EFTA01117750.pdf

Gu]£stream' A OSNIMAL DYNAMICS COMPANY PRELIMINARY INVOICE ParUModel GIV AC Serial No./Tail No.: 1085 / N212JE Bldg C.-FAX 561-681-9392 - \Vest Palm Beach, Florida 33406 Mail Remittance To: Overnight Remittance To: Wire Remittance To: Gulfstream Aerospace Corporation Gulfstmam Aerospace Corporation (Box 0 730349) Gulfstmam 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 Ft. Worth, TX 76155 Fedwire Routin No. ABA) S.W.I.F.T ACH Credit Routing No. (ABA Invoice Number: 7115002256 Bill To: JEGE LLC Invoice Date: 8/19/2015 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 23 Printed: 8/19/2015 1:08:28P1 Reel EFTA01117750  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 NoJTail 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 23 Printed: 8/19/2015 1:08:28P1 Rot EFTA01117751  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_WorkOrderPreliininaryInvoice.rpt 2011 Page 3 of 23 Printed: 8/19/2015 1:08:28P/ ;Ceti EFTA01117752  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 STM / 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 23 Printed: 8719/2015 1:08:28P1 Rot EFTA01117753  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_WorkOrderPreliininaryInvoice.rpt 2011 Page 5 of 23 Printed: 8/19/2015 1:08:28P1 Rot EFTA01117754  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/X XXX. 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 23 Printed: 8/19/2015 1:08:28P1 Rot EFTA01117755  Bill To: JEGE LW WO It 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 lout. * If after QC review, weight change is greater than 2 pounds or .05% of MAC, the weight and balance report will require recomputation. Resolution: N/A Discrepancy: 1.21 "Advise customer of preservation requirements per ATA Chapter 10 of the relevant maintenance manuals for Airframe, Engines, and APU; review requirements in relation to scheduled Date Promised and later potential Date Completed; and perform maintenance or preservation actions as directed by the customer and documented as a Work Order Squawk. Resolution: N/A Item: 2 Engine Team Manager: Sean Brown PartfModel #: Customer Coordinator: Benny Rios S/N: TSN/TS0: 8967.4 CSN/CS0: 4129 Aircraft Time: Discrepancy: 2.1 Assist Rolls Royce with LH fan clocking 180, to include fan trim balance test#9 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 23 Printed: 8/19/2015 1:08:28PI Retl EFTA01117756  Bill To: JEGE LLC WO $1: SC17734 Invoice Number: 7115002256 Resolution: Repositioned the No. 1 engine fan blades approximately 180 degrees from original position as required. Work performed IAW TAY -611-8 MM 72-31-12. REF Items 2.2 thru 2.25 for actual work performed and present location of each blade. Performed Rolls Royce Test No. 9 Trim Balance of the No. 1 engine LP Compressor Fan Blades IAW RR Tay-611-8 EMM 71-00.00-700-012-B02. Added balance weights as required. 9.5g at Pos. 7, 9.5g at Pos. 10, 9.5g at Pos12. REF Trim Balance sheet provided by Rolls Royce. Step: 2.1.1 Completed Repositioned the No. 1 engine fan blades approximately 180 degrees as required. Work performed IAW TAY -6114 MM 72-31-12. REF Items 2.2 thru 2.25 for actual work performed. Step: 2.1.2 Completed Performed Rolls Royce Test No. 9 Trim Balance of the No. 1 engine LP Compressor Fan Blades IAW RR Tay-611-8 EMM 71-0040-700-012-B02. Added balance weights as required. 9.5g at Pos. 7, 9.5g at Pos. 10, 9.5g at Pos12. REF Trim Balance sheet provided by Rolls Royce. Discrepancy: 2.2 CMP GIV 722901 LP Compressor Fan Blade No. 1 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722901 LP Compressor Fan Blade No. I - Removal / Installation. Removed P/N JR3I702, S/N KLUI. installed P/N on JR31702, SIN on KLW2 Discrepancy: 2.3 CMP GIV 722902 LP Compressor Fan Blade No. 2 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722902 LP Compressor Fan Blade No. 2 - Removal / Installation. Removed P/N JR31702, S/N KKA2. installed P/N on JR31702, S/N on KME2 Discrepancy: 2.4 CMP GIV 722903 LP