EFTA01114993

Gulfstreant OVNAM.CO COMPANY PRELIMINARY INVOICE ParUModel #: GIV AC Serial No./Tail No.: 1085 / N423TT Bldg C.-FAX Mail Remittance To: Overnight Remiaance To: Wire Remittance To: Gulfstream Aerospace Corporation Gulfstream Aerospace Corporation (Box # 730349) Gulfstream Aerospace Corporation do JP Morgan Chase Bank. NA JP Morgan Chase Bank. NA ATTN: Dallas National Wholesale Lockbox TX1-0029 Fedwire Routing No. (ABA) S.W.I.F.T. ACH Credit Routing No. ( Invoice Number. Bill To: JEGE, INC. Invoice Date: Customer ID: BJ388 P.O. Number. Repair Station: FAA CRS PB8R624N United States In Date: 04/01/2013 Out Date: 04/22/2013 Payment Type: Net 30-Open terms Payment Terms: Title: JEGE, INC. INVOICE SUMMARY FOR WORK ORDER NUMBER: SC13175 Time & Materials Flat Raw Total Labor USD: $23,939.84 $74,150.00 $98,089.84 Parts USD: $196,307.51 $0.00 $196,307.51 Services USD: $1,547.68 $0.00 $1,547.68 Detail Subtotal USD: $221,795.03 $74,150.00 $295,945.03 Subtotal USD: $295.945.03 Funds on Deposit USD: 50.00 Total USD: $295,945.03 Pre Test Flight Times /Cycles Airframe 8563.8 Hrs 3963 Lds Eng #1 8508.1 TSN 3929 CSN Eng #2 8528.0 TSN 3935 CSN Post Test Flight Times / Cycles Airframe 8567.0 Hrs 3964 Lds Eng #1 8511.3 TSN 3930 CSN Eng #2 8531.2 TSN 3936 CSN For detail description of the work complied with see the Work Order Detail report. Unless otherwi indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 1 of 57 Printed: 4/18/2013 II:38:5 Ftst X EFTA01114993 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Item: 1 Airframe Gulfstream GIV Scheduled N423TT Team Manager: Sean Brown Pan/Model GIV Customer Coordinator: Ray Kraber AC Serial No./Tail No.: 1085 / N423TT TSN/TSO: CSN/CSO: 3,964 Aircraft Time: 8,567.0 Discrepancy: 1.1 Return to Service EJM (10 or More) Resolution: ACTT: 8,563.8 LNDS: 3,963 DATE: April XX, 2013 Completed (INSERT TITTLE) inspection accordance with EJM (INSERT AIRCRAFT TYPE) Continuous Airworthiness Maintenance Program, EJNI Maintenance Procedure Manual and 14 CFR 135.411 (a)(2) and is approved for return to service. Authorized RTS Signature Thomas J. Choynowski, Sr. Airworthiness Inspector For; Gulfstream West Palm Beach, FL 33406 FAA CRS PB8R624N Discrepancy: 1.2 Inbound/Outbound Inspection Resolution: Complied with Inbound / Outbound Inspections. Labor USD: No Charge N/ C Step: 1.2.1 Completed Inbound/Preliminary Inspection Step: 1.2.2 Waiting Outbound Inspection approval (L) Discrepancy: 1.3 Preflight Inspection Resolution: N/A Discrepancy: 1.4 Comply with Debrief Checklist For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 2 of 57 Printed: 4/18/2013 11:38:51.41 Rd X EFTA01114994 Bill To: JEGE,INC. WO8: SC13175 Invoice Number: Resolution: N/A Step: 1.4.1 Completed Arrival/Debrief 90 Day Due List Review Accomplished. Step: 1.4.2 Completed List Operator's Airworthiness Requirements & Special Documentation Requests. Step: 1.4.3 Completed Review Technical Operations Update prior to return to service for newly released bulletins and advise operator. Discrepancy: 1.5 Tool Clearance Resolution: All tooling removed from aircraft. Discrepancy: 1.6 Cover & Protect Resolution: Protected aircraft as required for MX as required. Labor USD: No Charge N/ C Discrepancy: 1.7 Service Chemical Toilet/('lean Galley Resolution: N/A Discrepancy: 1.8 ArrivaUDeparture Assist & Video Aircraft Resolution: C/W as required. Discrepancy: 1.9 Sample Hydraulic Fluids Resolution: Sampled Hydraulic Fluids a required. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 3 of 57 Printed: 4/18/2013 11:38:51A) Ftst X EFTA01114995 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 1.10 Remove Valuables & Secure. Resolution: Discrepancy: 1.11 Comply with Service Team Manager Checklist Resolution: Labor USD: No Charge N/ C Discrepancy: 1.12 Fluids Used (Oils/Skydrol) - (Materials Only) Resolution: Billed Fluids Used (OiLs/Skydrol) - (Materials Only) as required. Discrepancy: 1.13 STM / Quality review of work order and logbook entry prior to departure Resolution: Labor USD: No Charge N/ C Discrepancy: 1.14 Towing (Does not include Hangar Moves) Resolution: Towed as required for MX. Billing Method Hours Rate Total Labor USD: Time and Material ST 4.50 @ $118.00 $531.00 Total USD: $531.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WodcOrderPreliminarylnvoicespt Page 4 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01114996 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 1.15 HazMat - Identify & provide a manifest, and a Shipper's Declaration for Dangerous Goods for all hazardous materials that are loaded aboard any aircraft. FAR Part 121 or 135 Operators will provide a hazardous material notification letter required by FAR 135.505 (e) prior to maintenance at this Repair Station iaw FAR 145.206 (a) (b). If there is to be loading of hazardous materials it shall be complied with by Hazmat trained authorized GDAS-PBI personnel only. Resolution: NM --- No Hazmat onboard aircraft at this time. Discrepancy: 1.16 Aircraft Cleaning Resolution: NM Discrepancy: 1.17 Billable Consumables & Shop Supplies Resolution: Billed for Shop Supplies and Consumables as required for MX. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WoikOrderPreliminarylnvoicespt Page 5 of 57 Printed: 4/18/2013 11:38:5 Ftst X EFTA01114997 Bill To: JEGE,INC. WO It: SC13175 Invoice Number: Discrepancy: 1.18 Major Alterations regulatory compliance requirements to be completed by installer as indicated on FAA form 8110-3. Copy and paste from attached statements as needed and edit as required. COMPLY WITH REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d). COMPLIED WITH THE REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d), via GROUND TEST REPORT-REPORT No. CEXXXXXXXX REV. X, ( IN SUPPORT OF STC XXXXXXXXX ) and GR4R216M REPAIR STATION INTERFERENCE TESTING REQUIREMENTS POST MAJOR ALTERATIONS COMPLIANCE FORM. COMPLY WITH REQUIREMENTS OF FAR 25.1529, INSTRUCTIONS FOR CONTINUED AIRWORTHINESS. REF XXXXX MANUAL, P/N XXXXXXX REV. X, FOR INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AND BLOCK 8 OF FAA FORM 337, DATED XX/XX/XXXX. COMPLY WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01.04 AND FAR 25.1353 (B) COMPLIED WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01.04 AND FAR 25.1353 (B) BY ENSURING ROUTING WAS IN ACCORDANCE AC43.13-1B, CHANGE 1 CHAPTER 11, SECTION S. Resolution: NM Discrepancy: 1.19 Update Weight & Balance Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 6 of 57 Printed: 4/18/2013 11:38:5IAD Rd X EFTA01114998 Bill To: JEGE,INC. WO SC13175 Invoice Number: Discrepancy: 1.20 Exterior Paint and Weight & Balance Requirements. Review scope of aircraft exterior paint touch-up/repairs, and skin replacements resulting in paint reapplication, and determine affect on weight and balance. For surfaces where paint is stripped and reapplied or added on top of existing paint on an area greater than 36 square feet the thickness values will be documented before and after painting . If average thickness values remain the same, weight and balance revision is not required. For surfaces painted with an area greater than 36 square feet and before and after paint thickness average varies, QC review for possible weight and balance revision will be required. * Thickness will be plotted on an aircraft drawing derived from AMM chapter 6 or other suitable sketch, attached to the work order and measurements taken on a two square foot grid. * Reference CAMPS 4000, paragraph 3.5.1 for paint restrictions to flight control surfaces and RVSM certified aircraft. * Reference CAMPS 4000, total average thickness shall not exceed 6 mils. * Per GAC Mass Properties Engineering, paint thickness of 5 mils equals .055 pounds per square foot. * If after QC review, weight change is greater than 2 pounds or .05% of MAC, the weight and balance report will require recomputation. Resolution: N/A Discrepancy: 1.21 "Advise customer of preservation requirements per ATA Chapter 10 of the relevant maintenance manuals for Airframe, Engines, and APU; review requirements in relation to scheduled Date Promised and later potential Date Completed; and perform maintenance or preservation actions as directed by the customer and documented as a Work Order Squawk. Resolution: N/A Item: 6 Avionics Team Manager: Sean Brown Pan/Model Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,567.11 / 3,964 Discrepancy: 6.1 RH wing emergency light inop Resolution: Removed defective bulb RH wing emergency light P/N GE303 nsn. Installed new bulb RH wing emergency light P/N GE303 nsn. Op's check good. All work was done JAW Gulfstream GIV AMM 33-10-01. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 7 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01114999 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Billing Method Hours Rate Total Labor USD: Time and Material ST 4.25 @ $118.00 $501.50 Pans USD: Time and Material $28.57 Total USD: $530.07 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 6.1 #1 303 LAMP 1 $1.75 $1.75 6.1 #2 PRI440-B-1/2 SEALANT, PRC,CARTRIDGE 1 $26.82 $26.82 Discrepancy: 6.2 While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #1 HF system does not transmit. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 2.25 @ $118.00 $265.50 Total USD: $265.50 Step: 6.2.1 Completed Verified discrepancy, performed HF press to test on #1 HF control head and received codes 19, 27. and 28 with the RT light illuminated. Hi' receives the Intl clock very clear. When the Press to Talk switch is pressed with the #1 HF system, Fault code 08 appears on the control head with the UP lamp illuminated. Further troubleshooting required at this time. All work performed 1AW G-IV maintenance manual 23-03-00. Discrepancy: 6.3 While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #2 HF system produces a power surge when press to talk is pressed that causes the external AC power cart to shut down. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 0.75 @ $118.00 $88.50 Total USD: $88.50 Discrepancy: 6.4 While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #1 Auto Throttle reports Excessive Friction and Servo Current Failures when tested. Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 8 of 57 Printed: 4/18/2013 11:38:51A) Rd X EFTA01115000 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 6.5 While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #2 Auto Throttle reports Servo Current Failure. Resolution: Discrepancy: 6.6 Performe Cockpit bulb sweep. While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the E-Batts switch capsules just left of the co-pilots yoke are partially loop. Also noted that theupper half of the first digit on the Differential Pressure Guage is out. The upper half of the Radar Stab IRU select switch just forward of the IRU MSU are loop. Resolution: Discrepancy: 6.7 Squawk from flight test - Standby fuel gauge totalizer is indicateing 2001bs lower than the LT and RT fuel gauges and there is a 150lbs difference between total fuel on EICAS primary and systems page compared to STBY totalizer gauge - EICAS and SYSTEMS page ind same Resolution: Step: 6.7.1 Waiting While deluding aircraft noticed that EICAS read 27501bs It and rt and 54001bs total and approval (L) standby ind read 27501bs It and rt but 44001bs total. The standby ind LOW FUEL light came on with 26001bs It and rt(suppose to be 6501bs). Discrepancy: 6.8 Squawk from flight test • LED light burned out on Rate of Climb / FPM (3 digit from LT) on pressurization controller Resolution: Discrepancy: 6.9 Squawk from flight test - With both engines and APU running and both converters on DC volts on the Right-Left-AUX or ESS selected indicate 47.8VDC Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 9 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115001 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 6.10 Squawk from flight test - At FL250 with Batteries only, DC volts on ABEX fluctuates 36.9 to 47.9 v Resolution: Discrepancy: 6.11 Squawk from flight test - RTU 1 there is a cyan line across display on screen - splits screen in half Resolution: Discrepancy: 6.12 Squawk from flight test - On RNAV approach VNAN worked and then became unavailable on approach Resolution: Discrepancy: 6.13 Squawk from flight test - Standby engine instrument gauge is indicating all "88118"s on RT HP gauge Resolution: Discrepancy: 6.14 Squawk from flight test - HF radios operated normally but NO SELCAL Resolution: Discrepancy: 6.15 EGPWS/Terrain database outdated Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WodcOrderPreliminarylnvoicespt Page 10 of 57 Printed: 4/18/2013 11:38:5IAD Ftst X EFTA01115002 Bill To: JEGE, INC. WO ft: SC13175 Invoice Number: Discrepancy: 6.16 Squawk from flight test - aft LAV reading light is Mop Resolution: Discrepancy: 6.17 Squawk from flight test - cabin management display at VIP , galley screen Mop Resolution: Discrepancy: 6.18 Squawk from flight test - perform ops test of nose camera Resolution: Discrepancy: 6.19 Satphone is inop Resolution: Item: 7 Interior Team Manager: Sean Brown Pan/Model 0: Customer Coordinator: Ray Kraher AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 7.1 Squawk [ruin flight test - FWD LAV water does not pump Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page I I of 57 Printed: 4/18/2013 11:38:5IAli Rd X EFTA01115003 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 7.2 Squawk from flight test - LH galley aft cutting board does not latch Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 0.87 @ $118.00 $102.66 Pans USD: Time and Material $1.86 Total USD: $104.52 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 7.2#1 MINI-LATCH SELBY-LATCH WHITE NICKEL 1 $1.86 $1.86 Step: 7.2.1 Completed Removed galley drawer and galley latch. All work performed IAW GIV MM 25-20-00. Discrepancy: 7.3 Squawk from flight test - RH #5 window shade does not fully close Resolution: Discrepancy: 7,4 Squawk from flight test - pax air gaspers loose, takes two hands to close the outlet Resolution: Discrepancy: 7,5 Squawk from flight test - fwd cabin door angle wing does not hit headliner when closed. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 2.10 @ $118.00 $247.80 Total USD: $247.80 Step: 7.5.1 Waiting Removed fwd pocket door, inspected pop-up door closeout mechanics, found no defects Insp at this time, lubricated mechanical areas as required, re-installed fwd door and pop-up door closeout still would not fully close. Further evaluation is needed. All work performed IAW GIV MM 25-20-00. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 12 of 57 Printed: 4/15/2013 11:38:5IA) Ftst X EFTA01115004 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Item: 8 Mechanical Team Manager: Sean Brown Pan/Model #: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 8.1 The No. 1 engines Outboard igniter plug is worn Resolution: Remove engine #1 ignitor plug #2 P/N Y183-5 S/N 1204. Instaled new engine #1 ignitor plug #2 P/N Y183-5 S/N 12047184. JAW RR EMM 74-21-03. Parts USD: No Charge N/C Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.1 #1 Y183-5 PLUG, IGNITOR 1 $0.00 $0.00 Discrepancy: 81 The No. 2 engines Outboard igniter plug is worn Resolution: Remove Engine #2 ignitor #2 P/N Y183-5 S/N 0601749. Installed new Engine #2 ignitor #2 P/N Y183-5 S/N 12047194. JAW RR EMM 74-21-03. Parts USD: No Charge N/C Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.2 Y183-5 PLUG, IGNITOR 1 $0.00 $0.00 Discrepancy: 8.3 The Left engine S/N 16291, No.8 combustion liner has a 1.8" crack and part of the crossover tube shroud is missing. Pictured sent to rolls royce. Resolution: With further investigation on the No.8 combution liner on the left engine S/N 16291, found the cranks to be within limits JAW the Rolls Royce TAY611-8 EMM chapter 71.00.00, and no further action is needed. With further investigation found the crossover tube to only have minor errosion and some carbon build up No further action is required on this item. All work performed JAW the Rolls Royce TAY611.8 EMM chapter 71.00.00. Discrepancy: 8.4 The Right engine S/N 16292, No.4 combustion liner has 4 cracks. (1.0", 3.2", 4.0", and 5.6") and over 30 HPT stage one bases LE cracked. Pictured sent to rolls royce. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 13 of 57 Printed: 4/18/2013 11:38:51A? Ftst X EFTA01115005 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Resolution: With further investigation of the No.4 combution liner of the right engine S/N 16292 found the cracking to only be 25% of what was originally determined. Total circumferential cracking was found to be less than 40% and no further special inspections will be needed for this item. All work was performed JAW the Rolls Royce TAY611-8 EMM chapter 71.00.00. Two HPT stage 1 Blade tips was found to be cracked on the LE with the crack protruding into the airfoil 0.050" (1.25mm). All work was performed IAW the Rolls Royce TAY611.8 EMM Task 71.00.00.210.001 (9)(a)(iii). Re-Inspect the blades within 400 hours (8,928.0 TSN) or 400 cycles (4,335 CSN) whichever occurs first. This crack can protrude into the airfoil up to a length of 0.315" (8.00 mm) Discrepancy: 8.5 Squawk from flight test - rubber stripping on leading edge of LT and RT MLG doors are torn Resolution: Removed damaged sections of rubber seal P/N GASl3AN-1.41from around L/H and R/H MLG bays, and installed new seal P/N GAS13AN-1-41 I/A/W GIV AMM 20-42-00 Billing Method Hours Rate Total Labor USD: Time and Material ST 2.08 @ $118.00 $245.44 Pans USD: Time and Material $109.18 Total USD: $354.62 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.5 #1 GASl3AN-1.41 SEAL, BUTTONED STRIP, WHEEL I $109.18 $109.18 WELL DOOR (5' SECTION) Discrepancy: 8.6 Squawk from flight test - Copilots seat is difficult to move in fore-aft position Resolution: Removed copilot seat and inspected seat track and rollers. Found no defects. Lubed seat track and rollers. Moved seat fore and aft with satisfactory results. Reinstalled copilot seat. Ref: GIV ALUM 25-11.00. