E • iiiiilik atillib . -• : rn elbalej*Ir itteN •;.0 EFTA00277945 AA AIRCRAFT RE RA NO. ga, ancisa""J".61.2 • • • . • * • 0.- . l. . " t • . OTICE Weight and balance or operatintlimitation ch ng(ez shall be entered in the appropriate aircraft record. An alteration must bp'compatible with all previous afteeatiots to assure continued conformiti, with the applicable airworthiness requirements. DESCRIPTION OF WORK:ACCOMPLISHEO (If more space is required, attach: additional'sheets, Identify with air- craft nationality/a0d registration mark and date WorlitomPleted.) 4 installed-on'of Dual Delco Careisel .1VA.TheitiiitifiviistionAiltas.01 74accordance with STC SA4164ME.Ammendeset dated.April,16,..1981_to include,: ' 727-31 model. Flight manual.seD004.11t-idlieed.datede4Pril 16*,19$1e- , ..• •• • It his been determined that theinterielationihip.between these,changes and. - : $ • any other previously. pprovad.ladlii4Otions will_not.adversety_effect.the 44rworthiness 014,this- alraInft • . . • •• " . Air0raft.hli been eeigbed. ileight_and balance and equipient_lief_reirtsud:' .The end. . . . • • • ) • • . : ::$. I -• t . • ' • • .•:.'• !. • . $ . . . 975-03.0.7 i7021-14/673-200/ 175 ."• . . • t( • . - .•• ' •fr V c.Y.1 • •4' .. F •••• • t t • . . • . . ••••$‘4:4?..:•4;;..r.. e EFTA00277946 - otycHT OP IRANSPOITATION Form Approved M EI • VIATTON ADMINISTRATION Rkiiign Bureau No. 04-RO60.1 • 0 MAJOR REPAIR AND ALTERATION FOR FAA USE ONLY sae • OFFICE IDENTIFICATION (Airframe, Powerplant, Propeller, or Appliance) INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or for instructions and disposition of this foam. subsequent revision thereof) MAKE 4 MODEL - I. AIRCRAFT Boeing 72'-31 SERIAL NO. NATIONALITY AND REGISTRATION MARK 20115 USA N505T NAME (As shown on registration certificate) ADDRESS (As shown on registration certificate) 2. OWNER .. 16951 JFK Blvd. _ Tenneco, Inc.. Houston. Texas•77205 _ 3. FO( FAA USE ONLY I 4. UNIT IDENTIFICATION 5. TYPE UNIT . MAKI MODEL ripAit ALTER- SERIAL NO. ATION • . AIRFRAME ensonennermenee (As des srand in item I ekes*nenneeneseinen X POWERPLANT . \ PROPELLER Tal APPLIANCE MANIOC-TURN -- 6. (ONFORMITY _STATEMENT A. AGENCY'S NAME AND ectousS IL KIND OF AGENCY C. CERTIFICATE NO. G. C. KOLS X u.s. OINTIPICATED MCKANIC Tenneco, Inc. IDISION CIITIPICATIO MECHANIC 16951 JFK Blvd. tionricmus REPAIR STATION - Houston, Texas 77205 '!itiodurAcruant 205-1 D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal and that the information furnished herein is true and correct to the best of my knowledge. Aviation Regulations DATE SIGNATURE OF AUTHOR ZED INDIVIDUAL , • 4-22-81 s- 7. fetfltOVAL FOR RETURN TO sinful ,---.--identified Pursuan to the authority given persons specified below the unit in item 4 wasNG;ted in the manner prelcribed by tne Administrator of the Federal Aviation Administra tion and II ILAPPROVED O REJE ID • ?AA IMPCTOT. FI STANDARDS OTIMI (Soma') mmilm'Acimms A _ IKIETC1/0114 AUTHORIZATION R BY CANADIAN DEPARTMENT PAA DESIONaTt WAIL STATION OP TRANSPORT *4$PECTOt OF AIRCRAFT DATE OF APPROVAL OR CERTIFICATE OR SIGNATURE Of AUTH RIZED INDIVIDUAL REJECTION DESIGNATION NO. A • 4-24-81 1337480 ' trib-/ ,, • • • 5 ife wat ql,,;‘cmuL • • ii.n.werh•ite).6se‘. • 4;t: • . • • ‘••••••:•--• -,.••• •-: ' EFTA00277947 NOTICE . 40 - Weight and balance or opering limitation changes shall be entered e the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION Of WORK ACCOMPLISHED (If more space is required, attach additional sheets. identify with air- craft nationality and registration mark and date work completed.) .supplempitail tights Grimes Smpplementary,Lighting System installed on wing tips.. Installation was in accordance with goo shop pratices per AC43.13-1A Chapter 5, Sec. 1, and Chater 6, Para. 48 and 249; Chapter 7, Sec. 1, Chapter 11, Sec. 1,2-3-4-5-7; Mfgs. Sp cifications; and Airesearch Aviation Co. Drawings I/1359002°A" (Mephanical) and 01783009 "NC" (Electrical). System was functionally checked.and operation was normal. Weight and Balance and Equipment List revised. ErIn-CiOVERIEMEW(PAINTING OFFICE: 1071-77b0211344 ti.k) • e . IP • •. - str—Iste.o•-- ali)t • , ;•-• .• • • .--••• . ' st. • .• ,• • EFTA00277948 DRAMMEN! SANUORMTION ' -; I Fast AVIATION ADM INISTRANON . . fond din stream No. 04-R060.1 . MAJOR REPAIR AND ALTERATIONS . • FOR FAA USE ONLY (Airframe, Powerplant, Propeller, or Appliance • ofFta IDENTIFICATION Ireg" 4- . INSTRUCTIONS: Print or type all entries. See FAR 4349, MR 49 Appendix katid AC43.9-1 (or Subsequent.revision thereof) for instructions and disposition of this. form: . • . .' • • MAKE ' MODEL . • . . I. AIRCRAFT 727.31 - ,• - SERIAL NO. . NATIONALITY AND REGISTRATION MARK • .............10115 . 