by date← Apr 18, 2013·Apr 18, 2013 →

EFTA01117652

Dataset 9

April 18, 201349 pages14,045 words

https://www.justice.gov/epstein/files/DataSet%209/EFTA01117652.pdf

Extracted Text

Gulfstreant AO CVNAMIC• COMPANY PRELIMINARY INVOICE ParUModel #: GIV AC Serial No./Tail No.: 1085 / N423W Bldg C.—FAX 561-681-9392 - West Palm Beach. Florida 33406 Mail Remittance To: Overnight Remittance To: Wire Remittance To: Gulfstream Aerospace Corporation Gulfstream Aerospace Corporation (Box # 730349) Gulfstream Aerospace Corporation P.O. Box 730349 do JP Morgan Chase Bank. NA JP Morgan Chase Bank. NA Dallas, Texas 75373-0349 ATTN: Dallas National Wholesale Lockbox TXI-0029 Chicago. IL 60670 14800 Frye Road Account No Ft. Worth, TX 76155 Fedwire Routing No. (ABA) S.W.I.F.T. CHASUS33 ACH Credit Routing No. (AB. Invoice Number. 7113001424 Bill To: JEGE, INC. Invoice Date: 4/18/2013 3800 SOUTHERN BLVD Customer ID: BJ388 SUITE 204 P.O. Number: WEST PALM BEACH, Florida 33406 Repair Station: FAA CRS PB8R624N United States In Date: 04/01/2013 Out Date: 04/26/2013 Payment Type: Net 30-Open terms Payment Terms: Title: JEGE, INC. INVOICE SUMMARY FOR WORK ORDER NUMBER: SC13175 Time & Materials Flat Rate Total Labor USD: $7,709.71 $76,680.00 $84,389.71 Pails USD: 83,113.48 $2,846.14 $5,959.62 Services USD: $1,547.68 $0.00 $1,547.68 Detail Subtotal USD: $12,370.87 $79,526.14 $91,897.01 Subtotal USD: $91.897.01 Funds on Deposit USD: $73.460.00 Total USD: $18,437.01 Pre Test Eight 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 otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 1 of 49 Printed: 5/1/2013 4:38:18P) Ref: I: EFTA01117652 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Item: 1 Airframe Gulfstream GIV Scheduled N423Tf Team Manager. Sean Brown ParVModel #: 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: 8567.0 LNDS: 3964 DATE: April 26, 2013 Completed Due List inspection accordance with EJM GIV Continuous Airworthiness Maintenance Program, EJM Maintenance Procedure Manual and 14 CFR 135.411 (a)(2) and is approved for return to service. Authorized RTS Signature Amanda Granacki. Airworthiness Inspector For; Gulfstream West Palm Beach, FL 33406 FAA CRS PB8R624N Billing Method Flours Rate Total Labor USD: Time and Material ST 0.95 @ $115.00 $109.25 Labor USD: Time and Material OT 0.40 @ $173.00 $69.20 Labor USD: Time and Material DT 0.65 @ $230.00 $149.50 Total USD: $327.95 Discrepancy: 1.2 Inbound/Outbound Inspection Resolution: Complied with Inbound / Outbound Inspections. Refer to steps below. Labor USD: No Charge N/ C Step: 1.2.1 Completed Inbound/Preliminary Inspection Step: 1.2.2 Completed Outbound Inspection Discrepancy: 1.3 Preflight Inspection Resolution: N/A 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_WorkOrderPreliminaryInvoice.rpt Page 2 of 49 Printed: 5/1/2013 4:38:18P) Ref: I: EFTA01117653 Bill To: JEGE, INC. WO SC13175 Invoice Number: 7113001424 Discrepancy: 1.4 Comply with Debrief Checklist Resolution: N/A Step: 1.4.1 Completed ArrivaVDebrief 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/Clean Galley Resolution: N/A Discrepancy: 1.8 Arrival/Departure 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_WorkOrderPreliminaryinvoice.rpt Page 3 of 49 Printed: 5/1/2013 4:313:1BPf Ref: I: EFTA01117654 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 1.10 Remove Valuables & Secure. Resolution: N/A Discrepancy: 1.11 Comply with Service Team Manager Checklist Resolution: Complied with as required. 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: Complied with as required. Labor USD: No Charge N/ C Discrepancy: 1.14 Towing (Does not include Hangar Moves/ Resolution: Towed as required for MX. 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_WorkOrderPreliminaryInvoice.rpt Page 4 of 49 Printed: 5/1/2013 4:313:18P) Ref: I: EFTA01117655 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 1.15 Hathlat - 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: N/A --- No Hazmat onboard aircraft at this time. Discrepancy: 1.16 Aircraft Cleaning Resolution: N/A Discrepancy: 1.17 Billable Consumables & Shop Supplies Resolution: Billed for Shop Supplies and Consumables as required for MX. Billing Method Flours Rate Total Parts USD: Flat Rate $2,846.14 Total USD: $2,846.14 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_WorkOrderPreliminaryInvoice.rpt Page 5 of 49 Printed: 5/1/2013 4:313:18P/i Ref: I: EFTA01117656 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 711300/424 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 8. Resolution: N/A Discrepancy: 1.19 Update Weight & Balance Resolution: N/A 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_WorkOrderPreliminaryInvoice.rpt Page 6 of 49 Printed: 5/1/2013 4:313:18P/i Ref: I: EFTA01117657 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 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 GAMPS 4000, paragraph 3.5.1 for paint restrictions to flight control surfaces and RVSM certified aircraft. * Reference GAMPS 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: Na Item: 5 Technical Bulletins (ASC, CB, AD, ACB) Team Manager. Sean Brown Part/Model #: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSNICSO: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 5.1 Comply with AD 2001-26-07, Engine Fire Bottle Elecrical Connections. Resolution: AD 2001-26-07, Engine Fire Bottle Elecrical Connections, was found to be N/A to this aircraft by S/N. No further action is 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_WorkOrderPreliminaryInvoice.rpt Page 7 of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117658 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Item: 6 Avionics Team Manager: Sean Brown Part/Model #: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8.567.0 / 3,964 Discrepancy: 6.1 RH wing emergency light Mop 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 IAW Gulfstream GIV AMM 33-10-01. Discrepancy: 6.5 While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #2 Auto Throttle reports Servo Current Failure. Resolution: C/W CMP-223005 ( L AfT Servo-Functional Check. Could not duplicate or verify discrepancy at this time. All work performed I.A.W. GIV M.M. 2240-00. 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 Mop. Also noted that the upper 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 Mop. Resolution: Removed the existing upper half "E-Batts" switch two bulbs P/N OL 3335, and installed two new bulbs P/N ()L 3335. New bulbs check good. Upper half of the "Radar Stab IRU" switch is not supposed to be illuminated. This switch checks good. No discrepency found with Differential Pressure indication. This work performed IAW GIV AMM 33.00.00. Discrepancy: 6.8 Squawk from flight test - LED light burned out on Rate of Climb / FPM (3 digit from LT) on pressurization controller Resolution: Customer elects no further action. Deferred IAW EJM GIV MEL 21-2 Category D Due 8-24-2013 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_WorkOrderPreliminaryInvoice.rpt Page 8 of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117659 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Step: 6.8.1 Completed Verified Discrepancy. Found lighting to be faulty on controller. PN: 1159SCF407-7. All work done JAW GIV MM 21-02-01 Discrepancy: 6.10 Squawk from flight test - At FL250 with Batteries only, DC volts on ABEX fluctuates 36.9 to 47.9 v Resolution: Duplicate discrepancy. Reference item SC13175.6.9 for corrective action. Step: 6.10.1 Completed Researched discrepancy. Discovered that the maintence crew who ran the aircraft, before test flight, did not see any fluctuations in DC Volts. Also discovered the flight crew had DC voltage indication fluctuation with either Left, Aux. Right, or ESS selected in the EPMP. Further action required on this squawk when maintenance schedule provides Hydraulic can to aircraft and/or outside engine runs If DC Volts fluctuation is duplicated, avionics can compare the DC volts from the Pilots CB panel test ports. Performed this work lAW GIV AMM 24-02-00. Step: 6.10.2 Completed With aircraft outside and APU