EFTA01112828.pdf

Gu]£stream' A OSSISNAL DYNAMICS COMPANY PRELIMINARY INVOICE ParUModel GIV AC Serial No./Tail No.: 1085 / N212JE Bldg C.—FAX - West Palm Beach, Florida 33406 Mail Remittance To: Overnight Remittance To: Wire Remittance To: Gulfstream Aerospace Corporation Gulfstream Aerospace Corporation (Box a 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 TX1-0029 Chicago, IL 60670 14800 Frye Road Account No. 10-15825 Ft. Worth, TX 76155 Fedwire Routing No. (ABA) 021 000 021 S.W.I.F.T. CHASUS33 ACH Credit Routing No. (ABA)071 000013 Invoice Number: 7115002256 Bill To: JEGE LLC Invoice Date: 8/14/2015 C/O GALAXY AVIATION INC Customer ID: BJ419 MTN: LARRY VISOSKI P.O. Number: 3800 SOUTHERN BLVD, SUITE 204 Repair Station: FAA CRS PB8R624N WEST PALM BEACH, Florida 33406 In Date: 08/03/2015 United States Out Date: 08/09/2015 Payment Type: COD - Certified Check Payment Terms: Title: JEGE LLC INVOICE SUMMARY FOR WORK ORDER NUMBER: SC17734 Time & Materials Flat Rate Total Labor USD: $3,920.49 $2,159.00 $6,079.49 Parts USD: $28,472.25 $362.62 $28,834.87 Services USD: $0.00 $9,956.01 $9,956.01 Detail Subtotal USD: $32,392.74 $12,477.63 $44,870.37 Subtotal USD: $44,870.37 Funds on Deposit USD: 50.00 Total USD: $44,870.37 Customer on the following programs:MSP(APU) HAPP and Corp care 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 2011 Page I of I8 Printed: 8/14/2015 12:44:27P1 Ret EFTA01112828  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Item: I Airframe Scheduled GIV N212JE Team Manager: Sean Brown Part/Model #: GIV Customer Coordinator: Benny Rios AC Serial No./rail No.: 1085 / N212JE TSN/TSO: 9023.1 CSN/CSO: 4163 Aircraft Time: 9023.1 Discrepancy: 1.1 Return to Service FAR Part 91. Resolution: ACTT: 9023.1 ACTL: 4163 DATE: 08/07/2015 I certify that the maintenance listed was performed in accordance with current Federal Aviation Regulations and is approved for return to service with regards to the maintenance accomplished. Further details are on file at this repair station under the above work order. A copy of the work order has been provided to the operator. Caryn Haner, Airworthiness Inspector Gulfstream West Palm Beach, FL 33406 FAA CRS PB8R624N Labor USD: No Charge N/ C Discrepancy: 1.2 Inbound/Outbound Inspection Resolution: Complied with inbound and outbound inspections as required. 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 Discrepancy: 1.4 Comply with Debrief Checklist 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 2011 Page 2 of 18 Printed: 8/14/2015 12:44:27P1 Rat: EFTA01112829  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Step: 1.4.1 Completed Arrival/Debrief 90 Day Due List Review Accomplished. Step: 1.4.2 Completed List Operator's Airworthiness Requirements & Special Documentation Requests. Step: 1.4.3 Completed Review Technical Operations Update prior to return to service for newly released bulletins and advise operator. Discrepancy: 1.5 "Feu] Clearance Resolution: AU tooling returned. Discrepancy: 1.6 Cover & Protect Resolution: Protected aircraft as required. Discrepancy: 1.7 Service Chemical Toilet/Clean Galley Resolution: N/A Discrepancy: 1.8 ArrivaUDeparture Assist & Video Aircraft Resolution: N/A Discrepancy: 1.9 Sample Hydraulic Fluids Resolution: N/A Discrepancy: 1.10 Remove Valuables & Secure. 