11.3.11. /1105T • NAME (As shown on tapir:Varian cartincots) ADDRESS (As shown on registration oett4ficote) - 2. OWNER .. • TEMEC0, INC. UM S.P.A. 11vd. - aistapo Tans 27205 3. FOR FAA USE OILY •. . . - . 4 UNff IDENTIFICATION • S•TYPE UNIT MODEI . ULM P.O. AMR- • . mama *WOO • ... AIRFRAME 000nnanewanntren (As dastrisad in Mom tabovA)nortan•••••••••••• • POWERPLANT PROPELLER . '. f . •`- 4 ... : . . .... .... .-ta'.1...i . . : APPLIANCE mAssusAcos . .tA. ! • :. • ."-- • •• • • • — --.' . -• : . .. .. . .. • ." . i. 101191MITI'SWINT • • • A. AGENCY'S NAME AND* awn . ____LL ' - E"ND OF AGENCY ' ' ' C. CERTIFICATE NO. u.s. tastmcstro awssrnc R. S. 4022 A AIOESEARCH. AVIATION CO.; mints« pormauto msatmoc • A/C CLASS 2-3:4 4150 0oneld Douglas Or., a protcatem WAIN VATiON ' RADIO CLASS 1-24 • Lang kith. CA- WIN ki#Numainsa • LIMITED INSTRUMENT. . SPECIALITro Q.re:yrs D.. I certify that the repair and/or alteration made to the, unit(s) identified in item 4 above and described on the•teverie or attachments hereto have Woo made in accordshee with the requirenient3 of Pan 43 of the U.S. Federal Aviation Regulations . and thit'the information furnished herein IS true :and• Correcsto the best', of my knowledge.., ,, ., • • • L •• DATE • . . . . a, • SI R2 A l/ED I DUAL .. . . APR.0. .3. 1981 -. ;.: ... • ••. • ' .:: ., .. ..• .... ."• . . .i . ... . . • •- f - 7 APPROVAL RONAN TO 1 Minoan to the authority given persons specified below the unit identified in item4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and 'is - Ili bPpROVED .ORfilEtttO FM RT. STANDARDS •kisv timiusidun ODOM (Specify) :_ „ • . INSPECTOR a minds:xi Mmtextusnost BY . ' • -, . • .• • - cAMa01AN DEPARTMENT FAA DESIGNEE x REPAIR STATION - Of TRANSPORT INSPECTOR Of - • .. DATE OF APPROVAL OR CERTIFICATE OR SI0 RE . . AUTH REJECTION ApR 0.3 199. DESIGNATION NO. . 1 R5 4022A • EFTA00277949 NOTICE Weight and balance or operating limitation changes shalt be entered iir the ;Appropriate aircraft record. • An alteration must be compatible withfill preYlous alteratiolii to golutetantinued-conforMity..with the applicable akworthineli requirements. • • 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. - Identify with air- craft nationality,antl registration mark and date work completed:Y.: ,• • , • • •, Installation of ciaal Delco Carousel IVkilnertintNatigetiOdir!iin accord= . ma with STC SA4104WL Flight Manual SuOOTement issued' deted,June 27..1980. • Installation of dual HF Communisationslysten usiwe'vertioal.lin.loading edge slotted antenna in' accordance . Eastern . A1rlineo RIC MVOS°, Oka* fOr. the. following deviations: • •• AAC prawing. 1418108.7.HF .;.1.Ostme CeStrOl Head Med. MC Draidig161019r .2'Ostia PAM Head Nod. It has been deteriaineethat'ths iniarrelationiblOibitween theie changes and ant:! -- other previously pi:proved modificetions will noCadversely affect the air- -- , worthiness of/this aircraft.': !*:, . :. . ' e Aircra ha been weighed. Weight.and.Belenee and Equipmint Litt anvil:ell , - .• • • D •OHM' • SHEETS ARE ATTACHED . : 1" hAi. 011 _NIENT PRINTING 6PPi:Ei'lliiii:in.021/780 -': EFTA00277950 r . , DIPARTMEhilit TRANSPORTATION Fenn Approved . FEDERAL AVAWE ADMINISTiATIOt4 Blke! B.:tram No. 04-R060.1 . ,. • 7 -------• ' =.- 1 OR REPAIR ANDALTERATION FOR FAA UP: ONLY .' (Airframe, Po • - • OFFICE IDENTIFICATION nf, Propeller or Appliance) INSTRUCTIONS: Print of type all entries. •See PAR al 41-e t'500 4 43.9, PAR 43 Appendix B, and AC 43.9-4. (or subsequent for instructions and disppsltion of this. form. - revision thereof) "' Le log MODEL . •• , • ., •-• .::: I. AIRCRAFT 727-31 ...-. SERIhrti . • . Pitierify Afi qrTitATf N MARK NAME (As shown 'on registrotion.cortikotol 1. OWNER regi &ion certificate) ADDRESS (As•shoWn on TOMOS)• ilIC• 7 . . . .:.17779.5 John F. Blvd. . WHIST:Ott g T 1 14 3. FOR FAA USE ONLY , .• . •. ,. . . . . ,. .. • . 1re data identified:herein compliei with Appli . • :, airwoithiniss requirements and Is approve liforabou • • .. . , • • . i described aircraft subject to Conformit . • .. . : :.-.;,...• %, “.. y, 1 p.edionby a •• perio uthoriied in,FAft 43.7... • ' • • •• eca/d (icey, A4-efirieor,....att •: , . ,. .• ab% /elc' • 4. UNIT IDENTIFICATION - - • 'UNIT • , . 5. TYPE MAKE - - SERIAL NO.