running, monitored the EPMP DC Volts indication. Did notice a few spikes in DC Volts on EPMP while the multimeter, which was connected to DC volts on Pilots CB Pnl test points, was reading a steady 26 VDC. No fluctuation on mulitimeter connected to DC test points. Performed this work lAW 6400 AMM 24-02-00. Discrepancy: 6.11 Squawk from flight test - RTU 1 there is a cyan line across display on screen - splits screen in half Resolution: Operator requested no further action be taken on this discrepancy. No approval for return to service has been issued for the aircraft, with regard to this discrepancy. Discrepancy: 6.16 Squawk from flight test - aft LAV reading light is loop Resolution: Removed the existing bulb P/N 1308. Installed a new bulb P/N 1308. Aft lay reading light checks good. Performed this work IAW GIV AMM 33.00.00. Step: 6.16.1 Completed Verified discrepancy. Found bulb to be bad and also socket loose. All work done JAW (MV MM 33-02-00 Step: 6.16.2 Completed Removed the existing bulb P/N 1308. Pulled the light socket back into its locking seat. Installed a new bulb P/N 1308. Aft lay reading light checks good. Performed this work JAW G1V AMM 33-00-00. Item: 7 Interior Team Manager: Stan Brown ParVModel VS: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSPVTSO: CSN/CSO: Aircraft Time: 8.567.0 / 3.964 Discrepancy: 71 Squawk from flight test - LH galley aft cutting board does not latch 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_WorkOrderPreliminaryInvoice.rpt Page 9 of 49 Printed: 5/1/2013 4:313:1BP/i Ref: I: EFTA01117660 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Resolution: Removed L/H aft lower galley drawer, Lai aft galley cutting board and aft galley cutting board damaged latch P/N MINI-LATCH, installed new galley cutting board latch P/N MINI-LATCH, re-installed L/H aft galley cutting board and L/H aft galley drawer. All work performed IAW GIV MM 25.20.00. Function check good, No defects noted. Step: 7.2.1 completed Renn.‘ed ;talk) drawer:old galle% latch. ..ill 111/It performed l.kW GIN \I\! 25-20-00. Item: 8 Mechanical Team Manager: Sean Brown Part/Model #: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSNICSO: 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. Discrepancy: 8.2 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. IAW RR EMM 74-21-03. 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 GAS13AN-1-41from around L/H and R/H MLG bays, and installed new seal P/N GASI3AN-1.41I/A/W GIV AMM 20-42-00 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. 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 10 of 49 Printed: 5/1/2013 4:38:18P) Ret: EFTA01117661 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 8.8 RII - Squawk from flight test - Flaps shudder felt when flaps selected to 39 degrees Resolution: RII - Verified discrepancy. Found all four actuators to be out of limits, two bad flap roller bearings and two flap tracks with play in them. REF items 8.29, 8.30, 8.31, 8.32, 8.34, 8.35, 8.44, 8.45, 15.40, 15.41 for all Removal and installations and work performed. Rigged and ran flaps as required. No defects noted IAW GIV MM 27-06-00. Discrepancy: 8.10 RH - Squawk from flight test - on the ground the flaps would intermittenly move from 20 to 39 degrees and 10 to 20 when selected. Resolution: RII - Verified discrepancy. Found all four actuators to be out of limits, two bad flap roller bearings and two flap tracks with play in them. REF items 8.29, 8.30, 8.31, 8.32, 8.34, 8.35, 8.44, 8.45, 15.40, 15.41 for all Removal and installations and work performed. Rigged and ran flaps as required. No defects noted IAW GIV MM 27-06-00. 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: Removed RT 12th stage A and B Servo Controller valve filter P/N: 856504-5 and installed new P/N: 856504-5 filter. IAW GIV AMM 36.01.01. C/W CMP 361008 Bleed Air System RAI Operational Test. Ops and leak check is good. No discrepancies noted at this time. All work I.A.W. GIV NUM 36-00-00. Step: 8.12.1 Completed CAV CMP 361007 Bleed Air System Ulf Operational Test. No discrepancies noted at this time. All work I.A.W. GIV MA! 36-00-041. 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: Removed LT 12th stage A and B Servo Controller valve filter P/N: 856504-5 and installed new P/N: 856504-5 filter. IAW GIV AMM 36.01.01. C/W CMP 361007 Bleed Air System IJH Operational Test. Ops and leak check is good. No discrepancies noted at this time. All work I.A.W. GIV MAI 36-00-00. Step: 8.13.1 Completed CAI/ CMP 361008 Bleed Air System R/11 Operational Test. No discrepancies noted at this time. All work I.A.W. GIV WM 36-00.00. Discrepancy: 8.15 Squawk from flight test - service hydraulic replenisher Resolution: Filled hydraulic replenisher tank with skydroll I/A/W GIV AMM 12.01.05 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_WorkOrderPreliminaryInvoice.rpt Page II of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117662 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 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: RII - Removed APU GTCP36-100, S/N P-465-C, with 6,449.0 TSN from GIV, N423TT, S/N 1085, IAW the GIV MM chapter 49-10-00. Installed repaired loaner APU P/N 3800062-9-1, S/N P-115C, with 7039.0 TSN. Complied with CMP 490001 APU GTCP36-100(G)- Removal/Installation and updated CMP. All maintenance performed IAW GIV AMM 49-10-00. Step: 8.17.1 Completed Removed APU generator Pinl 1159SCAV373-105 S/N 129A0171 VA/W GIV AMM 24.01.01 and sent APU out for repair. Step: 8.17.2 Completed Complied with CMP 490020, Auxiliary Power Unit GTCP36-100(G) Alternator- Removal / Installation. Installed APU Alternator P/N 1159SCAV373-105 S/N 129A0171 IAW GIV AMM 24-01-01. No discrepancies noted. Updated CMP 490020. Discrepancy: 8.19 Squawk from flight test - There is a soft spot in floor board 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. Discrepancy: 8.25 #2 Engine has multiple corroded clamps on forward IB area of engine. Resolution: Removed 12 corroded clamps P/N AS12847 and AS12817 and 5 clamps P/Ns AS12816 and AS12846 and installed 12 NEW clamps P/N AS12847 and AS12817 and 5 clamps P/Ns AS12816 and AS12846 IAW RR TAY611.8 MM 71.00.00. Step: 8.25.1 Completed Removed 12 corroded clamps P/N AS12847 and AS12817 and 5 clamps P/Ns AS12816 and AS12846 and installed 12 NEW clamps P/N AS12847 and AS12817 and 5 clamps P/Ns AS12816 and ASI2846 IAN' RR TAY6I1-8 MM 71.00.00. 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: Cut and removed 6" section with dent from fuel line P/N:1159P42012-022FP6 at RBS255.5 of R/H wing. Spliced in new 6" section of tubing on fuel line P/N:1159P42012-022FP6 at RBS255.5 of R/H wing. All work done IAW DAMPS 2507. Leak check is good. 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_WorkOrderPreliminaryInvoicesm Page 12 of 49 Printed: 5/1/2013 4:38:18P/ Ref: I: EFTA01117663 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Step: 8.28.1 Completed Cut and removed 6" section with dent from fuel line P/N: II59P42012-022FP6 at RBS255.5 of 12/H wing. Spliced in new 6" section of tubing on fuel line P/N:1159P42012-022FP6 at RBS255.5 of R/H wing. All work done lAW GAMPS 2507. Discrepancy: 8.29 RII - While T/S the squawk (8.10) for the flaps moving intermittenly found that the LH outboard flap actuator failed the Bannut End Play check. Endplay is .038in., limit is .0121n. Resolution: RII - Remove LH Outbd Flap Actuator PN 1159SCC201-13 SN 34-624 and installed an overhauled actuator PN 1159SCC212-15, S/N 90-913, as per GIV MM 27-06-00. No defect was noted. REF 15.43 for actual work performed Step: 8.29.1 Completed Remove worn LH actuator PN 11595CC 201-13 SN and installed a overhauld actuator PN 1159SCC201-16 SN as per GIV MM 27-02-00 Discrepancy: 8.30 RII - While T/S the squawk (8.10) for the flaps moving intermittenly found that the LH inboard flap actuator failed the Bannut End Play check. Endplay is .057in., limit is .012in. Resolution: RH - Remove Inbd flap actuator PN 1159SCC211-13 SN 44-514 and installed an overhauled actuator PN 1159SCC211-15 SN 58.1461as per GIV MM 27-06-00. No defect