Compressor Fan Blade No. 3 - Removal Installation Resolution: COMPLIED WITH CMP GIV 722903 LP Compressor Fan Blade No. 3 - Removal Installation. Removed P/N JR31702, S/N KNJ2. P/N on JR31702, S/N on KNL2 Discrepancy: 2.5 CMP GIV 722904 LP Compressor Fan Blade No. 4 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722904 LP Compressor Fan Blade No. 4 - Removal / Installation. Removed P/N JR31702. S/N KKB1. P/N on JR31702, S/N on KLNI 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 23 Printed: 8/19/2015 1:08:28PI ;Ceti EFTA01117757  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Discrepancy: 2.6 CMP GIV 722905 LP Compressor Fan Blade No. 5 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722905 LP Compressor Fan Blade No. 5 - Removal / Installation. Removed P/N JR31702, S/N ICNJ1. P/N on JR31702, S/N on KLR1 Discrepancy: 2.7 CMP GIN' 722906 LP Compressor Fan Blade No. 6 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722906 LP Compressor Fan Blade No. 6 - Removal / Installation. Removed P/N JR31702, S/N KKZ2. P/N on JR31702, S/N on KMG3 Discrepancy: 2.8 CMP GIV 722907 LP Compressor Fan Blade No. 7 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722907 LP Compressor Fan Blade No. 7 - Removal / Installation. Removed P/N JR31702, S/N KLSI. PIN on JR31702, S/N on KMD3 Discrepancy: 2.9 CMP GIV 722908 LP Compressor Fan Blade No. 8 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722908 LP Compressor Fan Blade No. 8 - Removal / Installation. Removed P/N JR31702, S/N KJW2. P/N on JR31702, S/N KIWI Discrepancy: 2.10 CMP GIV 722909 LP Compressor Fan Blade No. 9 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722909 LP Compressor Fan Blade No. 9 - Removal / Installation. Removed P/N JR31702, S/N KLZ3. P/N on JR31702, S/N on KSS2 Discrepancy: 2.11 CMP GIV 722910 LP Compressor Fan Blade No. 10 - Removal / Installation For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 9 of 23 Printed: 8/19/2015 1:08:28P1 Rot EFTA01117758  Bill To: JEGE LW WO It SC17734 Invoice Number: 7115002256 Resolution: COMPLIED WITH CMP GIV 722910 LP Compressor Fan Blade No. 10 - Removal / Installation. Removed P/N JR31702, S/N KSRI. P/N on JR31702, S/N on KKB2 Discrepancy: 2.12 CMP GIV 722911 LP Compressor Fan Blade No. 11 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722911 LP Compressor Fan Blade No. 11 - Removal / Installation. Removed P/N JR31702, S/N KLW2. P/N on JR31702, S/N on KLW3 Discrepancy: 2.13 CMP GIV 722912 LP Compressor Blade Fan No. 12 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722912 LP Compressor Blade Fan No. 12 - Removal / Installation. Remo% ed I"N JR31702, S/N KME2. P/N on JR31702, S/N on KKS1 Discrepancy: 2.14 CMP GIV 722913 LP Compressor Blade Fan No. 13 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722913 LP Compressor Blade Fan No. 13 - Removal / Installation. Remo' ed I"N JR31702, S/N KNL2. P/N on JR31702, S/N on KLUI Discrepancy: 2.15 CMP GIV 722914 LP Compressor Fan Blade No. 14 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722914 LP Compressor Fan Blade No. 14 - Removal / Installation. Removed P/N JR31702, S/N KLN1. P/N JR31702, S/N KKA2 Discrepancy: 2.16 CMP GIV 722915 LP Compressor Fan Blade No. 15 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722915 LP Compressor Fan Blade No. 15 - Removal / Installation. Removed P/N JR31702, S/N KLRI. P/N JR31702, S/N KNJ2 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 23 Printed: 8/19/2015 1:08:28PI ;Ceti EFTA01117759  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Discrepancy: 2.17 CMP GIV 722916 LP Compressor Fan Blade No. 16 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722916 LP Compressor Fan Blade No. 16 - Removal / Installation. Removed PIN JR31702, S/N KMG3. PIN on JR31702, SIN KKB1 Discrepancy: 2.18 CMP GIV 722917 LP Compressor Fan Blade No. 17 - Removal Installation Resolution: COMPLIED WITH CMP GIV 722917 LP Compressor Fan Blade No. 17 - Removal Installation. Removed JR31702, S/N