• - AUER- -. • : - IIEPAM ATION • • AIRFRAME . ..enewomengeoesee (As described !know n I ohowt)swaimenneemene :- POWERPLANT -...,*. ' ..; • ‘ 0.:0-1 PROPELLER . . - •••• • . ••: • . .. ins • . . .. : • .. . . .4 • ' . ,.. • , .. APPLIANCE MANUFACTURER * trielltr : I •A 4 (. . • •' NT CONFORMITY STATEMENT . . • • A. AGENCY'S NAME AND ADDRESS -,r• . - : - B.' KIND' OF AGENCY : C. CERT E NO. „yr AiResearcb Avtatlon Co. . • • u.s. Y.S. ltnitSATEDatECHANIC . • F. ' n. s. 4t.)24IFICAT A 4150 Donald Douglas Dr. . . A/C CLASS 2-3.4 ICIRElpi CERWICATED MECHANIC :. •:. ' Long beach, CA 90808 CERTIFICATED REPAIR STATION RADIO CLASS 1-2- • LIMITED INSTRUMENT• MANUFACTURER SPECIALIZCD SERVICE‘ ji U. I certify that the repair•and/or alteration -... attachments hereto have been made In'acc nit 'i to the unit(1 ).iden tifieci in item 4 above and described on the revers orders e or and that the information furnished herein is pe with the requirements :of Part 43 of the U.S. Fedeiil Aviation Regulations true and c EMI to the best of :m leukaalerlge. • .. . . • DATE SIG TU AubtraR ,,,,I ivioum,, . • APR 03 1981' ... :. tt • ' • 7 •.• I • 7 . pPR0VAL AR WORN TO SERVICE • : • Pursuan to the authority given persons specified below the Administrator of the Federal Aviation Administra the. ‘n:t Senticed in item 4 was inspected in the manner presc tion and is laAPPROVECT OREJECIL.3 , ribed by . FAA Fn. STANDARDS OTHER geerifit ' MANUFACTURER ' imPtcylori;AsamotaAnoi4: " . INSPECTOR . -.• • BY CANADIAN DEPARTMENT _ FAA DESIGNEE X REPAIR STATION OF TRANSPORT IKSPKTOR OF z• , AFT - t. . DATE OF APPROVAL OR CERTIFICATE OR SIG .?T E HO IN IVIDUAl.. REJECTION DesioN Rs AIRON NO. .- • APR 0 3 1981 402 a • , i - E• il . ..• FAA Form 337 11-67) EFTA00277951 Wegfp... ........................ Nil • IcL) NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible. with all previous cilterations.tO assgre cobtinued conformity with the applicable airworthiness requirements. ' 8. DESCRIPTION OF WORK ACCOMPLISHED (if more spare ii .required, attach additionarsheets. Identify with-air- craft'nationality and registration mark and date work completed.) — •• The fol owing 'systems were installed complete and .in accordance with manufacturer's- r• speC?fic ions; ACCS-32 all sections; AC4;3.13-2 Chapter- 2, 'para.• 21,22,23, Chapter 11, para. 1182, 183, e,f,g;--AC43-1A Chapter 16, sations 1,2,3;4,5; AiResearch Aviation Co. drawings Di. 1500553 avionics radio, DL 1600562 avionics elect and Hill Kennecky. DER FAA 8110-3 data Dual Collins 618M-3A coma system • • . Dual Collins 51RV-1 VHF navigation system. 7 Dual Collins FD-109Y flight director-system..J.1.i. Dual Collins DME-40 DFIE system', _..* Dual Collins TDR-90 transponder system': .'_. Dual Collins DF-206 AOF system_. .. . • . . Collins FPC-75 groUnd proximity warning systaa vo Collins 54141C comparator warning. system _ Collins 51Z-4 marker beacon system ., • RCA Primus-400,14XD coloradar system , a • Wulfsberg fligpkfone III air. to ground radiotelephone • • Flight Instruments: 2 IOC 521-28007005 servoed encoding altistetets 2 IDC 422-30510-130 static_defect corrector_and SAT/:TAS computers.. , • .4 2 IDC 575-25820-739 mach/airspeed indicators. . • 2 IDC 513-24660-101 TAS/SAT/TAT indicators_ ._ _. .• 1 IDC 540-25100-001 altitude alerter. • 3 Davtron 8118 digital clock/flight .time recorder 2 Collins 329B-8Y approach horizon indicators., 2 Collins 331A-96 course 'Indicators .Rosemount 102AH-2A6 dual timperature probe, Cabin audio entertainment system, .. , . The following systems interface and wiring_alsti initalled in accordance with AC 43.13-1A chapter 11 all sections 1607032 shaver outlits, mod . 1608092 utility outlets,.ftld cabin . 1608093 utility outlets aft cabin' 1608099: service outlets, mod 161013' ac power distribution, 161013: ac power galley,service;' , . •. „ 1611031 Freq.conv. static 115 vac, 60.-HZ 1636212 dc power distribution 1668006 engine oiler remote. pimp . 1683354: sch-electric oven, mod (Jena-Or) 1683355 electric oven, mod (Jenn-air). 1683371' galley, IVid unit, . 1683372 galley, aft unit.. *19764".0.-1703-1.1/673-1104,175 • • EFTA00277952 ; The following systiMsinterface andwiriagalSo inst ,,..chapter 11 all .sections: alled in accord#oce.with.AC.43:.134. • 1584011 sch-pniO, zone air cond, - ..„. . 1684012 sch-ckt, air cOnd.:,(zone temp,:cont4. 1684013 ...:sch-ckt..air. COnd, - ,(00rhe0Jlont.) .. 1685073' air'Cond.zohe tem0_Ontrol: . .1687047. air'cond. sensot.fons..:::' - ' 1692234::' . water blister, galleY.C184: -..,1692240'-- :.:. --- water heater, maStee.lav::20 gal:. 