was noted. REF Item 15.42 for actual work performed Step: 8.30.1 Completed Removed worn LH Inbd Actuator PN 1159SCC201- SN and installed overhauled actuator PN 1159SCC201- SN as per GIV MM 2702-00. REF 15.42 for actual work performed Discrepancy: 8.31 RII - 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 .0121n. Resolution: COMPLIED WITH CMP GIV 275008 Outboard Flap Actuator (Right) - Removal / Installation. Removed R/H Outbd Flap Actuator PN 1159SCC212-14, SN 60-257 and installed an overhauled actuator PN 1159SCC212-16 S/N 12-928. Work IAN GIV MM 27.06.00. REF item 15.45 for actual work performed Discrepancy: 8.32 RH - 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: RII - COMPLIED WITH CMP GIV 275006 Inboard Flap Actuator (Right) - Removal / Installation. Removed R/II Inb Flap Actuator PN 1159SCC211-13, SN 60-390 and installed an overhauled actuator PN 1159SCC211.15, SN 91.848. Work JAW GIV MM 27-06-00. REF 15.44 for actual work performed 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 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117664 Bill To: JEGE, INC. WO #: SCI3175 Invoice Number: 7113001424 Discrepancy: 8.34 RII - The RH flap's "C" tracks forward, inboard bearing is bad (1159SCC228-23) Resolution: RII - C/W CMP 275123. Removed worn RAI 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. Updated CMP 275123 Discrepancy: 8.35 RII - The LH flap's "B" tracks AFT, outboard bearing is bad (1159SCC226-7) Resolution: RH - Removed L/11 flap track B outboard roller bearing P/N 1159SCC226-7. Install new L/H flap track B outboard roller bearing P/N 1159SCC426-9 IAW GIV AMM 27-06-00. Updated CMP 275117 Step: 8.35.1 Completed Complied with G1V 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(5)(b). Removed defected flap roller P/N: 1159SCC266-7, S/N: NSN. Work done IAIV GIV CMP 275117 & GIV WM 27.06-00. Discrepancy: 8.36 The LH flap track "A" has corrosion Resolution: Removed light surface corrosion and pitting from I./H flap track "A" . Cad plated exposed surface IAW GIV SRM 51.21.26. Primed and painted. All Work performed JAW GAC drawing SE05811901. Step: 8.36.1 Completed Removed light surface corrosion and pitting from UN flap track "A" IAIV G1V AMM 27.06.00. Step: 8.36.2 Completed Cad plated exposed surface IAW GIV SRM 51-21-26. Discrepancy: 8.44 RII - The LH flap track "B" has play in the fwd attach bolt Resolution: On LH Flap Track "B", Removed Flap Track Attaching Bolt, Nut, And Lug Bushings. Cleaned And Removed Light Surface Corrosion From Inside Track Attaching Holes. Brush Cadmium Plated Bolt Holes In Accordance With Drawing 00-P-416 Type III. Installed New Lug Bushings With Primer (P/N 1159WM20235-3), Installed New Bolt (P/N NAS1312-23, Installed New Nut (P/N MS21083N12) On Flap Track Attaching Holes. All Maintenence Performed Reference To GIV AMM 27-00-00 And Drawing SE05811105. Step: 8.44.1 Completed Removed light surface corrosion and cad plated bolt holes. All work done JAW GIV AMM 27-06-00 and GIV SRM 51-21-26. Discrepancy: 8.45 RII - The RH flap track "B" has play in the fwd attach bolt Resolution: On RH Flap Track "B", Removed Flap Track Attaching Bolt, Nut, And Lug Bushings. Cleaned And Removed Light Surface Corrosion From Inside Track Attaching Holes. Brush Cadmium Plated Bolt Holes In Accordance With Drawing 00-P-416 Type III. Installed New Lug Bushings With Primer (P/N 1159WM20235-3), Installed New Bolt (P/N NAS1312-23, Installed New Nut (P/N MS21083N12) On Flap Track Attaching Holes. All Maintenence Performed Reference To GIV AMM 27-00-00 And Drawing SE05811105. 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_WorkOrderPreliminaryinvoice.rpt Page 14 of 49 Printed: 5/1/2013 4:313:18M Ref: I: EFTA01117665 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Step: 8.45.1 Completed Removed light surface corrosion and cad plated bolt holes. All work done IAW GIV AMM 27.06.00 and GIV SRM 51-21-26. Discrepancy: 8.46 Install prep and seal panels on tail surfaces. See steps for applicable sections. Resolution: Sealed panels 37-UPR-1, 37-UPR-3, 37-UPR-5 and 37-UPR-7 as required. REF GIV MM 27-00-09 Step: 8.46.1 Completed Peeped and sealed panel on vertical stab. Panel edge sealant ready for paint. IAN` GIV AMM 20-00-00 Step: 8.46.2 Completed Sealed panels on the upper vertical on the left and right. Closed lett horiz stab trailing edge panels, taped and ready to seal 37-UPR-1, 37-UPR-3, 37-UPR-5 and 37-UPR-7. REF GIV MM 27-00-00 Discrepancy: 8.47 APU enclosure and apu mount have heavy soot residue Resolution: Cleaned APU enclosure and apu mount as required IAW GIV SRM 51-21-00. Discrepancy: 8.50 R/H lower wing skin has corrosion near panel 22-FT-11 Resolution: Remove corrosion from Rill lower wing skin near panel 22-Fr-11. Prime and paint. Work done IAW GIV SRM 51-13.20. Discrepancy: 8.56 While removing R/H wing fuel panel 22-Pr -1 for sqk 15.32. Found ground mesh on panel to he torn. pn 1159WM40076.13 Resolution: Removed torn mesh gasket PIN 1159WM40076.13 and installed a NEW mesh gasket IVN 1159WM40076-13 as required JAW GIV MM 28.11.110. Discrepancy: 8.57 Squawk from flight test - MED seal was squealing during flight Resolution: Gain access to leak check the MED inflatable seal system from the pressure regulator to the MED seal. System was leak checked and no leaks were found at this time. Purged inflatable door seal system. Complied with main entrance door inflatable seal system ops check. No discrepancies found at this time. Cleaned MED seal and airframe as required. All work performed I.A.W. GIV M.M. 52-00-03. Ops. checks good. Updated CMPs: 521008 and 521080. 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 15 of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117666 Bill To: JEGE, INC. WOO: SC13175 Invoice Number: 7113001424 Discrepancy: 8.58 Refuel aircraft to 5000lbs Resolution: Refuel aircraft to requested 5000lbs in accordance with GIV Partial Refueling Procedures; Maintenance Manual Chapter 28.04.00. Discrepancy: 8.59 During right wing fuel tank leak check Squawk 15.62 found inboard fuel access panel 22-FT-1 missing a screw. Resolution: Installed NEW screw P/N NAS1580V4T10 on panel 22-FT-1 IAW GIV MM 28.11.00. Step: 8.59.1 Completed Ordered fuel panel screw p/n- NAS1580V4T10 per GIV IPC 57-20-00. Ref item # 15.62. Awaiting for part. Discrepancy: 8.60 CMP GIV 571004 Wing Fasteners - Cadmium Plating Degradation - Check (Right) Resolution: COMPLIED WITH CMP GIV 571004 Wing Fasteners - Cadmium Plating Degradation - Check (Right) No defects found. All work performed IAW the GIV MM chapter 57-10-00. Billing Method Flours Rate Total Labor USD: Flat Rate $3,220.00 Total USD: $3,220.00 Discrepancy: 8.61 While repacking cabin 02 masks found R/H forward and middle cabin masks to have the circle clips missing marked affected masks with orange streamers ) 289.601.228 Resolution: Removed Two (2) forward and Two (2) Middle Rai cabin masks P/N: 289.601.228 with not S/N's and replaced with new cabin masks P/N: 289-601-228 with not S/N's; All work done IAW GIV AMM 35-00-00. Discrepancy: 8.62 clean wing rear beams as required Resolution: Cleaned rear beams as required IAW GIV SRM 51-07-10. 