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 2011 Page 3 of IS Printed: 8/14/2015 12:44:27P1 Rd': EFTA01112830  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Resolution: N/A Discrepancy: 1.11 Comply with Service Team Manager Checklist Resolution: N/A Discrepancy: 1.12 Fluids Used (Oils/Skydrol) - (Materials Only) Resolution: N/A Discrepancy: 1.13 STN1 / Quality review of work order and logbook entry prior to departure Resolution: Na Discrepancy: 1.14 Towing (Does not include Hangar Moves) Resolution: Towed aircraft as required for maintenance. Discrepancy: 1.15 HazMat - Identify & provide a manifest, and a Shipper's Declaration for Dangerous Goods for all hazardous materials that are loaded aboard any aircraft. FAR Part 121 or 135 Operators will provide a hazardous material notification letter required by FAR 135.505 (e) prior to maintenance at this Repair Station iaw FAR 145.206 (a) (b). If there is to be loading of hazardous materials it shall be complied with by Hazmat trained authorized GAC-PBI personnel only. 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 2011 Page 4 of IR Printed: 8/14/2015 12:44:27P1 Rat: EFTA01112831  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Resolution: N/A Discrepancy: 1.16 Aircraft Cleaning Resolution: N/A Discrepancy: 1.17 Billable Consumables & Shop Supplies Resolution: To be billed as required. Billing Method I lours Rate Total Parts USD: Flat Rate $362.62 Total USD: $362.62 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 2011 Page 5 of IS Printed: 8/14/2015 12:44:27P1 Rat: EFTA01112832  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 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-IB, CHANGE 1 CHAPTER 11, SECTION 8. Resolution: Nut 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 2011 Page 6 of IS Printed: 8/14/2015 12:44:27P1 Rat: EFTA01112833  Bill To: JEGE LW WO #: SC17734 Invoice Number: 7115002256 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 GAN1PS 4000, total average thickness shall not exceed 6 mils. * Per CAC Mass Properties Engineering, paint thickness of 5 mils equals .055 pounds per square foul. * If after QC review, weight change is greater than 2 pounds or .05% of MAC, the weight and balance report \vill require recomputation. Resolution: N/A Discrepancy: 1.21 "Advise customer of preservation requirements per ATA Chapter 10 of the relevant maintenance manuals for Airframe, Engines, and APU; review requirements in relation to scheduled Date Promised and later potential Date Completed; and perform maintenance or preservation actions as directed by the customer and documented as a Work Order Squawk. Resolution: N/A Item: 3 Engine Team Manager: Sean Brown PartfModel #: Customer Coordinator: Benny Rios S/N: TSN/TS0: CSN/CS0: Aircraft Time: Discrepancy: 3.1 R/H engine - While removing #10 fan ring bolt, found threaded insert threads damaged. Removed threaded insert and bolt per Rolls Royce rep. Parts ordered under item 2.1. Resolution: Removed bad nut P/N AS27870 and installed a NEW nut P/N AS27870 IAW RR Tay-611-8 EMM 70-42-09 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_Work0rderPreliminaryInvoice.rpt 2011 Page 7 of 18 Printed: 8/14/2015 12:44:27P1 Rd': EFTA01112834  Bill To: JEGE LLC WO #: SC17734 Invoice Number: 7115002256 Discrepancy: 3.2 With Assistance from Rolls Royce perform fan dynamic trim balance test#9 Resolution: Complied wth Rolls Royce Dynamic Trim Balance test #9. Please see Rolls Royce Form T1-611-8 for details. All work In accordance with RRTAY611-8ENINI 71-00-00-700-013-B02TEST No-9 item. 6 ..kvionies Team Manager: Sean Brown Part/Model #: Customer Coordinator: Benny Rios AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 