1092241. ' water system line_heater0+NC. 1692242 '. water system line.heaters4- aft ::.. . , „. 1692316 water heaters; laVatories; mod.: 1700040 - '..' vent blower galley..... . ; 1755039:- -: air cond. zone temp'....indicatign.... .,_ 1782110 :• a-We-lights, tabin....,. ...-.. - ,,.. • • • lights 1784137 ' storage compt and closet light 1789059 - . ceiling its essential power s..., • - ;., 1792150 - cove '„lights, creVi„compt, ' ,..,..„ 1792151 cove lights, galley...:.., ...._ • .,..-:. 1792152 .. cove lights(' lounge, 7- ... 1792153- cove lights, fWC*.sttite.room ...... 1792154' ceiling & read Its.:,trew compt.. 1793268 Ceiling tts galley,,. ,.... :—.... .... 1793269 ceiling & read Its;.lounge----..:7,. 1793270 Ceiling & read...lts,.flitd stateroom 1793271 ceiling & read...)ts...oft stateroom 1793272 ceiling Its, aft)lavatOrY ' - ,.....: 1807045 table lamps cabin:..,. .„ 1808212 . thoWer fan/ It &J.drain_valVe. ..;... .., . 1813061 panel ltg. 3rd crewman's . ..„.:., 1813062 switch & panel ltgi.cabin 1821059 ceiling its, fkl.vettibtile . . ,.... i:,..- 4-...0i,,....... 1821060 ceiling its', aft ;vestibule r,,,I.-...:.. ,...- . 1824242 work & effect its, lounge bar, :. - 1824243 vanity lights. aft:vestibule,.:, . . 1824244 work Its, fwd and.aft.attehdag 1832400 . attendant's panef. fwd,vest....t's. 1832401 . attendant's pane1.901 . 1832402 0 attendant's panel aft vest • 1832103 vanity disconnects, laVotorieg s". 1832,j.04 circuit breaker panel. 0114n% 1832405 circuit breaker.panel,,mid cakin. . 1832406 „1. control panels,-„cabin.: . , .2-- . 1832407 electrical equipment.:instl. g4110: 1832408 electrical equip. inStl, mid lapi . -. 1837026 n::. .: . spare wires. electrical.: 1838211 electrical flusk.toiletS. 140(1,....- ,,,: . ....... 1838212 '.drain valves water,syttem .,..... .., 1838213 air compr.• & qty.i0d.,water system:: 1880028 air cond. overheat' control 1883071 emergency exit ltg,.mod 1886193 call system relAy.assy,„: 1886194 call system cabin .:..'.-:... 1886195 call system crew..H.... . • . „ . . . ••• 221141V ..;!..fa*•••!,.,,j, „atg_kt., „i;•;212.%:;, ., t-uz.k.z.:,:eir,„;.;;;;,. • ••:. • EFTA00277953 EFTA00277954 „ grz. . : 147:417:5N"C• ” Wilk • •••• • • • • • • "*.. - • • ., • •• 1. •• •• . • The following systems.interti a and tiring also installed.in()cordance chapter 11 all sections:, . 1887205 '' passenger warning signs.. ,,..„,... 1888050• smoke and flame.det...sentor aqt,i.1. - .1888053 smoke and flame.det. bag CoMpt. l.': . . .__. 1%1388. rad'o power feeds 150222, , radio.lights _. ,-...,:". 1503178 ' ADF-i system OFT.206.,4:L. 1504137 • . ADF-2 syttem OF206..„::_. 1505284 NAV-1 system 5181(71,t_ ' 1506266 mV-2 system 51111144„. 1507304 FD4 system FD-109Y 1508276 FD-2 system FD-109r..-:.. 1509281 DME-1 system DME740-,,,;. 1510184 DME-2 system DME1-40,.., ,,-. 1511058 DME indicator 1-.... .:. ' .1513193 marker setem 012!74.,:..:.:, 1514066 Selcal symtem 45SC.! modif "__ .1515205 VHF-1 system .610-38516207. ._,- ,. 10.6207 VHF-2 system 618t1-3A ..., .,.,.. 1520127 flltefone sySiem , : ,,..4; -.., 1521225 atc system tdr-90 (dual) v.-;.".. 1523254 pa/inph (modif), •••• 7 1524057 stereo system (cabin). :_. 1525090 tv;antenna (prbv). _ 1527211 cockpit audio (modif)., . 1529137 comparator system 54W-1C : „..:_ ..... 1530149 weather radar primUST400. • . ... ;._ ., 1533204 no. 1 radar•nitimeter ale-51A, modif 1531205 no. 2 radar altimeter ela-S1A.(modif) . 1535205 autopilot. systen.interface 1536231 comp-1 system interface. • 1537221 comp-2 system interface, 1538174- altitude system_interface. 1541186 ins-1 system CIVA. . ..: _ 1541188 ins-i system interface,. 1543187 ins-2 system CIVA. . ..,.., 1541189 ins-g-syttem interface. , 1544264 1.h. altimeter/alerter ... 1544265 .r.h. altimeter indicator 1544266 stby altimeter indicator 1545117 Mach/airspeed indicators 1547116 1.h. sat/tas system,. ..., 1547117. e.h. sat/tas system..,.L 1548034 scat system (modif) 1549249 annon system _ . .. 1550178 .reco accessory box .. ......: 1551077 digital clock system .j., 1'552007 oat indicator (modif).:.:',,. . ,„-._ 1557091 data select system ,. .., •.%. 1558010 rate of turn system (modif) ,;,. 1560020 GINS system (modif) . , ,,_ . . .1571017 ins relay unit _ .._._ ',, 1570028 nav relay unit ,. . v.,;,..; . 1592046 annunciator cp1r.diagram ..,., :,. 1594097 cockpit hf/inph_control. . ... 1594098 cabin flitefone/inphooatrol .-.