EFTA01117652.pdf

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 Dis