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.00 @ $118.00 $236.00 Total USD: $236.00 Discrepancy: 8.7 Squawk from flight test - Gear emergency reset handle not safetied (D-ring) Resolution: Safetied Gear Emergency Reset Handle (D-ring) IAW GIV AMM 32-00-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.70 @ $118.00 $200.60 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WoikOrderPreliminarylnvoice.rpt Page 14 of 57 Printed: 4/18/2013 11:38:5 IAD Rd X EFTA01115006 Bill To: JEGE, INC. WO 9: SC13175 Invoice Number: Total USD: $200.60 Discrepancy: 8.8 Squawk front flight test - Flaps shudder felt when flaps selected to 39 degrees Resolution: Discrepancy: 8.9 Squawk from flight test - screw needs tightening on panel behind pilots seat below CB panel Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 0.50 @ $118.00 $59.00 Total USD: $59.00 Discrepancy: 8.10 Squawk from flight test - on the ground the flaps would intermittenly move from 20 to 39 degrees and 10 to 20 when selected. Resolution: Billing Method flours Rate Total Labor USD: Time and Material ST 20.92 @ $118.00 $2,468.56 Total USD: $2,468.56 Discrepancy: 8.11 Squawk from flight test - power levers have 1/2 knob split at 15000ft and 80%HP (It lever is fwd) Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 15 of 57 Printed: 4/182013 11:38:51A) Rd X EFTA01115007 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 8.12 Squawk from flight test - while climbing through FL 430 with LT Pack OFF the RT Pack was 25psi (should be 27-33psi) Resolution: Discrepancy: 8.13 Squawk from flight test - while climbing through FL 430 with RT Pack OFF the LT Pack was 23psi (should be 27-33psi) Resolution: Discrepancy: 8.14 Squawk from flight test - One O2 mask in LAV and LT and RT AFT rear did not drop during test Resolution: Verified that aft left,aft right and lay oxygen masks would not deploy. Adjusted mask lid holding spring clips on all 3 mask boxes. Performed funtional check of the 3 locations. Ops checked good. No further defects noted. Billing Method Hours Rate Total Labor USD: Time and Material ST 4.36 @ $118.00 $514.48 Total USD: $514.48 Discrepancy: 8.15 Squawk from flight test - service hydraulic replenisher Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 1.20 @ $118.00 $141.60 Pans USD: Time and Material $319.92 Total USD: $461.52 Parts: Ref. No. P:nt number: Description Quantity Sell price USD Extended USD 8.15 500B4QT SKYDROL OIL IN QUART CANS 6 $53.32 $319.92 Discrepancy: 8.16 Squawk from flight test - At FL400 and climbing, RT engine MCI' was 1.79 but could only indicate 1.78 before LP RPM has an exceedance Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 16 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115008 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 8.17 While compling with APU GTCP36.100(G) Borescope the following was found. The plenum is cracked, the nozzle guide vane TE's are erroded and cracked, and the turbine wheel tips are erroded. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 1.47 @ $118.00 $173.46 Services USD: No Charge N/ C Total USD: $173.46 Services: Ref. No. Description Quantity Sell Price USD Extended USD 8.17 #1 REPAIR 1.00 $0.00 $0.00 Part Ref: GTCP36-100G APU (3800062-9-1) Step: 8.17.1 Completed Removed APU generator P/N I1598CAV373-105 SIN 129A0171 I/A/W G1V AMM 24-01-01 and sent APU out for repair. Discrepancy: 8.18 While tightening screw for squawk 8.9 found that the inboard metal protector (located on panel behind copilots seat) for the coplilots seat is bent and is cutting into copilot seat back rest. Resolution: Billing Method flours Rate Total Labor USD: Time and Material ST 1.50 @ $118.00 $177.00 Total USD: $177.00 Discrepancy: 8.19 Squawk from flight test - There is a soft spot in floor hoard just fwd of fwd LAV (feels like blowout panel isnt secure) Resolution: Removed broken clip P/N 159B10732-13 from blowout panel forward of forward lay and replaced with new clip P/N 159B10732-13 IAW GAC Drawing 159B10732. Billing Method flours Rate Total Labor USD: Time and Material ST 4.91 @ $118.00 $579.38 Pans USD: Time and Material $86.10 Total USD: $665.48 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryinvoicespt Page 17 of 57 Printed: 4/18/2013 I I:38:51AP Flet X EFTA01115009 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.19 NI 159B10732-13 SPRING CLIP 2 $43.05 $86.10 Discrepancy: 8.20 Evaluate flaking paint from steel doubler and adjacent structure on L/H horizontal stab at panel 38-UPR-4. Ref to sqk 15.25 Resolution: Cleaned suspect area and after further evaluation found no defects. No further action required. Work perfromed JAW GIV SRM 51.13.00. Billing Method Flours Rate Total Labor USD: Time and Material ST 3.40 @ $118.00 $401.20 Total USD: $401.20 Discrepancy: 8.21 While working sqk 15.26 CMP 551024. Found corrsion and pitting horizontal stabilizer skin at panel 38-UPR-5. Resolution: Removed minor surface corrosion and pitting from panel opening mounting flange of panel 38-UPR-5, cadmium plated exposed surface and applied coat of primer. All work done IAW GIV SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 733 @ $118.00 $864.94 Labor USD: Time and Material OT 0.10 @ $177.00 $17.70 Total USD: $882.64 Step: 8.21.1 Completed Nlechanicaly removed minor surface corrosion and pitting from panel opening mounting flange and cadmium plated exposed surface. All work done lAW GIV SRM 51-13-10. Discrepancy: 8.22 While working sqk 15.26 CMP 551023. Found corrsion and pitting horizontal stabilizer skin at panel 39-UPR-5. Resolution: Removed minor surface corrosion and pitting from panel opening mounting flange of panel 39-UPR-5, cadmium plated exposed surface and applied coat of primer. All work done JAW GIV SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 635 @ $118.00 $749.30 Labor USD: Time and Material OT 0.92 @ $177.00 $162.84 Total USD: $912.14 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 18 of 57 Printed: 4/18/2013 11:38:5 1Ali toe X EFTA01115010 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Step: 8.22.1 Completed Mechanical,' removed minor surface corrosion and pitting front panel opening mounting flange and cadmium plated exposed surface. All work done IAW GIV SRM 51-13-10. Discrepancy: 8.23 While working CMP 551023 sqk 15.25. Found horizontal stab thrust blocks to be worn out of limits. Resolution: Discrepancy: 8.24 #2 Engine EPR Flex line chaffing against fixed cowl. (Flagged) Resolution: Adjusted orientation of #2 Engine EPR Flex Line IAW GIV AMM 77-01-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.28 @ $118.00 $387.04 Total USD: $387.04 Discrepancy: 8.25 #2 Engine has multiple corroded clamps on forward IB area of engine. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 0.50 @ $118.00 $59.00 Total USD: $59.00 Discrepancy: 8.26 While performing wing HI-lite Collar (left) inspection CMP code 571011 found collar cracked at LBL 44.0 Resolution: Removed cracked HI-lite Collar at LBL 44.0, and installed new Colter P/N IIST70-8. All maintenance performed IAW Gulfstream GIV ASC 446 AMI. Billing Method Hours Rate Total Labor USD: Time and Material ST 0.47 @ $118.00 $55.46 Total USD: $55.46 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 19 of 57 Printed: 4/18/2013 11:38:5 IA) Ftst X EFTA01115011 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 8.27 While gaining access to cracked Hi-Lite Collar at LBL 44.0 found fasteners wet with hyd fluid at top of wing box section left and right of BL-0 Resolution: Billing Method Houri. Rate Total Labor USD: Time and Material ST 9.03 @ $118.00 $1,065.54 Total USD: $1,065.54 Discrepancy: 8.28 While performing wing HI-lite Collar RT inspection CMP code 571012 found a dented fuel line on center wing leading edge. Resolution: Billing Method Houri. Rate Total Labor USD: Time and Material ST 632 @ $118.00 $745.76 Pans USD: Time and Material $116.32 Total USD: $862.08 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.28 #1 D10036D06 UNION. PERMASWAGE 1 $51.50 $51.50 8.28 #2 D10036D06 UNION. PERMASWAGE 1 $51.50 $51.50 8.28 #3 6061T6-.375X.028 TUBING, ALUMINUM-3/8 2 $6.66 $13.32 Step: 8.28.1 Completed Cut and removed 6" section with dent front fuel line PIN:1159N2012-0221/P6 at RBS255.5 of RIR wing. Spliced in new 6" section of tubing on fuel line P/N:1159P42012.022FT6 at RBS255.5 of Ral wing. All work done IAN' GAMPS 2507. Discrepancy: 8.29 While T/S the squawk (8.10) for the flaps moving intermittenly found that the LH outboard flap actuator failed the Ballnut End Play check. Endplay is .038in., limit is .012in. Resolution: Billing Method Hours Rate Total Pans USD: Time and Material $38,000.00 Total USD: $38,000.00 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 819 11 1159SCC212-15 ACTUATOR.FLAP DRIVE, L- 1 $38,000.00 $38,000.00 OUTBOARD For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelitninaryInvoicespt Page 20 of 57 Printed: 4/15/2013 11:38:5 IA) Rd X EFTA01115012 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 8.30 While T/S the squawk (8.10) for the flaps moving intermittenly found that the LH inboard flap actuator failed the Ballnut End Play check. Endplay is .057in., limit is .012in. Resolution: Billing Method Hours Rate Total Pans USD: Time and Material $38,000.00 Total USD: $38,000.00 Parts: Ref. No. Pail number: Description Quantity Sell price USD Extended USD 830 /1 II59SCC211-15 ACTUATOR, FLAP DRIVE, INBD 1 $38,000.00 $38,000.00 Discrepancy: 8.31 While T/S the squawk (8.10) for the flaps moving intermittenly found that the RH outboard flap actuator failed the Ballnut End Play check. Endplay is .061in., limit is .012in. Resolution: Billing Method Houri. Rate Total Pans USD: Time and Material $76,000.00 Total USD: $76,000.00 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 83112 1159SCC212-16 ACTUATOR, FLAP DRIVE, R- 1 $38,000.00 $38,000.00 OUTBOARD 831 N3 1159SCC212-16 ACTUATOR, FLAP DRIVE, R- I 538,000.00 $38,000.00 OUTBOARD Discrepancy: 8.32 While T/S the squawk (8.10) for the flaps moving intermittenly found that the RH inboard flap actuator failed the Ballnut End Play check. Endplay is .030in., limit is .012in. Resolution: Billing Method Hours Rate Total Pans USD: Time and Material $38,000.00 Total USD: $38,000.00 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 83212 I I59SCC211.15 ACTUATOR, FLAP DRIVE, INBD 1 $38,000.00 $38,000.