%_. . . EFTA00277955 EFTA00277956 .. • • . rev. m-t‘ 0747.7 . . • •. . . 7.7 7WWTT•ii Vti 7:56175771-Prror P.:c7,eirart C's,s24, 1rtatT / 3 4"-• .'`‘'.1)••••• • . . 'POSIR01. 4sIt. 4USWitObOlVV- 0347411qpus 446tek epatlem 3424340i •.£'L5 • ti plot 3Y aspi43 vart - •Sdigt ' 6'I8. ti pvai'm cannin tiltUAOU itnoi •sdam act Si. APedt3- 00 iv=o1 129', ppa `SZO-Vtatreff 3t1 amigiu0339 u4 6ZL£-3 vuod so3 uoirti:mt tpasianny Jaalipso wag Ivy spiting plot 3v-30 tvoI.4oat° liv • ' COARTATENI; !TRANSPORTATION '. ; ' I r: Form Approved 1(..' Budge Moreau No. 04-R060.1 FEDER.4. AVIA ADMINISTRATION • • • ' • • FOR FAA USE ONLY - .'MAJOR . REPAIR. .AND. ALTERATION . ,- . i leFFICS,,ITTIFICATEI:ls„.....--• ! (Airframii, PowforploSt,,pfcpollfr, or Appliance) . - • . INSTRUCTIONS::Print or type all entries. 'Sei FAR 43.9. FAR 43 Appendix B. and AC 43.9-I (or subSequentsevision thereof) for instructions and •disposition-of this form. • .• • . ' ••• ' MAKE hImalf/e31 • ., 1. AIRCRAFT SERIAL NO: NATIONALITY AND REGISTRATION MARK • . .'' 20165 . . - NA I605! NAME (As shown•.on registration certificate) L, ADDRESS (As shown on regidration certificate) Z. OWNER . ? -• 7 . .. ..teensa .‘ 'sate - •• • 11796 ASA. 91vd. .. . • ' „A - • illestos. Tees 77205 • v FOR FAA USE WILY . . . • • .. • -_:.....: .: The data :We . ntitied herein . complies. with Applicable - airworthiness requirements and ,Is approved-only for above .. • • •• ' , _ . iascrib • aircraft subject to conformity inSpection.bya.• -• • • :7 - . . . .... ' Pe thoilze InTFAR 43q.' 7.- . . - ,.. . . _ .. ._ • • .• • • -:-, 4.-a0756471TSIT IDENTIFICATION -S. TYPE • , :,...„.:,,.;,.. . ... MODEL SMIAL NO. ' ALTER- UNIT - • ••• REPAIR - • • '. • .. ATION .. . . . ., . . . AIRFRAME • . nenninentieeiwiie (Aideals:it:di; iti.trik abiwOniiintion . . , . .. . I ... .. ••. ... .7 ., POWERPLANT ; 2:17:::: .: . . • • • . ,_ .. . . .. ... . ... . PROPELLER ‘...7•:•-; ' e.1 1-1 • •g •r ' -• ' ' • • i .. • . . .. . , . . . .• APPLIANCE .•t' MANUFACTURER . , • ' • . • • -. . •. - . . . .. .. . . , • ,. . . '' • • 6. CONFORMITY STATE ENT A. AGENCY'S NAME AND ADDRESS • -• • • S. FIND OF AGENCY • C. CERTIFICATE NO. R. a 4022 A :.AiRosaarat Aviation 0. : ••:, • ; , L-..; .1. '': lk-SZIgetICATID MECHANIC A/C CLASS 2-3-4 :MO Oonalot Onolos W.- - , - - . , •.; _;i:,,,;_., ., !QUIN' ORITIFICATED MECHANIC • RADIO CLASS X-2-3 Long 9sack..CA 90000; • .. - . .... .; „. • ,..-, 44IIIITIFICATEDtEPAIR STATION LIMITED INSTRUMENT .' , .7' •• • ' , •—• • • • ' • tent4U1ACTUItIlt• SPECIALIZED • SF ITT VI Cr . .. . ., . •. • . ._ .. ...- . . • . .- • D. 'I certify, that the repair and/or alt ion made to the anit(s) identified ici•iiem 4 above and described on the reverse or •. attachments hereto hive been midi iti accordance .w1tb.therrequirements of Part 43 of the U.S. Federal Aviation Regulations ' and that the information furnished•herein is true and comet to the best of y knowledge. .__......-- • • .. • • S D INDIVIDUAL• .n.... DATE . A R.:0.3 1981 - :!... •• _ - • . .. ; :t. - . , . 7. -AfflOYAL FO lETURIF TO SERVICE Pursuan to the authority giveepessons specified below.ithe unit gentified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administrition Ind is • -APPROVED 0 REJECTED : - • , . • • . ,• ,• R.. •... OTHER (Specify) • FAA RT: STANDARDS • MANUFACTURER — • - INSPECTION AUTHORIZATION - — . ...... . • . - -- - __'..- . . ...— INSPECTOR BY - , , • CANADIAN DEPARTMENT . . . FAA DESIGNEE I REPAIR STATION OF TRANSPORT INSPECTOR • _ OF • .. - DATE OF APPROVAL OR CERTIFICATE OR. SIG REJECTION . ...- gthigION NO '• • . APR 0 3 1981' sagar IFitil i • :. .It . .,-. ... I.: I . . . ..• . . ,.t • :; •` •e ' .-;esedi•-•;&*-4111‘..w.i.:;:,;:---en.• ..-- .. ...., . .,.. ..fleSatalialharairiEt • S"‘thrivoi'v 4,14L, ' ?ILL'S"'r•• -- •.. '•'../it1irilci'v -`'-'-'' .11,:t- # -' '.7..- •":2-7 ••4" 2L 1 .: .elarair:az :-.:"S• - i "4" -rA. '. . 1"‘JI .iPix....—•-z...!t. / °'' J :4_::..!..C......s....1. 4.-sec.:( ' '-`...:t1/2? et -2--''' LAI 1.5.7.V.` 1 • —e: -..:. --... .. EFTA00277957 NOTICE . ". Weight and balance• or, operating limitation changes shall be entered in the.appropriate aircraft record. An alteratiOn must be:compatible with oll'previOtis'alteiations to assure continued conformity with the applicable airworthiness requirements: 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space .la required, attach additional sheets. Identify with air- • craft nationality and registration mark and date work completed.) 