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 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117667 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Billing Method flours Rate Total Labor USD: Time and Material ST 2.25 @ $115.00 $258.75 Labor USD: Time and Material OT 1.30 @ $173.00 $224.90 Total USD: $483.65 Discrepancy: 8.65 LH horizontal stab 37-LE-1 panel (INBD L.E.) found deriorated seal. Resolution: Removed Worn Seal From L/H Horizontal Leading Edge InBoard Panel 37-LE-1 and Replaced With New Seal 1'/N 1159CS20258-21. All Maintenence Performed In Reference To GIV AMM 20-00-00. Discrepancy: 8.66 RH horizontal stab 38-LE-1 panel (INBD L.E.) found deriorated seal. Resolution: Removed Worn Seal From R/H Horizontal Leading Edge InBoard Panel 37-LE-1 and Replaced With New Seal P/N 1159CS20258-21. All Maintenence Performed In Reference To G1V AMM 20-00-00. Discrepancy: 8.67 As per CMP 361077 & 361078, Leak and Op's check due of both Lt and Rt 12th Stage Servo Controllers. Panels (29/30-UPR-2) require installation after leak check. Resolution: Complied with CMP 361007 and 361008 Bleed Air System L/14 and R/H Operational Test. Ops and leak check is good. No discrepancies noted at this time. All work I.A.W. GIV M/M 36.00.00. Item: 10 Outstanding Parts, Materials, and / or Services Team Manager: Sean Brown Part/Model #: Customer Coordinator: Ray Kraher AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8.567.0 / 3.964 Discrepancy: 10.1 Service for Signature for LAN' service Resolution: Completed. Services 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_WorkOrderPreliminaryInvoice.rpt Page 17 of 49 Printed: 5/1/2013 4:313:1BP/i Ref: I: EFTA01117668 Bill To: JEGE, INC. WO SC13175 Invoice Number: 7113001424 Discrepancy: 10.2 service for signature to fuel Resolution: Completed. Services USD: No Charge N/ C Discrepancy: 10.3 Service for Alt Resolution: Services USD: No Charge N/ C Services: Ref. No. Description Quantity Sell Price USD Extended USD 103 #1 REPAIR 1.00 $0.00 $0.00 Part Ref: GTCP36-100G APU (3800062-9-1) Discrepancy: 10.4 Service from 8.37 Resolution: Discrepancy: 10.5 8.33 Resolution: Discrepancy: 10.7 Clean aircraft Resolution: Services USD: No Charge N/ C Services: Ref. No. Description Quantity Sell Price USD Extended USD 10.7 #1 SERVICE 1.00 $0.00 $0.00 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_WorkOrderPreliminaryInvoice.rpt Page 18 of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117669 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Item: 12 Aircraft Records and Logbook Research Only Team Manager: Sean Brown Part/Model #: 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 CM 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 GIV 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 on 10/24/06. Resolution: Item was compled with by Duncan Aviation on 10/24/06 under W/O FK8BA. No further action taken. Discrepancy: 123 No log entry or tag was found for APU Fire bottle cartridge P/N AE30903823 S/N AENI-23 installed on August 3, 2005. Resolution: Researched records and found Tag for APU Fire bottle cartridge . No further action taken. Discrepancy: 12.4 No log entry• was found for NLG Axle Assy. P/N 1159LM40544-7 S/N BFG6056NTW installed on June 3, 1999. Resolution: Researched records and found Tag for NLG Axle. No further action taken. 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_WorkOrderPreliminaryInvoice.rpt Page 19 of 49 Printed: 5/1/2013 4:313:18P/i Ref:I: EFTA01117670 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 12.5 No 8130 found for Pilor& Co-pilot side window attach bolts. Replaced on 12/11/98. Resolution: Found 8130 for the Pilot'& Co-pilot side window attach bolts. Replaced on 12/11/98. The parts were installed New. No further action required. Discrepancy: 12.6 No 8130 found for isolator L/H Aft Fwd. S/N 2998 installed on 12/11/98. Resolution: Found 8130 for the L/H Aft Fwd. S/N 2998 installed on 12/11/98. The part was installed New. No further defects taken. Discrepancy: 12.7 No 8130 found for isolator 1./H Aft aft S/N 2982 installed on 12/11/98. Resolution: Found 8130 for the isolator I./H Aft aft S/N 2982 installed on 12/11/98. The part was installed New. No further defects noted. Discrepancy: 12.8 No 8130 found for isolator Rill Aft Fwd. S/N 2993 installed on 12/11/98. Resolution: Found 8130 for isolator R/H Aft Fwd. S/N 2993 installed on 12/11/98.The part was installed New. No further action taken. Discrepancy: 12.9 No 8130 found for isolator R/H Aft Aft. S/N 2994 installed on 12/11/98. Resolution: Found 8130 for isolator R/H Aft Aft. S/N 2994 installed on 12/11/98. The part was installed New. No further action taken. Discrepancy: 12.10 No 8130 or log entry found for nose wheel steering installed on 10/11/06. Resolution: The same steering unit PN. 1159SCL200-43 SN.1003 was only removed and installed for a corrosion inspection on 10-11-06 and no maintenance was performed on steering unit. No 8130 is required. No further action taken at this time. 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 20 of 49 Printed: 5/1/2013 4:313:18P/i Ref: I: EFTA01117671 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 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: This item is not due at this time. No further action taken. Item: 13 APU Borescope Team Manager: Sean Brown Part/Model Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 13.1 Comply with APU GTCP36-100(G) - Borescope Resolution: Complied with APU GTCP36.100(G) Borescope Inspection IAW 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 RII - Comply with CMP GIV 490001 APU GTCP36-100(G) - Removal / Installation Resolution: RII - Removed APU GTCP36-100, S/N P-465-C, with 6,449.0 TSN from GIV, N423TT, S/N 1085, IAW the GIV MM chapter 49-10-00. Installed repaired loaner APU P/N 3800062-9-1, S/N P-115C, with 7039.0 TSN. Complied with CMP 490001 APU GTCP36-100(G)- Removal/Installation and updated CMP. All maintenance performed IAW GIV AMM 49-10-00. Updated CMP 499010. Labor USD: No Charge N/ C Step: 13.2.1 Completed Removed APU Per CMP 490001 From A, B 1-14 a-I. All Maintenence Performed In Reference To GIV AMM 49-10-00. Step: 13.2.2 Completed Complied with CMP 490001 APU GTCP36-100(G) - Removal / Installation steps C-la thru C-Ig. AU work done JAW GIV M.M Ch.49-10-00. A.F410108 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_WorkOrderPreliminaryInvoice.rpt Page 21 of 49 Printed: 5/1/2013 4:313:18PF Ref: I: EFTA01117672 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 13.3 Comply with CMP GIV 490005 APU Enclosure GTCP36-100(G) - Inspection Resolution: Complied with CMP GIV 490005 APU Enclosure GTCP36-100(G) - Inspection. No discrepancies noted. Inspection performed IAW GIV AMM 49.00.00. Discrepancy: 13.4 Comply with CMP GIV 490002 APU GTCP36-100(G) - Ops Test Resolution: Complied with CMP GIV 490002 APU GTCP36-100(G) - Ops Test IAW GIV MM 49-10-00. No defects noted Item: 14 Engine Runs and Borescope Team Manager: Sean Brown Part/Model #: Customer Coordinator: Ray Kraher AC Serial No./Tail No.: TSN/TSO: CSNICSO: Aircraft Time: 8.567.0 / 3.964 Discrepancy: 14.1 Comply with Engine Runs and Borescope Resolution: Complied with Engine Runs and Borescope CMP's as required. Refer to items 14.2 through 14.21 helm% for maintenance performed. 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 Resolution: cm 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: 14.3 CMP GIV 710025 Engine Borescope - Inspection Resolution: COMPLIED WITH CMP GIV 710025 Engine Borescope - Inspection IAW RR TAY EMM 71-00-00. 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_WorkOrderPreliminaryInvoicespt Page 22 of 49 Printed: 5/1/2013 4:313:18P) Ref: I: EFTA01117673 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Billing Method Hours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $332.33 Total USD: $332.33 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 143 #1 A543013-210 OR1NG 1 $17.72 $17.72 143#2 A543013-348 OR1NG 2 $59.74 $119.48 143 #3 KB22748 O-RING 1 $10.51 $10.51 14.3 #4 PL32M SEALANT 2 $92.31 $184.62 Step: 143.1 Completed Gained access for Borescope. LAW CMP 710025 paragraph (B) 1-10 Step: 143.2 Completed Complied with CMP 710025 front step (11)(a) through step (51)(c) JAW the rolls Royce TAY611-8 mm chapter 71.00.00. See squawk 8.3 Step: 143.3 Completed Complied with CMP 710025 paragraph 53, (A)-(E) 1-7, 57.58 (A)-(E). Note could not install other access plugs do to having to order Hylomar. Step: 143.4 Completed Left #2 ENG open being that had to order Hylomar 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- EMM Chapter 71.00-W. Discrepancy: 14.4 CMP GIV 710031 Engine - Operational Test Resolution: COMPLIED WITH CMP GIV 710031 Engine - Operational Test during flight test ground runs. No defects noted IASI" RR71.00.00 Labor USD: No Charge NI C Discrepancy: 14.5 CMP GIV 730001 Fuel Contamination Check (Engine) - Inspection Resolution: OW CMP GIV 730001 Fuel Contamination Check (Engine) - Inspection UMW RR Tay 611.8 EMM 73-11-03. No defects noted 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. 