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 21 of 57 Printed: 4/18/2013 11:38:5IA) Rd X EFTA01115013 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 8.33 Found several chips and a soft spot that light can be seen through on the radonw nose, under the errosion hoot. Resolution: Discrepancy: 8.34 The RH flap's "C" tracks forward, inboard bearing is bad (1159SCC228.23) Resolution: C/W CMP 275123. Removed worn R/H flap "C" track roller P/N 1159SCC228-23. Installed new roller P/N 1159SCC228-23. All work I.A.W. GIV M/M 27-06.00. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.05 @ $118.00 $241.90 Pans USD: Time and Material $562.00 Total USD: $803.90 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.34 #1 1159SCC228-23 ROLLER -FLAP 1 $562.00 $562.00 Discrepancy: 8.35 The LH flap's "B" tracks AFT, outboard bearing is bad (1159SCC226-7) Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 4.47 @I $118.00 $527.46 Labor USD: Time and Material OT 0.18 @ $177.00 $3L86 Pans USD: Time and Material $1,590.32 Total USD: $2,149.64 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 835 #1 1159SCC426-11 BEARING, FLAP TRACK ROLLER 1 $819.88 $819.88 EXT 835 #2 1159SCC426-9 BEARING. TRACK ROLLER EXT - 1 S770.44 $770.44 FLAP Step: 8.35.1 Completed Complied with GIV CMP 275117 wing flap roller (Leftr outboard upper Aft B Track B-9) - Removal/Installation. steps A to B(2) and B(5)(a) to B(5Xb). Removed defected flap roller P/N: 1159SCC266-7, NSN. Work done IAW GIV CMP 275117 & GIV hl/M 27-06-00. Discrepancy: 8.36 The LH flap track "A" has corrosion For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 22 of 57 Printed: 4/18/2013 11:38:5 IA) toe X EFTA01115014 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 8.50 @ $118.00 $1,003.00 Total USD: $1,003.00 Step: 8.36.1 Waiting Removed light surface corrosion and pitting from IJH flap track "A" IAW GIV AMM Insp 27-06-00. Discrepancy: 8.37 The LH flap track "B" has corrosion Resolution: Billing Method !lours Rate Total Labor USD: Time and Material ST 0.50 @ $118.00 $59.00 Total USD: $59.00 Discrepancy: 8.38 The LH flap track "C" has corrosion Resolution: Billing Method I lours Rate Total Labor USD: Time and Material ST 0.50 @ $118.00 $59.00 Total USD: $59.00 Discrepancy: 8.39 The LH ❑ap track "I)" has corrosion Resolution: Billing Method Holm Rate Tot Labor USD: Time and Material ST 0.50 @ $118.00 559.00 Total USD: 559.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WoikOrderPreliminarylnvoicespt Page 23 of 57 Printed: 4/18/2013 11:38:5 IA) Ref X EFTA01115015 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 8.40 The RH flap track "A" has corrosion Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 0.50 @ $118.00 559.00 Total USD: $59.00 Discrepancy: 8.41 The RH flap track "B" has corrosion Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 1.50 @ $118.00 $177.00 Total USD: $177.00 Discrepancy: 8.42 The RH flap track "C" has corrosion Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 4.33 @ $118.00 $510.94 Total USD: $510.94 Discrepancy: 8.43 The RH flap track "D" has corrosion Resolution: Discrepancy: 8.44 The LH flap track "B" has play in the fwd attach bolt Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 24 of 57 Printed: 4/18/2013 11:38:5IA) Rd X EFTA01115016 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Billing Method Houri. Rate Total Labor USD: Time and Material ST 3.73 @ $118.00 $440.14 Pans USD: Time and Material $481.99 Total USD: $922.13 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.44 #1 1159Wd120235.3 BUSHING 2 $224.66 $449.32 8.44#2 NASI312-23 BOLT I $31.42 $31.42 8.44 #3 MS21083NI2 NUT I $1.25 $1.2.5 Discrepancy: 8.45 The RH flap track "0" has play in the fwd attach Molt Resolution: Billing Method Houri. Rate Total Parts USD: Time and Material $481.99 Total USD: $481.99 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.45 #1 1159WM20235.3 BUSHING 2 $224.66 $449.32 8.45 #2 NASI312-23 BOLT I $31.42 $31.42 8.45 #3 MS21083N12 NUT 1 $1.25 $1.25 Discrepancy: 8.46 Install prep and seal panels on tail surfaces. See steps for applicable sections. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 10.53 @ $118.00 $1,242.54 Labor USD: Time and Material OT 0.20 @ $177.00 $35.40 Total USD: $1,277.94 Step: 8.46.1 Completed Preped and sealed panel on vertical stab. Panel edge sealant ready for paint. IAW GIV AMM 20.00.00 Step: 8.46.2 Completed Sealed panels on the upper vertical on the left and right. Closed left horiz stab trailing edge panels, taped and ready to seal 37-UPR-1, 37-UPR-3, 37-UPR-5 and 37-UPR-7. REF G1V MM 27.00.00 Discrepancy: 8.47 APU enclosure and apu mount have heavy soot residue Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 25 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115017 Bill To: JEGE,INC. WO #: SCI3175 Invoice Number: Billing Method Hour,. Rate Total Labor USD: Time and Material ST 4.00 $118.00 $472.00 Total USD: $472.00 Discrepancy: 8.48 Squawk From night test - during climb #2 engine went into RED, pilots had to manually pull throttle back Resolution: Discrepancy: 8.49 Squawk from flight test - #1 engine was hotter than #2 by 80+ degrees Resolution: Discrepancy: 8.50 R/H lower wing skin has corrosion near panel 22-FT-11 Resolution: Discrepancy: 8.51 Rill lower wing skin has corrosion near panel 22•Ff•14 Resolution: Discrepancy: 8.52 R/H lower wing skin has corrosion near panel 22-FT-15 Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 26 of 57 Printed: 4/18/2013 11:38:5 IA) are 3: EFTA01115018 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 8.53 R/Ii lower wing skin has corrosion near panel 22-FT-7 Resolution: Discrepancy: 8.54 While C/W CMP 275123 sqk 8.34. CMP 275123 preferres that corresponding roller be replaced at same time. Resolution: Discrepancy: 8.55 While C/W CMP 275117 sqk 8.35. CMP 275117 preferres that corresponding roller be replaced at same time. Resolution: Discrepancy: 8.56 While removing R/II wing fuel panel 22-FT-1 for sqk 1532. Found ground mesh on panel to be torn. pn 1159WNI40076-13 Resolution: Item: 9 Paint Team Manager: Sean Brown Part/Model it: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 9.1 Ft/H lower wing skin has corrosion near panel 22-FT-7 Resolution: duplicate item to 8.53 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 27 of 57 Printed: 4/18/2013 11:38:5IA) Rd X EFTA01115019 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Item: 10 Outstanding Parts, Materials, and / or Services Team Manager: Sean Brown ParUModel Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 10.1 Service for Signature for LAV service Resolution: Services USD: No Charge N/ C Services: Ref. No. Description Quantity Sell Price USD Extended USD 10.1 B1 REPAIR AND UPGRADE 1.00 $0.00 $0.00 Item: 12 Aircraft Records and Logbook Research Only Team Manager: Sean Brown Pan/Model 0: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 12.1 Comply with Aircraft Records and Logbook Research Resolution: Complied with Aircraft Records and Logbook Research as required. See discrepancies below. Billing Method Flours Rate Total Labor USD: Flat Rate $13,000.00 Total USD: $13,000.00 Step: 12.1.1 Completed CiM, part of the aircraft avionics equipment inventory list. More inventory required. Step: 12.1.2 Completed Continued with the aircraft avionics equipment inventory list. More inventory required. Step: 12.1.3 Completed Continued with avionics inventory. Need to check with CMP to complete. Step: 12.1.4 Completed Completed GIA Aircraft Avionics Equipment Inventory List. Discrepancy: 12.2 No log entry found for the removal of NLG rod end P/N 1159HM40120-1 and the installation of P/N 1159SCL567-3. Mandatory CB 183 was PCW by Duncan Aviation on 10/24/06. Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryinvoicespt Page 28 of 57 Printed: 4/182013 11:38:51M. Ftst X EFTA01115020 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 12.3 No log entry or tag was found for API. Fire bottle P/N AE30903823 S/N AENI.23 installed on 2/28/2005. Resolution: Discrepancy: 12.4 No log entry was found for NIA; Axle Assy. P/N 1159LM40544-7 S/N BFG6056NTW installed on June 3, 1999. Resolution: Discrepancy: 12.5 No 8130 found for Pilot'& Co-pilot side window attach bolts. Replaced on 12/11/98. Resolution: Discrepancy: 12.6 No 8130 found for isolator LJH Aft Fwd. S/N 2998 installed on 12/11/98. Resolution: Discrepancy: 12.7 No 8130 found for isolator LH Aft aft S/N 2982 installed on 12/11/98. Resolution: Discrepancy: 12.8 No 8130 found for isolator R/H Aft Fwd. S/N 2993 installed on 12/11/98. Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 29 of 57 Printed: 4/18/2013 11:38:5IA) Rd X EFTA01115021 Bill To: JEGE,INC. WOO:S(13175 Invoice Number: Discrepancy: 12.9 No 8130 found for isolator R/II .\ft .\ft. S/N 2994 installed on 12/11/98. Resolution: Discrepancy: 12.10 No 8130 or log entry• found for nose wheel steering unitinstalled on 10/11/06. Resolution: Discrepancy: 12.11 AD74.08.09 R3 Lavatory Paper and Linen Waste Receptacle Enclosure Access Door and Disposal Door Inspection is due in 126.7 Hours Resolution: Item: 13 APU Borescope Team Manager: Sean Brown Pan/Model 0: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8567.0 / 3,964 Discrepancy: 13.1 Comply with APU GTCP36-100(G) - Borescope Resolution: Complied with APU GTCP36-100(G) - Borescope Inspection JAW Honeywell GTCP36-100(G) MM 49-20-00. REF Item 8.17 for discrepancies found. Billing Method flours Rate Total Labor USD: Flat Rate $900.00 Total USD: $900.00 Discrepancy: 13.2 Comply with CMP GIV 490001 APU GTCP36-100(G) - Removal / Installation For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoice.rpt Page 30 of 57 Printed: 4/18/2013 11:38:5 Ali Rd X EFTA01115022 Bill To: JEGE,INC. WO #: SCI3175 Invoice Number: Resolution: Removed APU GTCP36-100, S/N P-465-C, with 6,449.0 TSN from GIV, N423T1', S/N 1085, IAN the GIV MM chapter 49.10.00. Billing Method flours Rate Total Labor USD: Time and Material ST 5.00 $118.00 $590.00 Total USD: $590.00 Step: 13.2.1 Completed Removed APU Per CMP 490001 From A. BI la. ; tin ; Perforincil In Reference To GIV AMM 49-10-00. Discrepancy: 13.3 Comply with CMP GIV 490005 APU Enclosure GTCP36-100(C) - Inspection Resolution: Discrepancy: 13.4 Comply with CMP GIV 490002 APU GTCP36-100(G) - Ops Test Resolution: Item: 14 Engine Runs and Borescope Team Manager: Sean Brown Pan/Model #: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TS0: CSN/CS0: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 14.1 Comply with Engine Runs and Borescope Resolution: Billing Method flours Rate Total Labor USD: Flat Rate $14,500.00 Total USD: $14,500.00 Discrepancy: 14.2 CMP GIV 710019 Powerplant Internal - Inspection For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_Work0rderPrelintinaryInvoicespt Page 31 of 57 Printed: 4/18/2013 11:38:5IA) Rd X EFTA01115023 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Resolution: C/W CMP GIV 710019 Powerplant Internal - Inspection I/A/W GIV AMM 71-00-00 No defects noted Labor USD: No Charge N/C Parts USD: No Charge N/C Discrepancy: 14.3CMP GIV 710025 Engine Borescope - Inspection Resolution: COMPLIED WITH CMP GIV 710025 Engine Borescope - Inspection IAW RR TAY EMM 71-00-00. Billing Method Flours Rate Total Labor USD: No Charge N/C Parts USD: Time and Material $332.33 Total USD: $332.33 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 143 #1 AS43013-210 ORING 1 $17.72 $17.72 143 #2 A543013-348 ORING 2 $59.74 $119.48 143 #3 KB22748 O-RING I $10.51 $10.51 143 #4 PL32M SEALANT 2 $92.31 $184.62 Step: 143.1 Completed Gained access for Borescope. IAW CMP 710025 paragraph (B) 1-10 Step: 143.2 Completed Complied with ChIP 710025 from step (11)(a) through step (51)(c) lAW the rolls Royce TAY611.8 nun chapter 71.00-00. See squawk 8.3 Step: 143.3 Completed Complied with ChIP 710025 paragraph 53, (A)-(E) 1-7, 57-58 (A)-(E). Note could not install other access plugs do to having to order Hylontar. Step: 143.4 Completed Left #2 ENG open being that had to order Hy lomar and also awaiting possible second opinion from RR Step: 143.5 Completed Install all inner and outer engine panels and bore scope plugs IAW Rolls Royce TAY- Ehlhl Chapter 71-00-00. Discrepancy: 14.4 CMP GIV 710031 Engine - Operational Test Resolution: COMPLIED WITH CMP GIV 710031 Engine - Operational Test. Labor USD: No Charge N/C Discrepancy: 14.5 CMP GIV 730001 Fuel Contamination Check (Engine) - Inspection Resolution: C/W CMP GIV 730001 Fuel Contamination Check (Engine) - Inspection I/A/W RR Tay 611.8 EMM 73-11.03. No defects noted For detail description of the work complied with see the Work Order Detail report. Unless (Ahem' indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 32 of 57 Printed: 4/18/2013 11:38:5 IA) Rst X EFTA01115024 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 14.6 CMP GIV 742001 Engine Ignition System - Operational Test Resolution: COMPLIED WITH CMP GIV 742001 Engine Ignition System - Operational Test. Ops Check Ok. All Maintenence Performed In Reference To GIV AMM 74-00-00. Discrepancy: 14.7 CMP GIV 742006 Eng 1/ No. 2 Igniter Plug - Removal / Installation Resolution: Remove engine #1 ignitor plug #2 P/N Y183-5 SIN 1204. Instaled new engine #1 ignitor plug #2 PIN Y183-5 S/N 12047184. IAW RR EMM 74-21-03. Discrepancy: 14.8 CMP GIV 742016 No. 2 Igniter Plug - Inspection Resolution: COMPLIED WITH CMP GIV 742016 No. 2 Igniter Plug - Inspection. REF item 8 for discrepancies found. Work performed IAW RR MM 74.21.03. Discrepancy: 14.9 CMP GIV 774955 CHIP DETECTOR, ENG--INSP Resolution: C/W CMP GIV 774955 CHIP DETECTOR, ENG--INSP UMW RR Tay 6-11 EMM 77-33-01 No defects noted Billing Method Hours Rate Total Labor USD: No Charge l'i/ C Pans USD: Time and Material $176.00 Total USD: $176.00 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.9#2 BR49120 RING 4 $11.00 $44.00 14.9 #3 BR49120 RING 12 $11.00 $132.00 Discrepancy: 14.10 CMP GIV 792007 Filter, Engine Pressure Oil - Cleaning/Inspection Resolution: C/W CMP GIV 792007 Filter, Engine Pressure Oil - 72.01.01. No defects noted For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 33 of 57 Printed: 4/18/2013 11:38:5IA) Rd X EFTA01115025 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Billing Method Houri. Rate Total Labor USD: No Charge N/ C Pans USD: Time and Material $33.25 Total USD: $33.25 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.10 #3 1159CGSK792007 LIENG.OIL FILTER - R&I / 1000-3999 1 S33.25 $33.25 Discrepancy: 14.11 CMP GIV 792013 Engine Scavenge Strainers - Inspection Resolution: C/W CMP GIV 792013 Engine Scavenge Strainers - Inspection UMW RR Tay 611-8 EMM 72.01.01 No defects noted Billing Method Hours Rate Total Labor USD: No Charge N/ C Pans USD: Time and Material $195.60 Total USD: $195.60 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.11 #2 KB22722 O-RING 1 $8.40 $8.40 14.11 #3 KB22726 SEAL I $8.03 $8.03 14.11 #4 KB22727 O-RING 4 $33.00 $132.00 14.11 #5 KB22730 SEAL 2 $7.62 $15.24 14.11 #6 KB22732 0 RING I $31.93 $31.93 Discrepancy: 14.12 CMP GIV 710020 Powerplant Internal - Inspection Resolution: COMPLIED WITH CMP GIV 710020 Powerplant Internal - Inspection IAW GIV AMM 71.00.00. Ref 8.24 for descrepancies. Labor USD: No Charge N/ C Discrepancy: 14.13 CMP GIV 710026 Engine Borescope - Inspection Resolution: COMPLIED WITH CMP GIV 710026 Engine Borescope - Inspection IAW RR TAY EMM 71.00.00. Billing Method Flours Rate Total Labor USD: No Charge N/ C Pans USD: Time and Material $147.71 Total USD: $147.71 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 34 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115026 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.13 #1 kS43013-210 ORING 1 $17.72 $17.72 14.13#2 AS43013-348 ORING 2 $59.74 $119.48 14.13 #3 KB22748 O-RING 1 $10.51 $10.51 Step: 14.13.1 Completed Gained access for Borescope. lAW CMP 710025 paragraph (B) 1-10 Step: 14.13.2 Completed Complied with CMP 710026 from step (11)(a) through step (51)(c) lAW the rolls Royce TAY611.8 nun chapter 71.00-00. See squawk 8.4. Step: 14.13.3 Completed Install all inner and outer engine panels and bore scope plugs 1AW Rolls Royce TAY- EMM Chapter 71.00.00. Discrepancy: 14.14 CMP GIV 710032 Engine - Operational Test Resolution: Discrepancy: 14.15 CMP GIV 730002 Fuel Contamination Check (Engine) - Inspection Resolution: COMPLIED WITH CMP GIV 730002 Fuel Contamination Check (Engine) - Inspection. No defects noted IAW RR TAY 611-8 MM 73-11-03. Labor USD: No Charge N/ C Discrepancy: 14.16 CMP GIV 742002 Engine Ignition System - Operational Test Resolution: COMPLIED WITH CMP GIV 742002 Engine Ignition System - Operational Test. Ops Check Ok. All Maintenence Performed In Reference To GIV AMM 74-00-00. Discrepancy: 14.17 CMP GIV 742008 Eng #2 / No. 2 Igniter Plug - Removal / Installation Resolution: Remove Engine #2 ignitor #2 P/N Y183-5 S/N 0601749. Installed new Engine #2 ignitor #2 P/N Y183-5 S/N 12047194. JAW RR EMM 74-21-03. Discrepancy: 14.18 CMP GIV 742018 No. 2 Igniter Plug - Inspection For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 35 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115027 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Resolution: COMPLIED WITH CMP GIV 742018 No. 2 Igniter Plug- Inspection. REF Item 8.2 for discrepancies found. Work performed IAW RR MM 74.21.03 Discrepancy: 14.19 CMP GIV 774956 CHIP DETECTOR, ENG--INSP Resolution: COMPLIED WITH CMP GIV 774956 CHIP DETECTOR, ENG—INSP. No defects noted LAW RR TAY 611.8 MM 77-33.01. Billing Method Hours Rate Total Labor USD: No Charge N/ C Pans USD: Time and Material $176.00 Total USD: $176.00 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.19 #1 BR49120 