1. Inslpilled .the fellowtagAw:acortiance with ACCS-36 ill _sections. M43.13-2 chapter 1 Para. 1:454-.7-8-9-104142 AiResetrch Aviation Co. drawings, 11.13011611 401,1_ 1 analysis contained in Howard Pattervon.. gei 1102034 Installation table• Cocktell, !atria f/O2Of4 110244- table, -cocktail _ 1102046 °' table, cocktail wt: folding leaf •- 1104065 table, foldout • galley 1124232 " divan. r.h. 3_ place....„; ". 1124235 6-divan, 1.h. 2 place berthable 1124236 divan, curved, 4 place,_ 1124237 • " divan, transverse:.3.plece_ ___ 1124238 " divan, Motels. 3.place_lvd, facing 1124239 " divan, riviera, 3,21ace •ft.facing - 1124241 " kibitzer seat 1130090 6. closet/ desk. 1130093 clospt 1.h. 1130094 closilt, linen 1130096 6 clu coatroceicart 6 1130097 ° closet linen, 1139111 ." ledge 1142171 ° cabinet, refresiseigt.,_ 1144127 6 table, with folding.leaves 1146114 ° pull-out- table 1147184 ° cabinet overhead 1147185 " cabinet overhead 1160200- " fabrication bulkhaid.and.iloors 1160201 'Fabricates turn. panels. _ 1160228. FabrjgatleVniltkondAPOd.iiiiidi - 1160233 Installati ills nift•mitioeid_ _ 161-STD-052 Iestallation std.-blowout door eeilkultheat prey. 4164038 InstagiF on fittIng,..tnathead ti0418100. 1164046 ° bel and partition_uPPor 1164050 ° parti ons• eind.efet • • 1164052 ° pass partition and, attoch. 1165470 ° galley, r.h. frd,fee lacing, 1165478 ° galley, r.h. fid aft_f4;inie_ 2176173\° cabinet. vanity wi..gggt... ....__.. _ 1176174 I cabinet, aft lay... 1214196 " shower - - ' • 'I 1214200 "" aux. water tank 1214271 " hot water tank 1214329 " aux. water tank, aft.. 1220153 ° pallet, single Mt.. 1220155 ° pallet, single seat„ 1220158 ",pallet, 4th crew eieber_ . 1220159 6 floor support ends pallet .!tDDMOtiefil SHEETS Ald ATTACHED . . . • EFTA00277958 • 2./' **stall« the fuliculagi ta$44, eltsactläni and Ailkisaarch Mislike Co.• : . i 1245409 • Ploorplan • Intall4101, 11 11:1 9$ a. ALIS« sats :In ralstlao- -N to aergancy snitt 3‘_ oZ_stalled the follaul_8$ 4.1'082 all action.. 4b.353 Slø 202, 203.'204. VIL 206 (b) si 12g;17 44994å-tiOPSitplist-,f.likift. Instsliiitiiie"1;11‘1-ag 1b accortissicamith ACC5-32 all .sectias sACC5-33 all action. AC.43.13,1A depter 15.sect,..14-3-4-5 dustar 16. sen. 1-2-3-4-5. AC 43.1.1,2~ir 2. para. 21-22-23 tastar 3. pa 31-33-34-35-36-37-38 ad AiRasarch »Idiom Ca. dralon", . • • _ . 1410337 Layout- rodio rack EL 1410338 Layout - radio rad 14.,25. 1425272 kutal1dim fli telen motane ... 1461190 lostallatiou wasther.nar.rit sid.aat. 5. Installa da sofrotrustural,Itatin.acconlact with etui Installation- air.ictuator.sotasi • flat calling • -. i 181405 Layout instnnont .*11233259 Layout control 'hal :4191198- Nodification pitotistatic, 1401205 layout- radio controls. . 1411225 Installations. snor total _to"- 3I4+18COg layout overhead panel 1449004 Lanat flt effir. Itation . . . -•*wre;e . '-• •et.....,.:.•-_:*-- . .... • -•-•- :•••••-x-, - • • . • . --t • . • . . • . • ...: , ••%. • ............... • . • •• • a • . . ..t.:1. eMiLLISId 'it ilti :SaL‘• :.4,.2..'.?.::-i r..1 g. t." . ? ". .1a.• . L ..... . 4.:1,... - SiSilik Datia•SikAiC :;“2S :" . aNtS"... t.:•••• ".... i& ..;.k4,...&-I.S.:: ....:. ...:......:..: • EFTA00277959 EFTA00277960 －直雌崢蠻瘫，廬．蠱濞~剋薯I 凋」lil ］ 凋 ］ } , t .？翠譬对割胃剖叫到恫4 训翮阁耕，捌劃踊啁制1嘉 渊 ＄ r 滅瑚蟈萋劍斟目凋辆爿淄封1 ……一．＇鯊亏＾“餐 凸 妒 y翻 h 辐 扎 1\,＄毬t , i曳． 』 r. ； . 密 箋槛 跋氓 P 舌广‰． MP' • ,. DATE , ' APR 0 3 1981 ' •O11PARTMILNT Olt TRANSPORTATION FEDERAL AVIATION ADMINISTRATION • STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIF CATION'- • MAKE .. ' .I MODEL NO. . TYPE istiriNany. Rados Nolthoptyr, NAME OF APPLICANT ..727-31 AIRPLANE AIRESEARCH AVIATION CO. I • BOEING - . „ 1:1$T1 OF DATA TITLE ' • IDENTIFICATION I • . . C-3825 ' STRUCTURAL SUBSTANTIATION -Interior Installation -for . TENNECO, INC. 727-31, S/N 20115.- • . ..- . . • ... . . . ... C-3688 Weight and.Balance for S/N 20115. ' • ••• . . • :.-- .- ... •. . -. DL-1300517NC . Data List.-Anterior FUrnishings: . , .DL-1400319NC Data List -4iicionicsitiech. • •• . • . ..• . g .. • • • ... . ...... ,.. .. -. ..• . . . .• . ., . , •• • . . . .:. • . - ti ... . •-•r, • • . , - . .. , • ., • • -• •• .. - • . . PURPOSE OF DATA Substantiate BOEING 727-31:InteriOr Modific ation. on N505T Serial No. 20115 ONLY. . Final Aporoval.of the ModificationW111 be made bilAA. • APPLICAOLIE. NEOUIKEMENTS (Mot immeMS• nallono) ..