KMD3. P/N on JR31702, SIN on KNJ1 Discrepancy: 2.19 CMP GIV 722918 LP Compressor Fan Blade No. 18- Removal Installation Resolution: COMPLIED WITH CMP GIV 722918 LP Compressor Fan Blade No. 18 - Removal / Installation. Removed P N JR31702, S/N KJW1. P/N on JR31702, S/N on KKZ2 Discrepancy: 2.20 CMP GIV 722919 LP Compressor Fan Blade No. 19- Removal / Installation Resolution: COMPLIED WITH CMP GIV 722919 LP Compressor Fan Blade No. 19 - Removal Installation. Removed N JR31702, S/N KSS2. PIN on JR31702, SIN on KLS1 Discrepancy: 2.21 CMP GIV 722920 LP Compressor Fan Blade No. 20 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722920 LP Compressor Fan Blade No. 20 - Removal / Installation. Removed PIN JR31702, S/N KKB2. P/N on JR31702, S/N on KJW2 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 11 of 23 Printed: 8/19/2015 1:08:28PI ;Ceti EFTA01117760  Bill To: JEGE LW WO #: SC17734 Invoice Number: 7115002256 Discrepancy: 2.22 CMP GIV 722921 LP Compressor Fan Blade No. 21- Removal Installation Resolution: COMPLIED WITH CMP GIV 722921 LP Compressor Fan Blade No. 21 - Removal Installation. Removed PIN JR31702, S/N KLW3. PIN on JR31702, S/N KLZ3 Discrepancy: 2.23 CMP GIV 722922 LP Compressor Fan Blade No. 22 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 722922 LP Compressor Fan Blade No. 22 - Removal / Installation. Removed P N JR31702, S/N KKS1. P/N on JR31702, SIN on KSR1 Discrepancy: 2.24 CMP GIV 722017 FAIRING, NOSE CONE-- ENGINE Resolution: COMPLIED WITH CMP GIV 722017 FAIRING, NOSE CONE— ENGINE Discrepancy: 2.25 CMP GIV 722015 SPINNER, ENGINE Resolution: COMPLIED WITH CMP GIV 722015 SPINNER, ENGINE Item: 3 Engine Team Manager: Sean Brown Part/Model #: Customer Coordinator: Benny Rios S/N: TSN/TSO: CSNICSO: Aircraft Time: Discrepancy: 3.1 Ft/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 'ANY RR Tay-611-8 ENIM 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_WorkOrderPreliminaryInvoice.rpt 2011 Page 12 of 23 Printed: 8/19/2015 1:08:28PI Rot EFTA01117761  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 TI-611-8 for details. All work In accordance with RRTAY611-8EMM 71-00-00-700-013-B02TEST No-9 Item: 6 Avionics Team Manager: Sean Brown Part/Model Customer Coordinator: Benny Rios AC Serial Nolan 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 S/N 256. Installed OVERHAULED unit P/N 622-9851-001 S/N 384. All work accomplished IAW GIV AMM 23-01-00. Refer to item 6.2. Billing Method Hours Rate Twat Labor USD: Time and Material ST 2.67 ® $127.00 $339.09 Parts USD: Time and Material $2,0I 2.00 Total USD: $2,351.09 Paris: Rel. 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 tom control, pin 622-9851-001, on order. Failed sin 256. Work done IAW 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 PIN 622-9851-001 S/N 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 13 of 23 Printed: 8/19/2015 1:08:28PI Rot EFTA01117762  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 14 of 23 Printed: 8/19/2015 1:08:28P1 Rot EFTA01117763  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Discrepancy: 8.6 CMP GIV 324014 Main Gear Wheel Assembly (Right, Oil t Ima rd No. 4) - 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: 8.8 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 flours 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. I was found between pins I and 2. P.O.O. Work done IAW CIV M/N1 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 15 of 23 Printed: 8/19/2015 1:08:28P1 ;Ceti EFTA01117764  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 16 of 23 Printed: 8/19/2015 I:08:28P1 Rot EFTA01117765  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: N/A 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 17 of 23 Printed: 8719/2015 1:08:28PI Rot EFTA01117766  Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002256 Discrepancy: 10.3 Parts moved for MLG tires. Resolution: C/W Billing Method flours 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