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 23 of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117674 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 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 S/N 1204. Instaled new engine #1 ignitor plug #2 P/N Y183-5 S/N 12047184. IAW RR EMM 74-2143. 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 I/A/W RR Tay 6-11 EMM 77-33-01 No defects noted Billing Method Flours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $176.00 Total USD: $176.00 Pans: Ref. No. Pan 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 Billing Method Flours Rate Total Labor USD: No Charge N/ C Pans USD: Time and Material $33.25 Total USD: $33.25 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 14.10 #3 1159CGSK792007 L/ENG.OIL FILTER - R&I / 1000-3999 1 $33.25 $33.25 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_WorkOrderPreliminaryInvoice.rpt Page 24 of 49 Printed: 5/1/2013 4:38:18PF Ref: I: EFTA01117675 Bill To: JEGE, INC. WO #: SCI3175 Invoice Number: 7113001424 Discrepancy: 14.11 CMP GIV 792013 Engine Scavenge Strainers - Inspection Resolution: C/VV CMP GIV 792013 Engine Scavenge Strainers - Inspection 1/A/W RR Tay 611.8 EMM 72-01-01 No defects noted Billing Method Flours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $195.60 Total USD: $195.61) Parts: Ref. No. Pan number: Description S Sell price USD Extended USD 14.11 #2 KB22722 O-RING $8.40 $8.40 14.11 #3 KB22726 SEAL $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 $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 Parts USD: Time and Material $147.71 Total USD: $147.71 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 14.13 #1 AS43013-210 ORING 1 $17.72 $17.72 14.13 #2 AS43013-348 (UNG $59.74 $119.48 14.13 #3 KB22748 O-RING 1 $10.51 $10.51 Step: 14.13.1 Completed Gained access for Borescope. 'ASV CMP 710025 paragraph (B) 1-10 Step: 14.13.2 Completed Complied with CMP 710026 from step (11)(a) through step (51)(c) IAW the rolls Royce TAY611-8 mm chapter 71.00.00. See squawk 8.4. Step: 14.13.3 Completed Install all inner and outer engine panels and bore scope plugs IAW Rolls Royce TAY- EMM Chapter 71-00-00. 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_WorkOrderPreliminaryInvoice.rpt Page 25 of 49 Printed: 5/1/2013 4:38:18PF Ref: I: EFTA01117676 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 14.14 CMP GIV 710032 Engine - Operational Test Resolution: COMPLIED WITH CMP GIV 710032 Engine - Operational Test during flight test ground runs. No defects noted IAW RR71.00.00 Discrepancy: 14.15 CMP GIV 730002 Fuel Contamination Check (Engine) - Inspection Resolution: COMPLIED WITH CMP GIV 731)002 Fuel Contamination Check (Engine) - Inspection. No defects noted JAW 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 SIN 12047194. IAW RR EMM 74-21-03. Discrepancy: 14.18 CMP GIV 742018 No. 2 Igniter Plug - Inspection 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 IAW RR TAY 611.8 MM 77-33-01. 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 26 of 49 Printed: 5/1/2013 4:313:18P/i Ref: I: EFTA01117677 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Billing Method Flours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $176.00 Total USD: $176.00 Pans: 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 Flours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $31.25 Total USD: $31.25 Pans: Ref. No. Pan 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 7241-01. Billing Method Hours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $195.60 Total USD: $195.60 Pans: Ref. No. Part number: Description Quantity Sell in ice USD Extended USD 14.21 #2 KB22722 0 -RING 1 $8.40 $8.40 14.21 #3 KB22726 SEAL 1 $8.03 $8.03 14.21 #4 KB22727 0 -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 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 49 Printed: 5/1/2013 4:313:15P/i Ref: I: EFTA01117678 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 14.22 Related CUP Codes Resolution: Complied with related CMP codes as required. Refer to items 14.22 through 14.43 below for maintenance performed. Discrepancy: 14.23 CMP GIV 711009 Cowl Latch, Engine (Left) - Rigging Resolution: CNV CMP GIV 711009 Cowl Latch, Engine (Left) - Rigging GIV AMM 71-02-00 No defects noted Labor USD: No Charge N/ C Discrepancy: 14.24 CMP GIV 732001 Engine Acceleration Test / Adjustment Resolution: Complied with CMP GIV 732001 Engine Acceleration Test / Adjustment during flight test ground runs. No defects noted IAW RR71.00.00 Step: 14.24.1 Completed Removed all R/H horizontal stabilizer panels required for CMP 551020. All work I.A.W. GIV MA1 55-14-00. Discrepancy: 14.25 CMP GIV 732005 Engine Deceleration Test / Adjustment Resolution: Complied with CMP GIV 732005 Engine Acceleration Test / Adjustment during flight test ground runs. No defects noted JAW RR71.00.00 Parts USD: No Charge N/ C Discrepancy: 14.26 CMP GIV 732049 ENG HANDLE ACU SOLENOID CK Resolution: COMPLIED WITH CMP GIV 732049 ENG HANDLE ACU SOLENOID CK during flight test ground runs. No defects noted IAW RR71.00-00 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_WorkOrderPreliminaryInvoicespt Page 28 of 49 Printed: 5/1/2013 4:313:1BP/i Ref: I: EFTA01117679 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 71/3001424 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/I log book . All work LA.W. GIV MA! 55.14.00. Discrepancy: 14.27 CMP GIV 732057 SOLENOID, ENG APPR IDLE-OPS Resolution: COMPLIED WITH CMP GIV 732057 SOLENOID, ENG APPR IDLE-OPS during flight test ground runs. No defects noted IAW RR71.00-00 Discrepancy: 14.28 CMP GIV 732011 GROUND IDLE, ENG-TEST/ADJUST Resolution: COMPLIED WITH CMP GIV 732011 GROUND IDLE, ENG-TEST/ADJUST during flight test ground runs. No defects noted IAW RR71.00.00 Parts USD: No Charge N/ C Discrepancy: 14.29 CMP GIV 732013 APPROACH IDLE, ENG-TEST/ADJ Resolution: COMPLIED WITH CMP GIV 732013 APPROACH IDLE, ENG-TEST/ADJ during flight test ground runs. No defects noted IAW RR71.00.00 Discrepancy: 14.30 CMP GIV 783013 Thrust Reverser Interlock Feedback System (Left) - Operational Test Resolution: COMPLIED WITH CMP GIV 783013 Thrust Reverser Interlock Feedback System (Left) - Operational Test during flight test ground runs. No defects noted IAW RR71-00.00 Discrepancy: 14.31 CMP GIV 783014 Thrust Reverser Interlock Feedback System (Right) - Operational Test Resolution: COMPLIED WITH CMP GIV 783014 Thrust Reverser Interlock Feedback System (Right) - Operational Test during flight test ground runs. No defects noted IAW RR71.00.00 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_WorkOrderPreliminaryInvoice.rpt Page 29 of 49 Printed: 5/1/2013 4:313:18P) Ref: I: EFTA01117680 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 14.32 CMP GIV 783017 MAX REV THRUST, L-OPS TEST/ADJ Resolution: COMPLIED WITH CMP GIV 783017 MAX REV THRUST, L-OPS TEST/ADJ during flight test ground runs. No defects noted IAW RR71-00-00 Parts USD: No Charge N/ C Discrepancy: 14.33 CMP GIV 783018 MAX REV THRUST, R-OPS TEST/ADJ Resolution: COMPLIED WITH CUP GIV 783018 MAX REV THRUST, R-OPS TEST/ADJ during flight test ground runs. No defects noted IAW RR71-00-00 Discrepancy: 14.34 CMP GIV 791033 Oil Level - Check / Service Resolution: COMPLIED WITH CMP GIV 791033 Oil Level - Check / Service IAW RR TAY 611.8 EMM 5-10-00 and GIV MN1 79-01-00. Labor USD: No Charge N/ C Discrepancy: 14.35 CMP GIV 711010 Cowl Latch, Engine (Right) - Rigging Resolution: Complied with CMP GIV 711010 Cowl Latch, Engine (Right I - Rigging. No defects noted IAW GIV AMM 71.02.00. Labor USD: No Charge NI C Discrepancy: 1436 CMP GIV 732002 Engine Acceleration Test / Adjustment Resolution: COMPLIED WITH CMP GIV 732002 Engine Acceleration Test / Adjustment during flight test ground runs. No defects noted IAW RR71.00.00 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_WorkOrderPreliminaryInvoicespt Page 30 of 49 Printed: 5/1/2013 4:313:18P) Ref: I: EFTA01117681 Bill To: JEGE, INC. WO SC13175 Invoice Number: 7113001424 Discrepancy: 14.37 CMP