6.1 #3 standby comm radio display inoperative (Customer discrepancy) Resolution: Verified discrepancy. Removed # 3 Comm Control P/N 622-9851-001 SIN 256. Installed OVERHAULED unit P/N 622-9851-001 S/N 384. All work accomplished JAW GIV AMM 23-01-00. Refer to item 6.2. Billing Method flours Rate Total Labor USD: Time and Material ST 2.67 ® $127.00 $339.09 Parts USD: Time and Material $2,012.00 Total USD: $2,351.09 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 6.1 #1 622-9851-001 CONTROL COMM CTL2300 1 $2,012.00 $2,012.00 Step: 6.1.1 Completed Verified discrepancy. When turning control on, initially,all digits will light up, but then fade away within 2 seconds. Control is bad. Placed com control, p/n 622-9851-001, on order. Failed sin 256. Work done JAW GIV MM 23-01-00. Discrepancy: 6.2 CMP GIV 231023 CONTROL, #3 VHF COMM Resolution: COMPLIED WITH CMP GIV 231023 CONTROL, #3 VHF COMM JAW GIV AMM 23-01-00. Removed P/N 622-9851-001 SIN 256. Installed OVERHAULED P/N 622-9851-001 S/N 384. IAW GIV MM 23-01-00. Item: 8 Mechanical 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 2011 Page 8 of Is Printed: 8/14/2015 12:44:27P1 Rat: EFTA01112835  Bill To: JEGE LLC WO #: SC17734 Invoice Number: 7115002256 Team Manager: Sean Brown Part/Model #: Customer Coordinator: Benny Rios AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 8.1 CMP GIV 324042 Main Tire (Left, Inboard No. 2) - Breakdown / Buildup Procedure (Aircraft Braking System) (Customer Request) Resolution: As per customer request no action to be taken at this time. Parts USD: No Charge N/ C Discrepancy: 8.2 CMP GIV 324012 Main Gear Wheel Assembly 1.c ft, Inboard No. 2) - Removal / Installation Resolution: No action taken. Parts USD: No Charge Discrepancy: 83 CMP GIV 324038 TIRE -SERVICING Resolution: No action taken. Discrepancy: 8.4 CMP GIV 324052 MLG Wheel Bearings (Left I/B #2) - Insp / Pack (ABS) Resolution: No action taken. Parts USD: No Charge N/ C Discrepancy: 8.5 CMP GIV 324044 Main Tire (Right, Outboard No. 4) - Breakdown / Buildup Procedure (Aircraft Braking System) (Customer Request) Resolution: As per customer request no action to be 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_WorkOrderPreliminaryInvoice.rpt 2011 Page 9 of IS Printed: 8/14/2015 12:44:27P1 Rat: EFTA01112836  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Discrepancy: 8.6 CMP GIV 324014 Main Gear Wheel Assembly (Right, Outboard No. - Re 1110% al / Installation (ABS) Resolution: No action taken. Discrepancy: 8.7 CMP GIV 324054 MLG Wheel Bearings (Right O/B #4) - Insp / Pack (ABS) Resolution: No action taken. Discrepancy: tit Evaluate bleed air isolation valve for sticking. Resolution: Removed bleed air isolation/ shut off valve PN. 398896-3-1 SN. 396 and installed a repaired valve PN. 398896-3-1 SN. 738 IAW GIV MM 36-12-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 5.95 @ $127.00 $755.65 Labor USD: Time and Material OT 0.08 @ $127.00 $10.16 Parts USD: Time and Material $23,530.00 Total USD: $24,295.81 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.8 #3 398896-3-1 VALVE, ISOLATION, BLEED AIR 1 $23,530.00 $23,530.00 Step: 8.8.1 Completed Perfomed ops check of valve and verified valve is stuck in closed position. Cockpit isolation valve switch indication doesn't Illuminate. Bulbs check good. Removed connector 54L5 at isolation valve and checked for voltage. II5NAC was found between pins I and 2. P.O.O. Work done IAW CIV WM 36-12-00 and GIN' WDNI 36-12-00. Discrepancy: 