- • - • . . CAR 40.202, 4b.301, 4b.306 4b,260, 4b.358 and 4b..101 ' • --. with conditions and limitations CERTIFICATION • Utder attlaity vested by,dinetioe of the Administrator and is oscosiosso and attached Amos numbered •of appointment ender Part 183 of the Federal Aviation Repletion. data HAMA abiove a d medium and found to comply with applicable • have beet imuohisd is accordance with establishe .. .. .. • . • • .- lectuiremeats of the Federal Aviation aestiathas. • • • • Ai/There fore • DI Recommend apPrivsl of thesiidis. : - '. • I • 01 Approve these data • CLASSIFICATION(S) SIGNATURE(S) OF DESi NAT p EN0A ! EERDIO RElItESENTAIIVISO all1SIONATION IIMIIIERSIO ..:_i. 4. WE-663 • STRUCTURES Pa ,d.A....--. s - ' I .-- , - -------- EDITION FAk Fore 8110.3 t trio) sissaftscoat *ominous • • r•n;Aiki_g41..€71:tafit t-•-: • n °. hrj r Ssieditgas",: • ?....:26t (?;.249 e- • EFTA00277961 3- . • %ra.,;•,--, --•• • • =a= ‘41:itlaL.IctiCt ;"1 ;,!• EFTA00277962 FEDERAL AVIATION AGENCY DISTINCTIONS' Print to type. Do not Willie in shaded oracle/ liwo ors in FAA um tidy., Submit original only to on su- tutPoLiCatitliFOR AIRWORTHINESS CERTIFICATE thatind FAA Repro/Malin. II addltionol space b required, IFAR 211 ' ' : MN rano tide. I. TION MARK 2. AIRCRAFT MAKE . AMOLA/7 MODE USIGNATON ti, <: 93 0.3 Boeing 727-31 _ 4. AIRCRAFT SERIAL NO. 5. ENGINE MAX! 6. ENG0t MCGEE DESIGNATION I . . 1. v. 4' 20115 ' .Pratt & Whitney Jilt - 7 i .., AC o 7. NO. Of ENGINES R. PROPELLER MAKE 9. PlOPELLER MOOR DESIGNATION I0. YR. ARC. FACTUIEED -t Three NiA . IVA 9 A. APPLICATION IS HEREBY MADE FOlti 4 X ORIGINAL CERTIFICATE -AIRCRAFT ES USED IMPORT 4 AMENDMENT OR MODIFICATON OF CURRENT CERTIFICATE ' : . f OTHER (Specify) B. AIRWORTHINESS CLASSIFICATION (For mtmitifris ansfaaa., deal affmcriate ids° 2 I, X t STANDARD (Indicate canary) NORMAL UNITY i z ACROBATIC X TRANSPORT 2 LJAUTED . :14 ACIRCULTURE • PEST CONTROL AERIAL SURVEYING ft *SAL ADVERTISING RESTRICTED a."' • . 4,(ladicate (fereitios(1) FOREST (Wild Itfe cossersatin) PATROLLING i> WEATHER CONTROL * to be econfiected) % OTHER (Specify) EXPERIMENTAL RESEARCH AHD QEVEtOIMBaf Ai, (Inciirate opn etia(r) AMATEUR BURT i.; EXHIBITION r. to be cceedocted) RACING . TO 940W COMPLIANCE WITH FAR tis.'sits NOV/SIGNAL (Indicate dais) mos I CLASS II elte. A. REGISTERED OWNER (As than as Cat:fiats of Aircraft ResirMaraa) If DEALER CHECK HIKE .1r- X FLAME ACCESS Maim Oren, (My, State sad ZIP code) . _ The Boeing Company P. 0. Box 3707 Seattle. Washington 98124 g B. AIRCRAFT CERTIFICATION BASIS F AIRCRAFT SPECIFICAlON OR TYPE CERTVKATION DATA SHEET (Girt NA. AIRWORTEIRESS DIECTISI SUMMARY (Gin- year sad 411 card No.) g sad Rev. No.) tl - ASeiB. Raves 6 1 ;968 69-12 AIRCRAFT LATINO (Gin page WO) SLPREMENTAL ME 'CERTIFICATE (Giro No(i.)) • b. C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS O ,... X AIRCRAFT NEW —NO rtnictil .-LLSTORIcrN TOTAL MINFRAME 14O1)15 RECORDED RECORDS MAINTAINED IN COMPLIANCE WITH FAR 91.173 ?:25 I hereby certify that I am the registered owner (or his afar° deist aircraft described above; that the aircraft is registered with the Federal Aviation Agency In accordance with section 501 of the Federal Mink.° Act of 1958, and appii the aircraft has been Inn Aviation Regulations; and that and is airWorthy and eligible foe the cladailication s DATE OP APPLICATION NAME no nut (Priest or an.) SICK* JUN 6 1969 R.C.Ctuti 88 aillerthiII ell. . 1N ACCORDANCE WITH FAR 21.183, THE AIRCRAFT DESCIPMED MOVE HAS KEN INSPECTED ['FOUND AIRWORTHY BY: • X' t-- i CERTFICATED AM CARRIER F CESITIRCAND MEOULNIC DA) CERTIFICATED DOMESTIC IIPAIS STATION z ,a.t (Gin C.ertificate NA) ₹ (GIN Crstifcam Na) (Cisco Cute No.) - gr iC AIRCRAFT MAYARACIURER (Give mese of firs) alit OPUS Li 4' ..- A; DAM ,. .. SIGNATUE • .4,••- :,. ' .. MOILVLNICOG A. CURRENT OPERATING LIMITATIONS AVARAIILE IN AIRCRAFT X CI. THIS. NSPECTION RECORDED IN AIRCRAFT.EO0RDS . I. CURRENT OPERATING LIWTADONS ATTACHED 14. STATEMENT OF CONFORAUTT, FAA FORM 317 (Attach itb.en Trquirrti) X C. CURRENT APPROVED FUGER MANUAL AVAZAILE IN AIRCRAFT I. nrnous APPWOPTHIMPSS CERTIFICATE ISSUED IN ACCORDANCE WITH D. DATA, DRAWINGS, PHOTOGRAPHS, ETC, (Attach cobra required) SEINIMINICVAIIIV 'A )4,4 CAR (Orrg at:abed) X E. CURRENT WEIGHT I RAIANCE INFORMATION AVAILABLE R4 AIRCRAFT F. AIRWORTHIPR,IS CERTIFICATE ISSUED IN ACCORDANCE WITH , E. MAJOR REPAIR AFC ALTERATION:FAA FORM 337 (Ansel ears req.) X FAA ) 21.183(a) (Copy attached) X A. 1 have inspected the aircraft described above, find it conforms to ks type crailscitt. and b in condition for tale operation. -4 g B. I have inspected die aircraft descrthed- above, find it Is In condition for NSA experinatual operation. . 4 to C. Current Airword3inns Certificate amended. 11 OAR 6 / 4 01. t / 7 June 30, 1969 - b9 DESIGNATION FIO DMIR (42129 z) OFFICE NO. t3ICA ASDO F . 17teira7 .491// ) 41-2 9 3 24-0-46 ' W.A. O'Neal ••• nom.ataeztgRZamt,...., • • e r.,&:$c-e$ 211.fis EFTA00277963 EFTA00277964 ernm...••• ••••,•+ • 7 .. 7 -•-••-•^ -•-ws.• . . • • • .•• -.Wr.'n7.77c.AW7•c*Th'..g.. ..n.771.1.71: • c9,-••••• • .• . . . t!-- • 11 • • 7:••24•••t.,10. 1-Mtap ifi ttrfiegiraa,f1-:*-`1Wir .o.f•k• • St • .v • • • • . • ,.... • Z• p : • i - .,i-Osf.R .• . •, . • • '• .. : t.i.•f K i .1 • :as.", 111;410 ; r' N.:I ......".., \ it.F.0 ItiT It .. COINg.1A8CE I: REGISTRY ZiN t,•`• .. C.:•t•e :I' •,..:,..'.1:;.1:.'::, _ . - AIRCRAFT -.__-- - - _-_..... . . FAA ... _ . . .1 c .5 / 1 4. Er T ii,t in,h't•'•• •- .1.4`' -•F--:1•''''.- • • _ • , ..2.- tn..' 'LT .P.:2"L'.... P... fit .."ǹ—I.5.• ,:;...-,...' • 4 1• l• .,,r.. . ....“. t:.3.•,,. - --fly,. ,1...3...............m.y••••••••m....... :. - - .. - • •• . •r ., 1 2 ..„...... ._...,,,, •• I.- • A. r. . ., • .. r •...••• m• b.*•• • -. _ • - ..„. ••• ." i.li .4. , ••...1...•.: L rou tit S r ••• 2.0 EW. , .7::, :•7"1.11014,:re 'Il.1 2 -, .., '.." _ , • - OKLA • OKLAHOMA CITY, 3 r. • -.1•12;Zi-7,:r t,; • •cf • v. cr.; I ..• :c. i • Oh oap I WIT ' 1,1 - j ▪ ..;" ••• r. It :11'...r ..,. i . cot . . : .. . ::-.7 ...: . i rt L.; ... 1..: ., ••::::-..:•(::. wlvt.:...-..:::.:::,.;: .,-.....-...7-s. ‘',.... .., i c 4.'1 M. • •' -; ..... I j..', i t's Iii•- •': fi rl 7 El: •!'' . 1 .7.2....,..k‘.7:i0 4: r..- .11/...f., ; ; 41.. - ”- • ••••fietiV, .\ • . 1.%t" Cr;;...? 4 .4:••. ti.q... 1" -.. i..• . ...:- -_ .. -91w.C.--,--1.. ..,• .' --.1;:c.•: •- ''' •1-:' ',E kW P-G9 1 " - 1 .. s _ . .. . ) e4. -' ;,., 1 •:. .,.„:•!, ..,„ .„....,:,-, —z • • -kt • i . • if; tti I. • C' - Lf 1- 11. ' . IS. C * C.:fir-Cry. V;trio Tuses warrartst •,) - . west vf.teltrc.72.103;L:- • . ......' --. . : . : '. .. : 1 .. •-• ' . 4. .-.JSCI V•G :...‘ZciVic.r•Z 1.4 4,1 F."...Z . • - 1 , - ; - . . -• • •••-." 4 !" %."1 "'el • V•tij:30111,911.%/kt. tij P:C.:9.. , - . . ; • - . '. f ;-... 1 • , •fl Z ./C a. tiliat i lr4IIII ASPrH itilus ;:i . 1." ..L". ‘a ;M : C:11 7 P;." .:- ' “.) •:. . . ? 9.11•3, A CCZilil. G+[[ : ...::: I ! I:" • • 7 "._ --' 00 4. • .,. . • L t 0 103.4.13 el in ea . 4 • • f J • • ' - ...."- C . . .- . ..... 1 ...t ! Ir VfliCt :O. O::::., 1:',...... 4. •'1, •• • ..: • : ' ' • ... • : '. • I t'. '. :' : :- 4 i.••%:, .: .. . . . . • . . .. . , . . . - I: •i: I 1.; , i .5; : I vi,.."..-1,L(i..p.:::7;,1,o,;•• ‘...:".•- ::-N, • • •:iv• •••;.:1 ,.. .: i•...7••;S r.;••::1; , •".;.1 • •4; In)....,'.;/ :: :: .;.• " ' . 4; .7 "..; .7.: , . •.• :v.1 , .• •- •.::!' I I .•I 1 .1'.`.. Zr.) ', . 3: r- I ' •it.:C1et.: ..•-•:•.III:"."••:- • " ' ' " : - ' • • " - :,.,, , , .... . `22.2:::;:-..',... ,t ;pit::: ...-:::....:•1 ki:f.: :.- :-.• 1. -. -4; ,-.... ,.. -------- -.----7-7. - -- .. ... -. • ...;,,.. :tv J vilic.".-,44. ay.•::.t;;; ,.., 7 • , ,,••.:,77. --- ---- • 11 • • . •• • C'Cri E.. .• c••••`"i Cc:4. • 1%; • .i, •" -Pz: -Nis:rt;8 • •• C! BD:: • • • 0. . • . . • IV: t.:Zar.`..:72:1-.0. O V: l'• • • V ••••• • • . . . i ..;. 41.r •2:•:J•a•C• ..*:•• •, J • ".: . • 17.. • a i .• ••b; I . r• ".•16. •.V.•••.) ‘• 04 . • - ' - :e I •C r. Yr • ^.- .• ..• •, , • • • ; . • ; TV" • • t :I:~;~:::E • •. • 1 - 21- 4 4I• •• • I , lei:lit:5.4dg' 3,••.\\,' •, • . ,• 1.•;1•4•; I •2 ' • "•-•e'• t Cr • .• . . . • C •IC 1 t t. dl t, • • ‘t. • '• 4 UNITED STA ERICA • DEPARTMENT OF TRANSPORTATIO Al.. AVIATION ADMINISTRATION -.STAN RD AlftWOR ,1 I. NATIONALITY AND FACTURER A REGISTRATION MARKS sL 0. A V1 • 4."5 $7893 Bo 727a t 41 5. AUTHORITY AND BASIS FOR ISSU This airworthiness certifiazte date of issuance, the relict° , therefor, to be in condition comprehensive and detailed Aviation, except as noted Exceptions: None 6. TERMS AND CONDITIONS l it I Unless sooner surrendered, su , revalued, a this airworthiness certificate Is as long performed in accordance with P aircraft is registered in the U DATE OF ISSUANCE F 's DESIGNATION NUMBER June 30,1969 are OMR 4129 Any alteration, reproduction, or misuse of this tort =tellable by o fine not exceeding $1,000, or len- s prisonment not exceeding 3 years, or both. THIS CERTIFICATE MUST BE DISPLAYED IN. THE AIRCRAFT IN ACCORD- ANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. . I, FAA Form 810D-2 (7-67) FORMERLY FAA FORM 1362 )• COO: I417-0-270 631 • t. • .. EFTA00277965 EFTA00277966