GIV 732006 Engine Deceleration Test / Adjustment Resolution: COMPLIED WITH CMP GIV 732006 Engine Deceleration Test / Adjustment during flight test ground runs. No defects noted IAW RR71.00.00 Discrepancy: 14.38 CMP GIV 732050 ENG HANDLE ACU SOLENOID CK Resolution: COMPLIED WITH CMP GIV 732050 ENG HANDLE ACU SOLENOID CK during flight test ground runs. No defects noted IAW RR71.00-00 Discrepancy: 14.39 CMP GIV 732058 SOLENOID, ENG APPR IDLE-OPS Resolution: COMPLIED WITH CMP GIV 732058 SOLENOID, ENG APPR IDLE-OPS during flight test ground runs. No defects noted IAW RR71.00-00 Discrepancy: 14.40 CMP GIV 750006 AIRFLOW CONT SYS -TEST Resolution: COMPLIED WITH CMP GIV 750006 AIRFLOW CONT SYS -TEST during flight test ground runs. No defects noted IAW RR71-00-00 Discrepancy: 14.41 CMP GIV 732012 GROUND IDLE, ENG-TEST/ADJUST Resolution: COMPLIED WITH CMP GIV 732012 GROUND IDLE, ENG-TEST/ADJUST during flight test ground runs. No defects noted IAW RR71-00-00 Discrepancy: 14.42 CMP GIV 732014 APPROACH IDLE, ENG-TEST/ADJ 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 31 of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117682 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Resolution: COMPLIED WITH CMP GIV 732014 APPROACH IDLE, ENG-TEST/ADJ during flight test ground runs. No defects noted IAW RR71.00.00 Discrepancy: 14.43 CMP GIV 791034 Oil Level - Check / Service Resolution: COMPLIED WITH CMP GIV 791034 Oil Level - Check / Service IAW RR TAY 611.8 EMM 5-10-00 and GIV MM 79-01-00. Labor USD: No Charge NI C Item: 15 Customer Supplied Due List Team Manager: Sean Brown ParVModel #: 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: Complied with Customer Supplied Due List CMp's as required. Refer to items 15.2 through 15.32 below for maintenance performed. Billing Method Flours Rate Total Labor USD: Flat Rate $39,560.00 Parts USD: Time and Material $800.04 Total USD: $40,360.04 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.1 #2 PR1440-B-2 SEALANT, PRC, CARTRIDGE 6oz 3 $26.82 $80.46 15.1 #3 PR1440-B-2 SEALANT, PRC, CARTRIDGE 6oz 2 $26.82 $53.64 15.1 #4 PR1440-B-2 SEALANT, PRC, CARTRIDGE 6oz 4 $26.82 $107.28 15.1 #5 PR1440-B-1/2 SEALANT, PRC,CARTRIDGE I $26.82 $26.82 15.1 #6 05%620470-27 COVER I $120.30 $120.30 15.1 #7 1159SB20470-53 RETAINER ASSEMBLY I $218.08 $218.08 15.1 #8 PR1440-B-1/2 SEALANT, PRC,CARTRIDGE 1 26.82 $20 83 $26.82 15.1 #9 OIL2380 JET OIL 2380 EXXON 8 $166.64 Step: 15.1.1 Completed Installed NEW cover as required and painted. Need to be sealed. Work IAW GIV MM 20-00-00. 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_WorkOrderPreliminaryinvoicespt Page 32 of 49 Printed: 5/1/2013 4:38:18P/ Ref: I: EFTA01117683 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 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 IAW G-IV maintenance manual 3440.00. 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: GIN' AMM 25-11.00. Labor USD: No Charge N/ C Discrepancy: 15.7 CMP GIV 262045 Fire Bottle (Left Engine) - Hydrostatic Test Resolution: COMPLIED WITH CMP GIV 262045 Fire Bottle (Left Engine) - Hydrostatic Test. Hydo test of bottle P/N 32700022, S/N 06758C2 performed by Ameron Global Product Support w.o.# 276974 on 4/17/13. Next Hydro due 4/2018 Billing Method flours Rate Total 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 49 Printed: 5/1/2013 4:313:1BP/i Ref: I: EFTA01117684 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 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 Part Ret: 32700022 FIRE BOTTLE, ENGINE - WITHOUT CARTRIGE (HALON 1301) Discrepancy: 15.8 CMP GIV 262050 Fire Bottle (Right Engine) - Hydrostatic Test Resolution: COMPLIED WITH CMP GIV 262050 Fire Bottle (Right Engine) - Hydrostatic Test. Hydo test of bottle P/N 32700022, S/N 12204C1 performed by Ameron Global Product Support w.o.# 276973 on 4/17/13. Next Hydro due 4/2018 Billing Method Flours Rate Towl 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 IAW G-IV maintenance manual 27.01.01. Labor USD: No Charge N/ C Step: 15.9.1 Completed Complied with CMP 270101 Stall Barrier/AGA System - Operational check Steps B(1) thru B(23) with no discrepancies noted at this time. All work performed IAN` G-IV maintenance manual 27.01.01. Discrepancy: 15.10 CMP GIV 272038 Rudder Pedals - Lubrication Resolution: COMPLIED WITH CHIP GIV 272038 Rudder Pedals - Lubrication. No defects noted. Ref: GIV AMM 27-03-00. Labor USD: No Charge N/ C Discrepancy: 15.11 RII - CMP GIV 275009 Flap Actuator Yoke (Left Inboard) - Inspection Resolution: RII - COMPLIED WITH CMP GIV 275009 Flap Actuator Yoke (Left Inboard) - Inspection. No defect noted at this time. Work IAW GIV MM 27-06-00. 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_WorkOrderPreliminaryInvoice.rpt Page 34 of 49 Printed: 5/1/2013 4:38:18PF Ref: I: EFTA01117685 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Labor USD: No Charge N/C Parts USD: No Charge N/C Discrepancy: 15.12 RII - CMP GIV 275010 Flap Actuator Yoke (Right Inboard) - Inspection Resolution: RII - 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 Parts USD: No Charge N/ C Discrepancy: 15.13 RII - CMP GIV 275011 Flap Actuator Yoke (Left Outboard) - Inspection Resolution: RII - 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 Noun Rate Total Parts USD: Time and Material $57.60 Total USD: $57.60 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 15.13 #2 ADLF8-4005 BUSHING 1 $57.60 $57.60 Discrepancy: 15.14 RII - CMP GIV 275012 Flap Actuator Yoke (Right Outboard) - Inspection Resolution: RII - 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 Parts USD: No Charge N/C Discrepancy: 15.15 RII - CMP GIV 275027 Flap Actuator Bushing (Left) - Service / Lubrication Resolution: RII - COMPLIED WITH CMP GIV 275027 Flap Actuator Bushing (Left) - Service / Lubrication as required. Work IAW GVI MM 27-06-00. 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_WorkOrderPreliminaryInvoicespt Page 35 of 49 Printed: 5/1/2013 4:M18P) Ref: I: EFTA01117686 Bill To: JEGE, INC. WO 9: SC13175 Invoice Number: 7113001424 Discrepancy: 15.16 RII - CMP GIV 275028 Flap Acuator Bushing (Right) - Service / Lubrication Resolution: RII - COMPLIED WITH CMP GIV 275028 Flap Acuator Bushing (Right) - Service / Lubrication as required. Work IAW GVI MM 27-06-00. Discrepancy: 15.17 CMP GIV 280005 Fuel Control System - Functional Test Resolution: COMPLIED WITH CMP GIV 280005 Fuel Control System - Functional Test. REF item 6.7 for discrepancy found. Work performed LAW GIV MM 28.05.00 Labor USD: No Charge N/ C 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 GIN/ AMM 53-12-00. Billing Method Flours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $6.84 Total USD: $6.84 Pails: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.19 #1 RTV732-30Z.CLR SEALANT, CLEAR 1 $6.84 $6.84 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_WorkOrderPreliminaryInvoice.rpt Page 36 of 49 Printed: 5/1/2013 4:313:15P/i Ref: I: EFTA01117687 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Step: 15.19.1 Completed Complied with steps B(l) thru B(1) 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 perfcormed IAW. G-IV MM. 53.20.00. Billing Method Hours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $161.40 Total USD: $161.40 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.20 #1 D9100 TAPE, 3 INCH FLAME RETARDANT 1 $161.40 $161.40 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 with no defects noted. All 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 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_WorkOrderPreliminaryInvoice.rpt Page 37 of 49 Printed: 5/1/2013 4:38:18P) Ref: I: EFTA01117688 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Step: 15.23.1 Completed Removed all L/H horizontal stabilizer panels required for CMP 551019. All work I.A.W. GIV MAI 55-14-00. 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. G1V MAI 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. All work I.A.W. GIV MAI 55-14-00. Step: 15.24.2 Completed C/W section B thru B(h) of CMP 551020. No discrepancies noted. All work I.A.W. GIV MAI 55.00.00 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 1JH horizontal stabilizer and elevator panels required for CMP 551023. All work I.A.W. GIV MA1 55-14-00. Step: 15.25.2 Completed C/W section B thru B(k) of CMP 551023. See sqk 8.23 and8.20 for discrepancies noted. All work I.A.W. GIV Mal 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.W. GIV M/M 55-00-00. Labor USD: No Charge N/ C Step: 15.26.1 Completed In progress removal of R/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/1 log book All work I.A.W. GIV M/M 55.14.00. Step: 15.26.2 Completed Removed remaining required panels for CAP 551024. CM section B thru B(k) of CMP 551024. See sqk 8.21 and 8.22 for discrepancies noted. All work I.A.W. GIV MAI 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 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_WorkOrderPreliminaryInvoice.rpt Page 38 of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117689 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 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 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, 109-LH-9, 109-LH-11, 109-LH-10, 109-RB-I, 109-LH-8, 110-LH-1,110-LH-2, 110-LH-3, 110-LH-4, 110-LH-5, 110-LH-6, 109-LH-7. Work done IAN' GIV CMP 553007 & GIV MAI 55.30.00. Step: 15.28.3 Completed Continue with removal of all requlered panels of CMP 553007; And Complied with steps B.(1) thru step B(22).All work done IAW 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 816. 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: COMPLIED WITH CMP GIV 571025 Wing Tank Interior (Left) - Inspection. No defect noted at this time. Work IAW GIV MM 57-00-00. 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_WorkOrderPreliminaryinvoice.rpt Page 39 of 49 Printed: 5/1/2013 4:313:18M Ref: I: EFTA01117690 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 15.32 CMP GIV 571026 Wing Tank Interior (Right) - Inspection Resolution: COMPLIED WITH CMP GIV 571026 Wing Tank Interior (Right) - Inspection. No defect noted at this time. Work 1AW GIV MM 57-00-00. 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-FT-5. Work done 1A1V GIV NUM 28-11.00. Discrepancy: 15.33 Related CMP Codes Resolution: Complied with related CMP codes as required. Refer to items 15.34 through 15.64 below for maintenance performed. Discrepancy: 15.34 CMP GIV 251109 SEAT ASSEMBLY, PILOT Resolution: COMPLIED WITH CMP GIV 251109 SEAT ASSEMBLY, PILOT. Removed pilot seat assy. (PN: I159SCF213-5, 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) - Removal / Installation Resolution: Remove L/H fire bottle P/N 32700022 S/N 06758C2. Install overhauled L/H fire bottle P/N 32700022 S/N 06758C2 IAW GIV AMM 26-02-00. Labor USD: No Charge N/ C Step: 15.36.1 Completed Removed L/H fire bottle P/N 32700022 SIN 06758C2, squibs removed and stored in parts room. L/A/W GIV AMM 26-02-00 Discrepancy: 15.37 CMP GIV 262065 Fire Bottle (Left Engine) - Weight Check 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 40 of 49 Printed: 5/1/2013 4:38:18P/ Ref: I: EFTA01117691 Bill To: JEGE, INC. WO SC13175 Invoice Number: 7113001424 Resolution: COMPLIED WITH CMP GIV 262065 Fire Bottle (Left Engine) - Weight Check IAW GIV AMM 26-02-00. 10.97 lbs Labor USD: No Charge N/ C Discrepancy: 15.38 CMP GIV 262030 Engine Fire Bottle (Right) - Removal / Installation Resolution: Remove R/H fire bottle P/N 32700022 S/N 12204C1. Install overhauled R/H fire bottle P/N 32700022 S/N 12204C1 IAW GIV AMM 26-02-00. Labor USD: No Charge N/ C Step: 1538.1 Completed Removed R/H fire bottle P/N 32700022 S/N 12204C1, squibs removed and stored in parts room. 1./A/W GIV AMM 26-02-00 Discrepancy: 15.39 CMP GIV 262070 Fire Bottle (Right Engine) - Weight Check Resolution: COMPLIED WITH CMP GIV 262070 Fire Bottle (Right Engine) - Weight Check IAW GIV AMM 26.02-00. 10.05 lbs Labor USD: No Charge NI C Discrepancy: 15.40 RII - CMP GIV 275003 Flap (Left) Resolution: RII - COMPLIED WITH CMP GIV 275003 Flap (Left). Removed LH Flap PN 1159CS20005-S43 SN 1086, Installed LH Flap PN 1159CS20005.543 SN 1086 IAW GIV MM 27-06-00. Labor USD: No Charge NI 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 LH Flap PN 1159C520005543 SN 1086 Step: 15.40.3 Completed Installed LH Flap PN 1159CS20005-S43 SN 1086 IAW GIV MM IAW GIV MM 27.06.00. Discrepancy: 15.41 RII - CMP GIV 275004 Flap (Right) Resolution: RII - COMPLIED WITH CMP GIV 275004 Flap (Right). Removed RH flap PN 1159C520005-844 SN 1085 and Installed RH flap PN 1159C520005-844 SN 1085 IAW GIV MM 27-06.00. 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_WorkOrderPreliminaryInvoice.rpt Page 41 of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117692 Bill To: JEGE, INC. WO SC13175 Invoice Number: 7113001424 Step: 15.41.1 Completed Complied with CMP 275004 RIGHT FLAP REMOVAL/ INSTALLATION steps A, B and C as required. Work IAW GIV MM27-06-00. Step: 15.41.2 Completed Remove RH flap PN 1159C520005.544 SN 1085 Step: 15.41.3 Completed Installed RH flap PN 1159CS20005-544 SN 1085 JAW GIV MM 27-06-00. Discrepancy: 15.42 RII - CMP GIV 275005 Inboard Flap Actuator (Left) - Removal / Installation Resolution: RII - Remove Inbd flap actuator PN 1159SCC211-13 SN 44-514 and installed an overhauled actuator PN 1159SCC211-15 SN 58.1461as per GIV MM 27-06-00. No defect was noted. Labor USD: No Charge N/ C Step: 15.42.1 Completed Performed CMP code 275005 Remove Inbd Flap Actuator PN 1159SCC211-13 SN44-514 steps B-1 through B-I0 complete. Discrepancy 15.43 RH - CMP GIV 275007 Outboard Flap Actuator (Left) - Removal / Installation Resolution RH - Remove LH Outbd Flap Actuator PN 1159SCC201-13 SN 34-624 and installed an overhauled actuator PN 1159SCC212-15, S/N 90.913, as per GIV MM 27-06-00. No defect was noted. Labor USD: No Charge N/ C Step: 15.43.1 Completed Performed CMP code 275007 Remove Outbd Flap Actuator PN 1159SCC212-13 SN34-624 steps B-1 through B-11 complete. Discrepancy: 15.44 RII - CMP GIV 275006 Inboard Flap Actuator (Right) - Removal / Installation Resolution: RII - COMPLIED WITH CMP GIV 275006 Inboard Flap Actuator (Right) - Removal / Installation. Removed R/H Inb Flap Actuator PN 1159SCC211-13, SN 60-390 and installed an overhauled actuator PN 1159SCC211.15, SN 91-848. Work IAW GIV MM 27-06-00. 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 IAW GIV M3127-06-00. Step: 15.44.2 Completed Complied with CMP 275006 Inboard Flap Actuator (Right) - Removal I Installation step C. Work IAW GIV M5127-06-00. Discrepancy: 15.45 RII - CMP GIV 275008 Outboard Flap Actuator (Right) Removal / Installation Resolution: RH - COMPLIED WITH CMP GIV 275008 Outboard Flap Actuator (Right) - Removal / Installation. Removed R/H Outbd Flap Actuator PN 1159SCC212-14, SN 60.257 and installed an overhauled actuator PN 1159SCC212-16 S/N 12-928. Work IAW GIV MM 27-06-00. 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 42 of 49 Printed: 5/1/2013 4:313:18PF Ref: I: EFTA01117693 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Step: 15.45.1 Completed Complied with CMP 275008 Outboard Flap Actuator (Right) - Removal / Installation steps A and B. Work IAW GIV MM27-06-00. Step: 15.45.2 Completed Complied with CMP 275008 Outboard Flap Actuator (Right) - Removal / Installation step C. Work IAW 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: performed HF Communication System No.1- Operational Check. No defects noted. All work performed I.A.W. GIV M.M. 23.03-00. CAV CMP-231114. Labor USD: No Charge N/ C Discrepancy: 15.48 CMP GIV 231117 HF Communication Antenna - Continuity Check (Installed) Resolution: N/A, HF antenna was not removed. Discrepancy: 15.49 CMP GIV 231155 HF Communication Antenna Assembly - Removal / Installation Resolution: N/A, HF antenna was not removed. Discrepancy: 15.50 CMP GIV 231115 HF COMM SYS #2-OPS TEST Resolution: COMPLIED WITH CMP GIV 231115 HF COMM SYS #2-OPS TEST. HF Comm system #2 passes operational checks with no defects found. Performed this work IAW 6400 AMM 23-03-00. 