8.9 Visually Inspect LJH Engine Isolator Mount Resolution: Opened IJH Cowl to to gain access. Visually inspected Fwd and Aft engine Isolator mounts as installed on engine, took messurement of isolator for sagging condition as noted..7 in from pin to top of isolator and 5.5 in for lower dimension, aft mount messures the same as the front. Found Dog bone link to be centered. All dimensions are normal at this time. Performed IAW GIV MM. 71-01-00 Billing Method flows Rate Total Labor USD: Time and Material ST 3.00 @ $127.00 $381.00 Total USD: $381.00 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 2011 Page 10 of 18 Printed: 8/14/2015 12:44:27P1 Rd': EFTA01112837  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Step: 8.9.1 Completed Opened 1./II Cowl to to gain access. Visually inspected Fwd and Aft engine Isolator mounts as installed on engine, took messurement of isolator for sagging condition as noted..7 in from pin to top of isolator and 5.5 in for lower dimension, aft mount messures the same as the front. Found Dog bone link to be centered. Performed lAW GIV MM. 71-01.00 Discrepancy: 8.10 Visually Inspect 12/11 Engine Isolator Mount Resolution: Opened FUN Cowl to to gain access. Visually inspected Fwd and Aft engine Isolator mounts as installed on engine, took messurement of isolator for sagging condition as noted, .7 in. from pin to top of isolator and 5.5 in for lower dimension. Aft mount isolators measure the same as the front. Found Dog bone link to be aprox .010 thou from touching side of crane beam. Repositioned link to center position. All Dimensions normal at this time. Performed JAW GIV MM. 71-01-00 Billing Method flours Rate Total Labor USD: Time and Material ST 7.00 @ $127.00 $889.00 Total USD: $889.00 Step: 8.10.1 Completed Opened Cowl to to gain access. Visually inspected Fwd and Aft engine Isolator mounts as installed on engine, took messurement of isolator for sagging condition as noted, .7 in. from pin to top of isolator and 5.5 in for lower dimension. Aft mount isolators measure the same as the front. Found Dog bone link to be aprox .010 thou from touching side of crane beam. Repositioned link to center position. Discrepancy: 8.11 During engine runs found HYD fluid leaking down inboard LH wing LE from behind wing to fuselage panel Resolution: Removed L/H lower wing and L/H fwd. wing to fuselage panel for inspection.Cleaned area around IB LH Wing LE, ran engines, found no evidence of leak at this time. All work performed IAW GIV 29-00-00. Reinstalled all panels removed for access. Billing Method flours Rate Total Labor USD: Time and Material ST 5.50 @ $127.00 $698.50 Total USD: $698.50 Discrepancy: 8.12 CMP GIV 361065 Bleed Air Isolation Shutoff Valve - Removal / Installation Resolution: COMPLIED WITH CMP GIV 361065 Bleed Air Isolation Shutoff Valve - Removal / Installation. Removed bleed air isolation/ shut off valve PN. 398896-3-1 SN. 396 and installed a repaired valve PN. 398896-3-1 SN. 738 IAN' GIV MM 36-12-00. 