RING 12 $11.00 $132.00 14.19#2 BR49120 RING 4 $11.00 $44.00 Discrepancy: 14.20 CMP GIV 792009 Filter, Engine Pressure Oil - Cleaning/Inspection Resolution: COMPLIED WITH CMP GIV 792009 Filter, Engine Pressure Oil - Cleaning/Inspection. No defects noted IAW RR TAY 611-8 MM 72-01-01. Billing Method Houri. Rate Total Labor USD: No Charge N/ C Pans USD: Time and Material $31.25 Total USD: $31.25 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.20#2 EU18144 WASHER 1 $8.80 $8.80 14.20 #3 KB22782 SEAL 1 $22.45 $22.45 Discrepancy: 14.21 CMP GIV 792014 Engine Scavenge Strainers - Inspection Resolution: COMPLIED WITH CMP GIV 792014 Engine Scavenge Strainers - Inspection. No defects noted IAW RR TAY 611-8 MM 72-01-01. Billing Method Hours Rate Total Labor USD: No Charge N/C Pans USD: Time and Material $195.60 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 36 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115028 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Total USD: $195.60 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.21 #2 KB22722 O-RING 1 $8.40 $8.40 14.21 #3 KB22726 SEAL 1 $8.03 $8.03 14.21 #4 KB22727 O-RING 4 $33.00 $132.00 14.21 #5 KB22730 SEAL 2 $7.62 $15.24 14.21 #6 KB22732 0 RING 1 $31.93 $31.93 Discrepancy: 14.22 Related CMP Codes Resolution: Discrepancy: 14.23 CMP GIV 711009 Cowl Latch, Engine (Left) - Rigging Resolution: CM CMP GIV 711009 Cowl Latch, Engine (Left) - Rigging GIV AMM 71-02-00 No defects noted Billing Method Hours Rate Total Labor USD: Flat Rate $230.00 Total USD: $230.00 Discrepancy: 14.24 CMP GIV 732001 Engine Acceleration Test / Adjustment Resolution: Step: 14.24.1 Completed Removed all R/H horizontal stabilizer panels required for CMP 551020. AB work I.A.W. GIV NUM 55-14-00. Discrepancy: 14.25 CMP GIV 732005 Engine Deceleration Test / Adjustment Resolution: Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Parts USD: No Charge N/ C For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 37 of 57 Printed: 4/18/2013 11:38:5 IA) Ftst X EFTA01115029 Bill To: JEGE, INC. WO 8: SC13175 Invoice Number: Total USD: $460.00 Discrepancy: 14.26 CMP GIV 732049 ENG HANDLE ACU SOLENOID CK Resolution: Step: 14.26.1 Completed In progress removal of R/H horizontal stabilizer and elevator panels required for CMP 551023 ;Panels on top of R/H elevator still need to be removed, for details of panels removed refer to the open and close section of the R/1 log book . All work I.A.W. GIV MAI 55-14-00. Discrepancy: 14.27 CMP GIV 732057 SOLENOID, ENG APPR IDLE-OPS Resolution: Discrepancy: 14.28 CMP GIV 732011 GROUND IDLE, ENG-TEST/ADJUST Resolution: Parts USD: No Charge N/ C Discrepancy.: 14.29 CM!) 7321113 APPROACH IDLE, ENG•TEST/ADJ Resolution: Discrepancy: 14.30 CMP GIV 783013 Thrust Reverser Interlock Feedback System (Left) - Operational Test Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 38 of 57 Printed: 4/18/2013 11:38:5IA) Rd X EFTA01115030 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 14.31 CMP GIV 783014 Thrust Reverser Interlock Feedback System (Right) - Operational Test Resolution: Discrepancy: 14.32 CMP GIV 783017 MAX REV THRUST, L-OPS TEST/ADJ Resolution: Paris USD: No Charge N/ C Discrepancy: 14.33 CMP GIV 783018 MAX REV THRUST, R-OPS TEST/ADJ Resolution: Discrepancy: 14.34 CMP GIV 791033 Oil Level - Check / Service Resolution: Discrepancy: 14.35 CMP GIV 711010 Cowl Latch, Engine (Right) - Rigging Resolution: Complied with CMP GIV 711010 Cowl Latch, Engine (Right) - Rigging. No defects noted IAW GIV AMM 71.02.00. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.65 @ $118.00 $312.70 Total USD: $312.70 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WodcOrderPreliminarylnvoice.rpt Page 39 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115031 Bill To: JEGE,INC. WO 8: SC13175 Invoice Number: Discrepancy: 14.36 CMP GIV 732002 Engine Acceleration Test / Adjustment Resolution: Discrepancy: 14.37 CMP GIV 732006 Engine Deceleration Test / Adjustment Resolution: Discrepancy: 14.38 CMP GIV 732050 ENG HANDLE ACU SOLENOID CK Resolution: Discrepancy: 14.39 CMP GIV 732058 SOLENOID, ENG AI'PR IDLE-OPS Resolution: Discrepancy: 14.40 CMP GIV 750006 AIRFLOW CONT SYS -TEST Resolution: Discrepancy: 14.41 CMP GIV 732012 GROUND IDLE, ENG-TEST/ADJUST Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 40 of 57 Printed: 4/18/2013 11:38:5 IA) Ftst X EFTA01115032 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 14.42 CMP GIV 732014 APPROACH IDLE, ENG-TEST/ADJ Resolution: Discrepancy: 14.43 CMP GIV 791034 Oil Level - Check / Service Resolution: Item: 15 Customer Supplied Due List Team Manager: Sean Brown Pan/Model 0: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 15.1 Comply with Customer Supplied Due List Resolution: Billing Method flours Rate Total Labor USD: Flat Rate $39,560.00 Pans USD: Time and Material $268.20 Total USD: $39,828.20 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.1 #2 PRI440 -B-2 SEALANT, PRC, CARTRIDGE 6oz 3 $26.82 $80.46 15.1 #3 PRI440 -B-2 SEALANT, PRC, CARTRIDGE 6oz 2 $26.82 $53.64 15.1 #4 PR1440-8-2 SEALANT, PRC, CARTRIDGE 6oz 4 $26.82 $107.28 15.1 #5 PR1440-8-112 SEALANT, PRC,CARTRIDGE 1 $26.82 $26.82 Discrepancy: 15.2 CMP GIV 100310 Check Airworthiness Directives Resolution: Complied with Airworthiness Directives check as required. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 41 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115033 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 15.3 CMP GIV 100320 AIRWORTHINESS CHECK Resolution: COMPLIED WITH CMP GIV 100320 AIRWORTHINESS CHECK as required. Discrepancy: 15.4 CMP GIV 191108 Review Aircraft Status and Records Resolution: Complied with Aircraft Status and Records Review as required. Discrepancy: 15.5 CMP GIV 231001 AVIONICS--FUNC RAMP TEST Resolution: COMPLIED WITH CMP GIV 231001 AVIONICS--FUNC RAMP TEST with discrepancies noted at this time. See items in section 6 for discrepancies. All work performed LAW G-IV maintenance manual 34-00.00. Labor USD: No Charge N/ C Discrepancy: 15.6 CMP GIV 251114 Pilot and Copilot Seat - Inspection / Lubrication Resolution: COMPLIED WITH CMP GIV 251114 Pilot and Copilot Seat - Inspection / Lubrication. No defects noted. Ref: GIV AMM 25-11-00. Labor USD: No Charge N/ C Discrepancy: 15.7 CMP GIV 262045 Fire Bottle (Left Engine) - Hydrostatic Test Resolution: Billing Method Hours Rate Total Labor USD: No Charge N/ C Services USD: Time and Material $773.84 Total USD: $773.84 Services: Ref. No. Description Quantity Sell Price USD Extended USD 15.7 #1 HYDROSTATIC TEST 1.00 $773.84 $773.84 Pan Ref: 32700022 FIRE BOTTLE, ENGINE - WITHOUT CARTRIGE (HALON 1301) For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryinvoicesm Page 42 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115034 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 15.8 CMP GIV 262050 Fire Bottle (Right Engine) - Hydrostatic Test Resolution: Billing Method Hours Rate Total Services USD: Time and Material $773.84 Total USD: $773.84 Services: Ref. No. Description Quantity Sell Price USD Extended USD 15.8 #1 HYDROSTATIC TEST 1.00 $773.84 $773.84 Part Ref: 32700022 FIRE BOTTLE, ENGINE - WITHOUT CARTRIGE (HALON 1301) Step: 15.8.1 Completed Entered in Error. Step moved to item 15.9.1. Discrepancy: 15.9 CMP GIV 270101 Stall Barrier / Angle of Attack System - Ops Test Resolution: COMPLIED WITH CMP GIV 270101 Stall Barrier / Angle of Attack System - Ops Test with no discrepancies noted at this time. All work performed JAW G-IV maintenance manual 27.01.01. Labor USD: No Charge N/ C Step: 15.9.1 Completed Complied with CMP 270101 Stall Barrier/AOA System - Operational check Steps B(l) that B(23) with no discrepancies noted at this time. All work performed IAW G-IV maintenance manual 27.01.01. Discrepancy: 15.10 CMP GIV 272038 Rudder Pedals - Lubrication Resolution: COMPLIED WITH CMP GIV 272038 Rudder Pedals - Lubrication. No defects noted. Ref: GIV AMM 27.03.00. Labor USD: No Charge N/ C Discrepancy: 15.11 CMP GIV 275009 Flap Actuator Yoke (Left Inboard) - Inspection Resolution: COMPLIED WITH CMP GIV 275009 Flap Actuator Yoke (Left Inboard) - Inspection. No defect noted at this time. Work IAW GIV MM 27.06.00. Labor USD: No Charge N/C Pans USD: No Charge N/C For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryinvoicespt Page 43 of 57 Printed: 4/18/2013 11:38:5IM. Rd X EFTA01115035 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 15.12 CMP GIV 275010 Flap Actuator Yoke (Right Inboard) - Inspection Resolution: COMPLIED WITH CMP GIV 275010 Flap Actuator Yoke (Right Inboard) - Inspection. No defect noted at this time. Work IAW GIV MM 27-06-00. Labor USD: No Charge N/C Pans USD: No Charge N/C Discrepancy: 15.13 CMP GIV 275011 Flap Actuator Yoke (Left Outboard) - Inspection Resolution: COMPLIED WITH CMP GIV 275011 Flap Actuator Yoke (Left Outboard) - Inspection. No defect noted at this time. Work IAW GIV MM 27-06-00. Billing Method Hours Rate Total Pans USD: Time and Material $57.60 Total USD: $57.60 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.13 82 ADLFS-4005 BUSHING I $57.60 $57.60 Discrepancy: 15.14 CMP GIV 275012 Flap Actuator Yoke (Right Outboard) - Inspection Resolution: COMPLIED WITH CMP