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_WorkOrderPreliminaryinvoicespt Page 43 of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117694 Bill To: JEGE, INC. WO SC13175 Invoice Number: 7113001424 Discrepancy: 15.51 CMP GIV 280018 Fuel Tank (Left) - Leak Check Resolution: COMPLIED WITH CMP GIV 280018 Fuel Tank (Left) - Leak Check All work done IAW GIV AMM 28.01.00. No defects noted at this time. Labor USD: No Charge N/ C Parts USD: No Charge N/ C Step: 15.51.1 Completed Complied with CMP 280018 Fuel Tank (Left) - Leak Check All work done IAW GIV AMM 28-01.00. No defects noted at this time. Discrepancy: 15.52 CMP GIV 574005 Wing Leading Edge (Left Inboard) - Removal / Installation Resolution: Complied with CMP GIV 574005 Wing Leading Edge (Left Inboard) - Removal / Installation as required IAW GIV MM 57-40-00. Billing Method Flours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $347.34 Total USD: $347.34 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 15.52 #1 M83248/1-226 0 RING PACKING-HTM,1.974 ID 6 $1.61 $9.66 S2L-226 S2D-226 15.52 #2 M83248/1-230 0 RING PACKING-HTM,2.474 ID 24 $1.26 $30.24 15.52 #3 GG510C300A 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 GIV 574011 Wing Leading Edge (Left Center) - Removal / Installation Resolution: Complied with CMP GIV 574011 Wing Leading Edge (Left Center) - Removal / Installation as required IAW GIV MM 57-40-00. Labor USD: No Charge N/ C Step: 15.53.1 Completed Remove gap band 21-LE-4 ansd center section leading edge front aircraft for inspection 2ILE-5 Discrepancy: 15.54 CMP GIV 574017 Wing Leading Edge (Left Outboard) - Removal / Installation Resolution: Complied with CMP GIV 574017 Wing Leading Edge (Left Outboard) - Removal / Installation as required IAW GIV MM 57-40-00. 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_WorkOrderPreliminaryInvoice.rpt Page 44 of 49 Printed: 5/1/2013 4:38:18PF Ref: I: EFTA01117695 Bill To: JEGE, INC. WO SC13175 Invoice Number: 7113001424 Step: 15.54.1 Completed Remove gap bands 21-LE-6 and 21LE-8. Remove outboard section leading edge 211.E-7 from wing. Discrepancy: 15.55 CMP GIV 574006 Wing Leading Edge (Right Inboard) - Removal / Installation Resolution: Complied with CMP GIV 574006 Wing Leading Edge (Right Inboard) - Removal / Installation as required IAW GIV MM 57-40-00. Billing Method flours Rate Total Labor USD: No Charge N/C Parts USD: Time and Material $187.74 Total USD: $187.74 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 15.55 #1 PR1440-B-1/2 SEALANT, PRC,CARTRIDGE 2 $26.82 $53.64 15.55 #2 PR1440-B-1/2 SEALANT, PRC,CARTRIDGE 1 $26.82 $26.82 15.55 #3 PR1440-B-1/2 SEALANT, PRC,CARTRIDGE 2 $26.82 $53.64 15.55 #4 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: COMPLIED WITH CMP GIV 574012 Wing Leading Edge (Right Center) - Removal / Installation as required IAW GIV MM 57-40-00. Labor USD: No Charge N/C Discrepancy: 15.57 CMP GIV 574018 Wing Leading Edge (Right Outboard) - Removal / Installation Resolution: COMPLIED WITH CMP GIV 574018 Wing Leading Edge (Right Outboard) - Removal / Installation as required IAW GIV MM 57-40-00. Labor USD: No Charge N/C Discrepancy: 15.58 CMP GIV 280010 Defueling Procedures Resolution: COMPLIED WITH CMP GIV 280010 Defueling Procedures IAW GIV MM 28-04-00. Defueled 5000Ibs. 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_WorkOrderPreliminaryinvoice.rpt Page 45 of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117696 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 15.59 CMP GIV 282025 Fuel Pickup Screen (Main Left Wing) - Inspection Resolution: COMPLIED WITH CMP GIV 282025 Fuel Pickup Screen (Main Left Wing) - Inspection IAW GIV AMM 28-00-00. Labor USD: No Charge NI C Discrepancy: 15.60 CMP GIV 282026 Fuel Pickup Screen (Alternate Left Wing) - Inspection Resolution: COMPLIED WITH CMP GIV 282026 Fuel Pickup Screen (Alternate Left Wing) Inspection IAW GIV AMM 28-00-00. No defects found. Labor USD: No Charge NI C Discrepancy: 15.61 CMP GIV 571003 Wing Fasteners - Cadmium Plating Degradation - Check (Left) Resolution: COMPLIED WITH CMP GIV 571003 Wing Fasteners - Cadmium Plating Degradation - Check (Left). No defect noted at this time. Work IAW GIV MM 57-10-00. Labor USD: No Charge N/ C Discrepancy: 15.62 CMP GIV 280019 Fuel Tank (Right) - Leak Check Resolution: Complied with CMP 280019 Fuel Tank (Right ) - Leak Check All work done IAW GIV AMM 28-01-00. No defects noted at this time. Labor USD: No Charge NI C Step: 15.62.1 Completed Completed CMP 280019 Fuel Tank (Right ) - Leak Check All work done IAW CIV AMM 28.01.00. No defects noted at this time. Discrepancy: 15.63 CMP GIV 282027 Fuel Pickup Screen (Main Right Wing) - Inspection Resolution: COMPLIED WITH CMP GIV 282027 Fuel Pickup Screen (Main Right Wing) - Inspection JAW GIV AMM 28-00-00. No defects found. Labor USD: No Charge NI 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_WorkOrderPreliminaryInvoice.rpt Page 46 of 49 Printed: 5/1/2013 4:38:18P/i Ref: I: EFTA01117697 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 15.64 CMP GIV 282028 Fuel Pickup Screen (Alternate Right Wing) - Inspection Resolution: COMPLIED WITH CMP GIV 282028 Fuel Pickup Screen (Alternate Right Wing) - Inspection IAW GIV AMM28-00-00. No defects found. Labor USD: No Charge NI C Item: 16 Pilots for Conditioned Survey Flight (Pre Test Flight) Team Manager. Sean Brown ParVModel #: 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: Test flight performed by GAC pilots Billing Method flours Rate Total Labor USD: Flat Rate $5,500.00 Services USD: No Charge NI C Total USD: $5,500.00 Services: Ref. No. Description Quantity Sell Price USD Extended USD 16.1 #1 SERVICE 1.00 $0.00 $0.00 Discrepancy: 16.2 Perform Preparation for Flight Test Traveler Resolution: Complied with GIV Preparation For Flight Test IAW QAP 9.2, RS-Q(7-0217 Rev. 01 and RSQCT-54 Rel. 18, refer to steps for details. Billing Method Flours Rate Total Labor USD: Time and Material ST 49.62 @ $115.00 $5,706.30 Labor USD: Time and Material OT 0.82 @ $173.00 $141.86 Parts USD: Time and Material $213.28 Total USD: $6,061.44 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 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_WorkOrderPreliminaryInvoice.rpt Page 47 of 49 Printed: 5/1/2013 4:313:1BP/i Ref: I: EFTA01117698 Bill To: JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Pans: 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: 16.2.1 Completed Complied with Preparation for Flight Test Traveler section C thru Q JAW Flight Test Traveler Step: 161.2 Completed Complied with most items on the checklist. All work done JAW Traveler Number RS-QC-F-0217 Rev. 01. Step: 16.2.3 Completed Complied with open items on hot cockpit checklist. All work done JAW Traveler Number RS-QCT-0217 Rev. 01. Discrepancy: 16.3 Perform bulb sweep Resolution: Removed several defective lights bulb's on Cockpit Overhead Panel (COP) P/N 0L3335 nsn. Installed new lights bulb's on Cockpit Overhead Panel (COP) P/N OL3335 nsn. Op's check good. All work was done IAW Gulfstream GIV AMM 33.10.01. Billing Method Flours Rate Total Labor USD: Time and Material ST 4.00 @ $115.00 $460.00 Parts USD: Time and Material $51.50 Total USD: $511.50 Pans: Ref. No. Pan number: Description Quantit • Sell price USD Extended USD 16.3 #1 OL3335 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 Howl Rate Total Labor USD: Time and Material ST 4.00 @ $115.00 $460.00 Total USD: $460.00 Discrepancy: 16.5 Return to service EJM for Evaluation Flight. 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 48 of 49 Printed: 5/1/2013 4:313:15P/ Ref: I: EFTA01117699 Bill To: JEGE, INC. WO4/: SC13175 Invoice Number: 7113001424 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; Gulfstream West Palm Beach, FL 33406 FAA CRS PB8R624N Billing Method Flours Rate Total Labor USD: Time and Material ST 0.57 @ $115.00 565.55 Total USD: $65.55 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 Mum Rate Total Labor USD: Time and Material ST 0.56 @ $115.00 564.40 Total USD: $64.40 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 PO BOX 2206, Savannah, GA 31402 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 49 Printed: 5/1/2013 4:313:18P/i Ref: I: EFTA01117700

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