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 2011 Page I I of 18 Printed: 8/14/2015 12:44:27P1 Rat: EFTA01112838  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Discrepancy: 8.13 The LH belly panel 107/21-LWR-FIL-2 needs a new form in place gasket Resolution: Created new form in place gasket for LH Belly Panel 107/21-LWR-FIL-2 IAW GIVAMM 20-42-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 4.00 @ $127.00 $508.00 Parts USD: Time and Material $74.34 Total USD: $582.34 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.13 #1 PR1440-B-2 SEALANT, PRC, CARTRIDGE 6oz 2 $37.17 $74.34 (MEETS SPEC AMS-S-8802 REV C) 2 HOUR WORK LIFE Item: 10 Outstanding Parts, Materials, and / or Services Team Manager: Scan Brown ParVModel #: Customer Coordinator: Benin• Rios AC Serial NoJTail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 10.1 Loading estimates Resolution: Discrepancy: 10.2 O&A for SC17436.4.182 PN 1159SCAV373-105 Generator JEGE LLC Note: "Terminal Block is cracked - Replace. Shaft is out of specs - Replace. Remove & re-install D.E. End Bell Support & J-2 Cannon Plug. " Resolution: Billed accordingly Billing Method flours Rate Total Services USD: Flat Rate $9,956.01 Total USD: $9,956.01 Services: Ref. No. Description Quantity 10.2 #1 ADD'L BILL-LINE TO CARRY COST 1.00 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 2011 Page 12 of 18 Printed: 8/14/2015 12:44:27P1 Rat: EFTA01112839  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Discrepancy: 10.3 Parts moved for MLG tires. Resolution: Billing Method Hours Rate Total Parts USD: Time and Material $59.48 Total USD: $59.48 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 103 #5 PR1440-B-112 SEALANT, PRC, CARTRIDGE 1 $29.74 $29.74 (MEETS SPEC AMS-S-8802 REV C) 103 #6 PR1440-B-112 SEALANT, PRC, CARTRIDGE 1 $29.74 $29.74 (MEETS SPEC AMS-S-8802 REV C) Item: 12 Service Center Maintenance Induction Checklist Team Manager: Sean Brown Part/Model #: Customer Coordinator: Benny Rios AC Serial No/Tail No.: N/A / N/A TSN/TS0: N/A CSN/CS0: N/A Aircraft Time: N/A Discrepancy: 12.1 CMP GIV 010010 Service Center Maintenance Induction Checklist Resolution: Complied with CMP GIV 010010 Service Center Maintenance Induction Checklist Item: 13 Post Test Flight discrepancies Team Manager: Sean Brown Part/Model #: GIV Customer Coordinator: Benny Rios AC Serial No/Tail No.: 1085 / N212JE TSN/TS0: 9024.2 CSN/CS0: 4164 Aircraft Time: 9023.9 Discrepancy: 13.1 Return to Service FAR Part 91. 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_Work0rderPreliminaryInvoice.rpt 2011 Page 13 of 18 Printed: 8/14/2015 12:44:27P1 Rat: EFTA01112840  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Resolution: ACTT: 9024.2 ACTL: 4164 DATE: 8-10-15 I certify that the maintenance listed was performed in accordance with current Federal Aviation Regulations and is approved for return to service with regards to the maintenance accomplished. Further details are on file at this repair station under the above work order. A copy of the work order has been provided to the operator. David A. Cabral , Airworthiness Inspector Gulfstream West Palm Beach, FL 33406 FAA CRS PB8R624N Labor USD: No Charge N/C Parts USD: No Charge N/C Discrepancy: 13.2 CMP GIV 324042 Main Tire (Left, Inboard No. 2) - Breakdown / Buildup Procedure (Aircraft Braking System) Resolution: COMPLIED WITH CMP GIV 324042 Main Tire (Left, Inboard No. 2) - Breakdown / Buildup Procedure (Aircraft Braking System) Removed #2 main tire (PN: 348F83-2, SN: 03313401) and installed new tire (PN: 348F83-2, SN: 21733406). Ref: GIV AMM 32.42-00. See item 13.10 for original discrepancy Billing Method Bows Rate Total Labor USD: Flat Rate $444.50 Parts USD: Time and Material $1,411.40 Total USD: $1,855.90 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 13.2 #1 1159SCL206-33 TIRE, MAIN 1 $1,353.00 $1,353.00 13.2 #2 MS28775-383 PACKING 2 $27.03 $54.06 13.2 #3 RG-30 BRING 2 $2.17 $4.34 Discrepancy: 13.3 CMP GIV 324012 Main Gear Wheel Assembly (Left, Inboard