GIV 275012 Flap Actuator Yoke (Right Outboard) - Inspection. No defect noted at this time. Work IAW GIV MM 27.06.00. Labor USD: No Charge N/C Pans USD: No Charge N/C Discrepancy: 15.15 CMP GIV 275027 Flap Actuator Bushing (Left) - Service / Lubrication Resolution: Discrepancy: 15.16 CMP GIV 275028 Flap Acuator Bushing (Right) - Service / Lubrication Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 44 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115036 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 15.17 CMP GIV 280005 Fuel Control System - Functional Test Resolution: Discrepancy: 15.18 CMP GIV 303005 Pitot Heat System - Operational Test Resolution: COMPLIED WITH CMP GIV 303005 Pitot Heat System - Operational Test with no discrepancies noted at this time. All work performed IAW G-IV maintenance manual 30-03-00. Labor USD: No Charge N/ C Discrepancy: 15.19 CMP GIV 531007 FS 85 Bulkhead - Inspection Resolution: COMPLIED WITH CMP GIV 531007 FS 85 Bulkhead - Inspection.No defects noted. All work accomplished IAW GIV AMM 53-12-00. Billing Method Hours Rate Total Labor USD: No Charge N/ C Pans USD: Time and Material $6.84 Total USD: $6.84 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 15.19 NI RTV732-3OZ.CLR SEALANT, CLEAR I $6.84 $6.84 Step: 15.19.1 Completed Complied with steps B(1) thru B(I) of CMP GIV 531007 Instructions. No defects noted. All work accomplished IAW GIV AMM 53-12-00. Discrepancy: 15.20 CMP GIV 532007 Forward Cabin Compartment Below Floor - Inspection Resolution: COMPLIED WITH CMP GIV 532007 Forward Cabin Compartment Below Floor - Inspection with no defects noted. All work perfeormed IAW. G-IV MM. 53.20.00. Billing Method Hours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $162.66 Total USD: $162.66 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryinvoicespt Page 45 of 57 Printed: 4/18/2013 11:38:5 IA) Flee X EFTA01115037 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.20 NI D9100 TAPE, 3 INCH FLAME RETARDANT 1 $162.66 $162.66 Discrepancy: 15.21 CMP GIV 532009 Midcabin Compartment Below Floor - Inspection Resolution: COMPLIED WITH CMP GIV 532009 Midcabin Compartment Below Floor - Inspection with no defects noted. All work performed IAW. G-IV MM. 53-30-00 Labor USD: No Charge N/ C Discrepancy: 15.22 CMP GIV 532011 Aft Cabin Compartment Below Floor - Inspection Resolution: COMPLIED WITH CMP GIV 532011 Aft Cabin Compartment Below Floor - Inspection w ith no defects noted. .‘11 work performed IAW. G-IV MM. 53.50.00. Labor USD: No Charge N/ C Discrepancy: 15.23 CMP GIV 551019 Horizontal Stabilizer / Elevator (Exterior) {Left} - Inspection Resolution: COMPLIED WITH CMP GIV 551019 Horizontal Stabilizer / Elevator (Exterior) (Left) - Inspection. IAW GIV AMM 55-14-00. No defects noted at this time. Labor USD: No Charge N/ C Step: 15.23.1 Completed Removed all L/H horizontal stabilizer panels required for CNIP 551019. All work LA. W. GIV M/6155.14-00. Step: 15.23.2 Completed C/W section B thru B(h) of CMP 551019. No discrepancies noted at this time. All work I.A.W. GIV M/M 55-14.00. Discrepancy: 15.24 CMP GIV 551020 Horiz Stabilizer / Elevator (Exterior) {Right} - Insp Resolution: COMPLIED WITH CMP GIV 551020 Horiz Stabilizer / Elevator (Exterior) {Right) - Insp. No discrepancies noted at time. All work I.A.W. GIV M/M 55.00.00. Labor USD: No Charge N/ C Step: 15.24.1 Completed Removed all R/H horizontal stabilizer panels required for CMP 551020. AU work I.A.W. GIV M/M 55-14-00. Step: 15.24.2 Completed (:/W section B thru B(h) of CMP 551020. No discrepancies noted. AU work I.A.W. MAI 55.00.011 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WoikOrderPreliminarylnvoice.rpt Page 46 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115038 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 15.25 CMP GIV 551023 Horizontal Stabilizer / Elevator (Interior / Exterior) (Left) - Inspection Resolution: COMPLIED WITH CMP GIV 551023 Horizontal Stabilizer / Elevator (Interior / Exterior) (Left) - Inspection. See sqk 8.23 and 8.20 for discrepancies noted. All work I.A.W. GIV M/M 55.14.00. Labor USD: No Charge N/ C Step: 15.25.1 Completed Removed all L/H horizontal stabilizer and elevator panels required for CMP 551023. All work I.A.W. GIV M/M 55.14.00. Step: 15.25.2 Completed (:/W section B thru B(k) of CMP 551023. See sqk 8.23 and8.20 for discrepancies noted. All work I.A.W. GIV M/M 55-14-00. Discrepancy: 15.26 CMP GIV 551024 Hz Stabilizer/Elevator (Interior/Exterior) (Right) - Insp Resolution: COMPLIED WITH CMP GIV 551024 Hz Stabilizer/Elevator (Interior/Exterior) (Right) - Insp. See sqk 8.21 and 8.22 for discrepancies noted. All work I.A.N. GIV M/M 55-00-00. Labor USD: No Charge N/ C Step: 15.26.1 Completed In progress removal of It/11 horizontal stabilizer and elevator panels required for CMP 551023 for details of the panels already removed refer to the open and close section of the R/I log book. All work I.A.W. GIV M/M 55-14-00. Step: 15.26.2 Completed Removed remaining required panels for CMP 551024. C/W section B thru B(k) of CMP 551024. See sqk 8.21 and 8.22 for discrepancies noted. All work I.A.W. GIV hf/M 55.00.00. Discrepancy: 15.27 CMP GIV 553005 Vertical Stabilizer / Rudder (External) - Inspection Resolution: COMPLIED WITH CMP GIV 553005 Vertical Stabilizer / Rudder (External) - Inspection. REF GIV MM 55-30-00, CMP 553005. No defects noted. Labor USD: No Charge N/ C Discrepancy: 15.28 CMP GIV 553007 Vertical Stabilizer / Rudder (Internal) - Inspection Resolution: COMPLIED WITH CMP GIV 553007 Vertical Stabilizer / Rudder (Internal) - Inspection. IAW GIV AMM 55-30-00. No defects noted at this time. Labor USD: No Charge N/ C For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 47 of 57 Printed: 4/18/2013 11:38:5IA) Rd X EFTA01115039 Bill To: JEGE,INC. WO 9: SC13175 Invoice Number: Step: 15.28.1 Completed Removed Vertical Stab zone 109 LH trailing edge panels as per CMP GIV 553007. Continue panel removal to facilitate CMP GIV 553007 Vertical Stabilizer / Rudder (Internal) - Inspection. Step: 15.28.2 Completed Continued removing panels to gain access for inspection. Removed panels 109-LE-2, I09-LH-9, 109-LH-11, 109-1.H10, 109-RB-1, 109-1.H-8, 110-LH-I,110-LH-2, 110-LH-3, 110-LH-4, 110-LH-5, 110-LH-6, 109-LH-7. Work done JAW G1V CMP 553007 & GIV Mal 55-30-00. Step: 15.28.3 Completed Continue with removal of all requiered panels of CMP 553007; And Complied with steps B.(I) thru step B(22).All work done IAN' GIV AMM 53-30-00. Discrepancy: 15.29 CMP GIV 571011 Wing Front Beam Hi-Lite Collars (Left) - Inspection Resolution: COMPLIED WITH CMP GIV 571011 Wing Front Beam Hi-Lite Collars (Left) - Inspection as per GIV MM 57-11-00. Reference squawk 8.26. Labor USD: No Charge N/ C Discrepancy: 15.30 CMP GIV 571012 Wing Front Beam Hi-Lite Collars (Right) - Inspection Resolution: COMPLIED WITH CMP GIV 571012 Wing Front Beam Hi-Lite Collars (Right) - Inspection as per GIV MM 57-11-00. Reference item 8.28 for defect. Labor USD: No Charge N/ C Discrepancy: 15.31 CMP GIV 571025 Wing Tank Interior (Left) - Inspection Resolution: Labor USD: No Charge N/ C Discrepancy: 15.32 CMP GIV 571026 Wing Tank Interior (Right) - Inspection Resolution: Labor USD: No Charge N/ C Step: 15.32.1 Completed Removed R/H wing fuel panels 22-FT-1, 22-FT-2, 22-FT-3, 22-FT-4, 22-Fr-5. Work done IAVVI GIV NI/11 28.11-00. Discrepancy: 15.33 Related CMP Codes Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 48 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115040 Bill To: JEGE,INC. WO ft: SC13175 Invoice Number: Discrepancy: 15.34 CMP GIV 251109 SEAT ASSEMBLY, PILOT Resolution: COMPLIED WITH CMP GIV 251109 SEAT ASSEMBLY, PILOT. Removed pilot seat assy. (PN: 1159SCF213-5, SN: 11217) and installed pilot seat assy. (PN: 1159SCF213-5, SN: 11217). Ref: GIV AMM 25-10-00. Labor USD: No Charge N/ C Discrepancy: 15.35 CMP GIV 251110 SEAT ASSEMBLY, COPILOT Resolution: COMPLIED WITH CMP GIV 251110 SEAT ASSEMBLY, COPILOT. Removed copilot seat assy. (PN: 1159SCF213.6, SN: 10980) and installed copilot seat assy. (PN: 1159SCF213-6, SN: 10980). Ref: GIV AMM 25-10-00. labor USD: No Charge N/ C Discrepancy: 15.36 CMP GIV 262025 Engine Fire Bottle ( Left ) - Remo' / Installation Resolution: labor USD: No Charge N/ C Step: 15.36.1 Completed Removed LAI fire bottle PIN 32700022 SAN 06758C2, squibs removed and stored in parts room. 1/ANt. GIV AMM 26-02-00 Discrepancy: 15.37 CMP GIV 262065 Fire Bottle (Left Engine) - Weight Check Resolution: Discrepancy: 15.38 CMP GIV 262030 Engine Fire Bottle (Right) - Removal / Installation Resolution: Labor USD: No Charge N/ C For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 49 of 57 Printed: 4/18/2013 11:38:51M Rd X EFTA01115041 Bill To: JEGE, INC. WO It: SC13175 Invoice Number: Step: 15.38.1 Completed Removed R/H fire bottle P/N 32700022 S/N 12204C1, squibs removed and stored in parts room. I/A/W GIV AMM 26-02-00 Discrepancy: 15.39 CMP GIV 262070 Fire Bottle (Right Engine) - Weight Check Resolution: Discrepancy: 15.40 CMP GIV 275003 Flap (Left) Resolution: Labor USD: No Charge N/ C Step: 15.40.1 Completed Complied with CMP 275003 LEFT FLAP REMOVAL/ INSTALLATION steps A, B and C as required. Work IAW GIV MM 27-06-00. Step: 15.40.2 Completed Remove 1.H Flap PN 1159C520005-543 SN 1086 Discrepancy: 15.41 CMP GIV 275004 Flap (Right) Resolution: Labor USD: No Charge N/ C Step: 15.41.1 Completed Complied with CMP 275004 RIGHT FLAP REMOVAL/ INSTALLATION steps A, B and C as required. Work IAW GIV Mbl27-06-00. Step: 15.41.2 Completed Remove RH flap PN 1159CS20005-S44 SN 1085 Discrepancy: 15.42 CMP GIV 275005 Inboard Flap Actuator (Left) - Removal / Installation Resolution: Labor USD: No Charge N/ C Step: 15.42.1 Completed Performed CMP code 275005 Remove Inbd Flap Actuator PN 1159SCC2I1-13 SN44-514 steps B-I through B-I0 complete. Discrepancy: 15.43 CMP GIV 275007 Outboard Flap Actuator (Left) - Removal / Installation Resolution: Labor USD: No Charge N/ C For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 50 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115042 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Step: 15.43.1 Completed Performed CMP code 275007 Remove Outbd Flap Actuator PN 1159SCC212-13 5N34-624 steps B-1 through B-I I complete. Discrepancy: 15.44 CMP GIV 275006 Inboard Flap Actuator (Right) - Removal / Installation Resolution: Labor USD: No Charge N/ C Step: 15.44.1 Completed Complied with CMP 275006 Inboard Flap Actuator (Right) - Removal / Installation steps A and B. Work lAW GIV N13127-06-00. Discrepancy: 15.45 CMP GIV 275008 Outboard Flap Actuator (Right) - Removal / Installation Resolution: Labor USD: No Charge N/ C Step: 15.45.1 Completed Complied with CMP 275008 Outboard Flap Actuator (Right) - Removal / Installation steps A and B. Work lAW GIV MM27.06.00. Discrepancy: 15.46 CMP GIV 273003 Elevator Free Play - Inspection Resolution: COMPLIED WITH CMP GIV 273003 Elevator Free Play - Inspection. IAW GIV AMM 27-01-00. No defects noted at this time. Labor USD: No Charge N/ C Discrepancy: 15.47 CMP GIV 231114 HF Communications System No. 1 - Operational Check Resolution: Discrepancy: 15.48 CMP GIV 231117 HF Communication Antenna - Continuity Check (Installed) Resolution: Discrepancy: 15.49 CMP GIV 231155 HF Communication Antenna Assembly - Removal / Installation For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 51 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115043 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Resolution: Discrepancy: 15.50 CMP GIV 231115 HF COMM SYS 82-0PS TEST Resolution: Discrepancy: 15.51 CMP GIV 280018 Fuel Tank (Left) - Leak Check Resolution: Discrepancy: 15.52 CMP GIV 574005 Wing Leading Edge (Left Inboard) - Removal / Installation Resolution: Billing Method Hours Rate Total Labor USD: No Charge N/C Pans USD: Time and Material $347.34 Total USD: $347.34 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.52 #1 M83248/I-226 0 RING PACKING-HT61,1.974 ID 6 $1.61 $9.66 S2L-226 S2D-226 1532 #2 M83248/1-230 0 RING PACKING-HTM,2.474 ID 24 $1.26 $30.24 1532 #3 G(;510C300A GASKET 2 $153.72 $307.44 Step: 15.52.1 Completed Remove LH wing leading edge gap bands. Remove bottom screws from inbd section of leading edge and some of the top screws. Removal is in progerss, leading edge can be removed after all screws are removed. Discrepancy: 15.53 CMP (NV 574011 Wing Leading Edge (Left Center) - Removal / Installation Resolution: Labor USD: No Charge N/ C For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliiiiinaryinvoicespt Page 52 of 57 Printed: 4/18/2013 11:38:5 IA) Rst X EFTA01115044 Bill To: JEGE, INC. WO it: SC13175 Invoice Number: Step: 15.53.1 Completed Remove gap band 2I-LE-4 ansd center section leading edge from aircraft for Inspection 2ILE-5 Discrepancy: 15.54 CMP GIV 574017 Wing Leading Edge (Left Outboard) - Removal / Installation Resolution: Labor USD: No Charge N/ C Step: 15.54.1 Completed Remove gap bands 21-LE-6 and 211.E-8. Remove outboard section leading edge 211.E-7 from wing. Discrepancy: 15.55 CMP GIV 574006 Wing Leading Edge (Right Inboard) - Removal I Installation Resolution: Billing Method Flours Rate Total Labor USD: No Charge N/C Pans USD: Time and Material $134.10 Total USD: $134.10 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.55 #1 PRI440-B-1/2 SEALANT, PRC,CARTRIDGE 2 $26.82 $53.64 15.55 #2 PR1440-B-1/2 SEALANT, PRC,CARTRIDGE I $26.82 $26.82 15.55 #3 PR1440-B-1/2 SEALANT, PRC,CARTRIDGE 2 $26.82 $53.64 Step: 15.55.1 Completed Remove gap bands 22-LE-2 and 22LE-4 and inbd leading edge screws (except for 4 upper screws). Discrepancy: 15.56 CMP GIV 574012 Wing Leading Edge (Right Center) - Removal / Installation Resolution: Labor USD: No Charge N/C Discrepancy: 15.57 CMP GIV 574018 Wing Leading Edge (Right Outboard) - Removal / Installation Resolution: Labor USD: No Charge N/C Discrepancy: 15.58 CMP GIV 280010 Defueling Procedures For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_Work0rderPrelititinaryInvoicespt Page 53 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115045 Bill To: JEGE,INC. WO ft: SC13175 Invoice Number: Resolution: Labor USD: No Charge N/ C Discrepancy: 15.59 CMP GIV 282025 Fuel Pickup Screen (Main Left Wing) - Inspection Resolution: Discrepancy: 15.60 CMP GIV 282026 Fuel Pickup Screen (Alternate Left Wing) - Inspection Resolution: Discrepancy: 15.61 CMP GIV 571003 Wing Fasteners - Cadmium Plating Degradation - Check ( Left ) Resolution: Discrepancy: 15.62 CMP GIV 280019 Fuel Tank (Right) - Leak Check Resolution: Discrepancy: 15.63 CMP GIV 282027 Fuel Pickup Screen (Main Right Wing) - Inspection Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 54 of 57 Printed: 4/18/2013 Rd X EFTA01115046 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 15.64 CMP GIV 282028 Fuel Pickup Screen (Alternate Right Wing) - Inspection Resolution: Item: 16 Pilots for Conditioned Survey Flight (Pre Test Flight) Team Manager: Sean Brown Pan/Model Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,563.8 / 3,963 Discrepancy: 16.1 Two Pilot's for Condition Survey Flight (Must be performed with Item 14. Engine Runs and Borescope) Resolution: Billing Method Hours Rate Total Labor USD: Flat Rate $5,500.00 Total USD: $5,500.00 Discrepancy: 16.2 Perform Preparation for night Test Traveler Resolution: Complied with GIV Preparation For Flight Test IAW QAP 9.2, RS-OCT-0217 Rev. 01 and RSQCT-54 Rev. IS, refer to steps for details. Billing Method Hours Rate Total Labor USD: Time and Material ST 49.62 @ $118.00 $5,855.16 Labor USD: Time and Material OT 0.82 @ $177.00 $145.14 Pans USD: Time and Material $213.28 Total USD: $6,213.58 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 16.2 #1 500B4QT SKYDROL OIL IN QUART CANS 4 $53.32 $213.28 Step: 161.1 Completed Complied with Preparation for Flight Test Traveler section C thru Q IAW Flight Test Traveler Step: 161.2 Completed Complied with most items on the checklist. All work done IAW Traveler Number RS-QCT-0217 Rev. 01. Step: 16.2.3 Completed Complied with open items on hot cockpit checklist. All work done IAW Traveler Number RS-QCT-0217 Rev. 01. Discrepancy: 16.3 Perform bulb sweep For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 55 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115047 Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Resolution: Removed several defective lights bulb's on Cockpit Overhead Panel (COP) P/N OL3335 nsn. Installed new lights bulb's on Cockpit Overhead Panel (COP) PIN 013335 nsn. Op's check good. All work was done JAW Gulfstream GIV AMM 33.10.01. Billing Method Houri. Rate Total Labor USD: Time and Material ST 4.00 @ $118.00 $472.00 Paris USD: Time and Material $51.50 Total USD: $523.50 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 163 #1 01_3335 LAMP 10 $5.15 $51.50 Discrepancy: 16.4 Service AC with 18000 Lbs (1700 Gal) of fuel for test Flight. Resolution: Complied with by Signature. Billing Method Flours Rate Total Labor USD: Time and Material ST 4.00 @ $118.00 $472.00 Total USD: $472.00 Discrepancy: 16.5 Return to service EJM for Evaluation Flight. Resolution: ACTT: 8,563.8 LNDS: 3,963 DATE: April 08, 2013 Completed Preflight Inspection Checklist and other maintenance in accordance with EJM Gulfstream G-IV Continuous Airworthiness Maintenance Program, EJM Maintenance Procedure Manual and 14 CFR 135.411 (a)(2) and is approved for return to service. Randy LaPlace, Sr. Airworthiness Inspector For Gu[(stream West Palm Beach, FL 33406 FAA CRS PB8R624N Billing Method Flours Rate Total Lkor USD: Time and Material ST 0.57 @ $118.00 $67.26 Total USD: $67.26 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 56 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA01115048 Bill To: JEGE, INC. WO ft: SC13175 Invoice Number: Discrepancy: 16.6 Comply with an outbound inspection for test flight. Resolution: Complied with an outbound inspection for test flight with no defects noted at this time. Note: This work order is to remain open with open prebuy inspection items to be worked upon return. Billing Method Hours Rate Total Labor USD: Time and Material ST 0.56 @ S118.00 566.08 Total USD: $66.08 Communications concerning disputed debts, including a check or other instrument tendered as full satisfaction of a debt, must be forwarded to: Gulfstream Aerospace Attn: Credit Manager M/S B•05 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 57 of 57 Printed: 4/18/2013 11:38:5IM. Rd X EFTA01115049