No. 2) - Removal / Installation (ABS) Resolution: COMPLIED WITH CMP GIV 324012 Main Gear Wheel Assembly (Left, Inboard No. 2) - Removal / Installation (ABS) Removed #2 main wheel assy. (PN: 5008447-1, SN: MAR90-18) and installed same servicable wheel assy (PN: 5008447-1, SN: MAR90-18). Ref: GIV AMM 32-42-01. See item 13.10 for original discrepancy 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_WorkOrderPreliminaryInvoice.rpt 2011 Page 14 of 18 Printed: 8/14/2015 12:44:27P1 Rat: EFTA01112841  Bill To: JEGE LLC WO #: SC17734 Invoice Number: 7115002256 Labor USD: Flat Rate $317.50 Total USD: $317.50 Discrepancy: 13.4 CMP GIV 324052 MLG Wheel Bearings (Left UB #2) - Insp / Pack (ABS) Resolution: COMPLIED WITH CMP GIV 324052 MLG Wheel Bearings (Left UB #2) - Insp / Pack (ABS) See item 13.10 for original discrepancy Billing Method Hours Rate Total Labor USD: Flat Rate $254.00 Parts USD: No Charge N/C Total USD: $254.00 Discrepancy: 13.5 CMP GIV 324044 Main Tire (Right, Outboard No. 4) - Breakdown / Buildup Procedure (Aircraft Braking System) Resolution: COMPLIED WITH CMP GIV 324044 Main Tire (Right, Outboard No. 4) - Breakdown / Buildup Procedure (Aircraft Braking System) Removed #4 main tire assy (PN: 348F83-2, SN: 03203402) and installed new tire assy (PN: 348F83-2, SN: 01593138). Ref: GIV AMM 32-42-00. See item 3.11 for original discrepancy Billing Method flours Rate Total Labor USD: Flat Rate $444.50 Parts USD: Time and Material $1353.00 Total USD: $1,797.50 Parts: Ref'. No. Part number: Description Quantity Sell price USD Extended USD 13.5 #1 1159SCL206-33 TIRE, MAIN 1 $1,353.00 $1353.00 Discrepancy: 13.6 CMP GIV 324014 Main Gear Wheel Assembly (Right, Outboard No. 4) - Removal / Installation (ABS) Resolution: COMPLIED WITH CMP GIV 324014 Main Gear Wheel Assembly (Right, Outboard No. 4) - Removal / Installation (ABS) Removed #4 main wheel assy (PN: 5008447-3, SN: APRI0-713) and installed same servicable wheel assy. (PN: 5008447-3, SN: APRI0-713) Ref: GIV AMM 32-42-01. See item 13.11 for original discrepancy 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 2011 Page 15 of 18 Printed: 8/14/2015 12:44:27P1 Rat: EFTA01112842  Bill To: JEGE LLC WO #: SC17734 Invoice Number: 7115002256 Billing Method Hours Rate Total Labor USD: Flat Rate $317.50 'total USD: $317.50 Discrepancy: 13.7 CMP GIV 324054 MLG Wheel Bearings (Right 0/B #4) - Insp / Pack (ABS) Resolution: COMPLIED WITH CMP GIV 324054 MLG Wheel Bearings (Right O/B #4) - Insp / Pack (ABS) See item 13.11 for original discrepancy Billing Method Hours Rate Total Labor USD: Flat Rate $254.00 Total USD: $254.00 Discrepancy: 13.8 CMP GIV 324038 TIRE - SERVICING Resolution: COMPLIED WITH CMP GIV 324038 TIRE - SERVICING See items 13.10 and 13.11 for original discrepancy. Labor USD: No Charge N/ C Step: 13.8.1 Completed Serviced both #2 and #4 tires to 187 PSI with nitrogen for 12 hour leak check. Servicing was accomplished at 16:30 on 818115. All work done IMV GIV MM 32-40-00. Step: 13.8.2 Completed Checked and serviced tires as necessary. No defects noted. Ref: GIV MM sec 32-40-00. Discrepancy: 13.9 Inspect NILG for evidence of Hydraulic leak Resolution: Inspected left and right main landing gear for hydraulic leaks, no leaks found. Ref: GIV MM sec 32-00-00. Billing Method flours Rate Total Labor USD: Flat Rate $127.00 Total USD: $127.00 Discrepancy: 13.10 #2 main tire requires replacement 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 2011 Page 16 of 18 Printed: 8/14/2015 12:44:27P1 Rat: