EFTA00609734.pdf

Gulfstreant DYNAMISM• COMPANY PRELIMINARY INVOICE ParUModel #: GIV AC Serial No./Tail No.: 1085 / N423TT Bldg C.-FAX - West Paint Beach. Florida 33406 Mail Remittance To: Overnight Remiaance To: Wire Remittance To: Gulfstream Aerospace Corporation Gulfstream Aerospace Corporation (Box # 730349) Gulfstream Aerospace Corporation P.O. Box 730349 Go 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 Routing No. S.W.I.F.T. ACII Credit Routing No. ( Invoice Number. Bill To: JEGE, INC. Invoice Date: 3800 SOUTHERN BLVD Customer ID: SUITE 204 P.O. Number. WEST PALM BEACH, Florida 33406 Repair Station: FAA CRS PB8R624N United States In Date: 04/01/2013 Out Date: 04/22/2013 Payment Type: Net 30-Open terms Payment Terms: Title: JEGE, INC. INVOICE SUMMARY FOR WORK ORDER NUMBER: SC13175 Time & Materials Flat Raw Total Labor USD: $23,939.84 $74,150.00 $98,089.84 Parts USD: $196,307.51 $0.00 $196,307.51 Services USD: $1,547.68 $0.00 $1,547.68 Detail Subtotal USD: $221,795.03 $74,150.00 $295,945.03 Subtotal USD: $295.945.03 Funds on Deposit USD: 50.00 Total USD: $295,945.03 Pre Test Flight Times /Cycles Airframe 8563.8 Hrs 3963 Lds Eng #1 8508.1 TSN 3929 CSN Eng #2 8528.0 TSN 3935 CSN Post Test Flight Times / Cycles Airframe 8567.0 Hrs 3964 Lds Eng #1 8511.3 TSN 3930 CSN Eng #2 8531.2 TSN 3936 CSN For detail description of the work complied with see the Work Order Detail report. Unless otherwi indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rm Page 1 of 57 Printed: 4/18/2013 11:38:51Ali Ftst X EFTA00609734  Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Item: 1 Airframe Gulfstream GIV Scheduled N423TT Team Manager: Sean Brown Pan/Model GIV Customer Coordinator: Ray Kraber AC Serial No./Tail No.: 1085 / N423TT TSN/TSO: CSN/CSO: 3,964 Aircraft Time: 8,567.0 Discrepancy: 1.1 Return to Service EJM (10 or More) Resolution: ACTT: 8,563.8 LNDS: 3,963 DATE: April XX, 2013 Completed (INSERT TITTLE) inspection accordance with EJM (INSERT AIRCRAFT TYPE) Continuous Airworthiness Maintenance Program, EJNI Maintenance Procedure Manual and 14 CFR 135.411 (a)(2) and is approved for return to service. Authorized RTS Signature Thomas J. Choynowski, Sr. Airworthiness Inspector For; Gulfstream West Palm Beach, FL 33406 FAA CRS PB8R624N Discrepancy: 1.2 Inbound/Outbound Inspection Resolution: Complied with Inbound / Outbound Inspections. Labor USD: No Charge N/ C Step: 1.2.1 Completed Inbound/Preliminary Inspection Step: 1.2.2 Waiting Outbound Inspection approval (L) Discrepancy: 1.3 Preflight Inspection Resolution: N/A Discrepancy: 1.4 Comply with Debrief Checklist For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 2 of 57 Printed: 4/18/2013 11:38:51.41 Rd X EFTA00609735  Bill To: JEGE,INC. WO8: SC13175 Invoice Number: Resolution: N/A Step: 1.4.1 Completed Arrival/Debrief 90 Day Due List Review Accomplished. Step: 1.4.2 Completed List Operator's Airworthiness Requirements & Special Documentation Requests. Step: 1.4.3 Completed Review Technical Operations Update prior to return to service for newly released bulletins and advise operator. Discrepancy: 1.5 Tool Clearance Resolution: All tooling removed from aircraft. Discrepancy: 1.6 Cover & Protect Resolution: Protected aircraft as required for MX as required. Labor USD: No Charge N/ C Discrepancy: 1.7 Service Chemical Toilet/('lean Galley Resolution: N/A Discrepancy: 1.8 ArrivaUDeparture Assist & Video Aircraft Resolution: C/W as required. Discrepancy: 1.9 Sample Hydraulic Fluids Resolution: Sampled Hydraulic Fluids a required. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 3 of 57 Printed: 4/18/2013 11:38:51A) Ftst X EFTA00609736  Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 1.10 Remove Valuables & Secure. Resolution: Discrepancy: 1.11 Comply with Service Team Manager Checklist Resolution: Labor USD: No Charge N/ C Discrepancy: 1.12 Fluids Used (Oils/Skydrol) - (Materials Only) Resolution: Billed Fluids Used (OiLs/Skydrol) - (Materials Only) as required. Discrepancy: 1.13 STM / Quality review of work order and logbook entry prior to departure Resolution: Labor USD: No Charge N/ C Discrepancy: 1.14 Towing (Does not include Hangar Moves) Resolution: Towed as required for MX. Billing Method Hours Rate Total Labor USD: Time and Material ST 4.50 @ $118.00 $531.00 Total USD: $531.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WodcOrderPreliminarylnvoicespt Page 4 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA00609737  Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 1.15 HazMat - Identify & provide a manifest, and a Shipper's Declaration for Dangerous Goods for all hazardous materials that are loaded aboard any aircraft. FAR Part 121 or 135 Operators will provide a hazardous material notification letter required by FAR 135.505 (e) prior to maintenance at this Repair Station iaw FAR 145.206 (a) (b). If there is to be loading of hazardous materials it shall be complied with by Hazmat trained authorized GDAS-PBI personnel only. Resolution: NM --- No Hazmat onboard aircraft at this time. Discrepancy: 1.16 Aircraft Cleaning Resolution: NM Discrepancy: 1.17 Billable Consumables & Shop Supplies Resolution: Billed for Shop Supplies and Consumables as required for MX. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WoikOrderPreliminarylnvoicespt Page 5 of 57 Printed: 4/18/2013 11:38:5 Ftst X EFTA00609738  Bill To: JEGE,INC. WO It: SC13175 Invoice Number: Discrepancy: 1.18 Major Alterations regulatory compliance requirements to be completed by installer as indicated on FAA form 8110-3. Copy and paste from attached statements as needed and edit as required. COMPLY WITH REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d). COMPLIED WITH THE REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d), via GROUND TEST REPORT-REPORT No. CEXXXXXXXX REV. X, ( IN SUPPORT OF STC XXXXXXXXX ) and GR4R216M REPAIR STATION INTERFERENCE TESTING REQUIREMENTS POST MAJOR ALTERATIONS COMPLIANCE FORM. COMPLY WITH REQUIREMENTS OF FAR 25.1529, INSTRUCTIONS FOR CONTINUED AIRWORTHINESS. REF XXXXX MANUAL, P/N XXXXXXX REV. X, FOR INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AND BLOCK 8 OF FAA FORM 337, DATED XX/XX/XXXX. COMPLY WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01.04 AND FAR 25.1353 (B) COMPLIED WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01.04 AND FAR 25.1353 (B) BY ENSURING ROUTING WAS IN ACCORDANCE AC43.13-1B, CHANGE 1 CHAPTER 11, SECTION S. Resolution: NM Discrepancy: 1.19 Update Weight & Balance Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 6 of 57 Printed: 4/18/2013 11:38:5IAD Rd X EFTA00609739  Bill To: JEGE,INC. WO SC13175 Invoice Number: Discrepancy: 1.20 Exterior Paint and Weight & Balance Requirements. Review scope of aircraft exterior paint touch-up/repairs, and skin replacements resulting in paint reapplication, and determine affect on weight and balance. For surfaces where paint is stripped and reapplied or added on top of existing paint on an area greater than 36 square feet the thickness values will be documented before and after painting . If average thickness values remain the same, weight and balance revision is not required. For surfaces painted with an area greater than 36 square feet and before and after paint thickness average varies, QC review for possible weight and balance revision will be required. * Thickness will be plotted on an aircraft drawing derived from AMM chapter 6 or other suitable sketch, attached to the work order and measurements taken on a two square foot grid. * Reference CAMPS 4000, paragraph 3.5.1 for paint restrictions to flight control surfaces and RVSM certified aircraft. * Reference CAMPS 4000, total average thickness shall not exceed 6 mils. * Per GAC Mass Properties Engineering, paint thickness of 5 mils equals .055 pounds per square foot. * If after QC review, weight change is greater than 2 pounds or .05% of MAC, the weight and balance report will require recomputation. Resolution: N/A Discrepancy: 1.21 "Advise customer of preservation requirements per ATA Chapter 10 of the relevant maintenance manuals for Airframe, Engines, and APU; review requirements in relation to scheduled Date Promised and later potential Date Completed; and perform maintenance or preservation actions as directed by the customer and documented as a Work Order Squawk. Resolution: N/A Item: 6 Avionics Team Manager: Sean Brown Pan/Model Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,567.11 / 3,964 Discrepancy: 6.1 RH wing emergency light inop Resolution: Removed defective bulb RH wing emergency light P/N GE303 nsn. Installed new bulb RH wing emergency light P/N GE303 nsn. Op's check good. All work was done JAW Gulfstream GIV AMM 33-10-01. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 7 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA00609740  Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Billing Method Hours Rate Total Labor USD: Time and Material ST 4.25 @ $118.00 $501.50 Pans USD: Time and Material $28.57 Total USD: $530.07 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 6.1 #1 303 LAMP 1 $1.75 $1.75 6.1 #2 PRI440-B-1/2 SEALANT, PRC,CARTRIDGE 1 $26.82 $26.82 Discrepancy: 6.2 While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #1 HF system does not transmit. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 2.25 @ $118.00 $265.50 Total USD: $265.50 Step: 6.2.1 Completed Verified discrepancy, performed HF press to test on #1 HF control head and received codes 19, 27. and 28 with the RT light illuminated. Hi' receives the Intl clock very clear. When the Press to Talk switch is pressed with the #1 HF system, Fault code 08 appears on the control head with the UP lamp illuminated. Further troubleshooting required at this time. All work performed 1AW G-IV maintenance manual 23-03-00. Discrepancy: 6.3 While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #2 HF system produces a power surge when press to talk is pressed that causes the external AC power cart to shut down. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 0.75 @ $118.00 $88.50 Total USD: $88.50 Discrepancy: 6.4 While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #1 Auto Throttle reports Excessive Friction and Servo Current Failures when tested. Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 8 of 57 Printed: 4/18/2013 11:38:51A) Rd X EFTA00609741  Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 6.5 While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #2 Auto Throttle reports Servo Current Failure. Resolution: Discrepancy: 6.6 Performe Cockpit bulb sweep. While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the E-Batts switch capsules just left of the co-pilots yoke are partially loop. Also noted that theupper half of the first digit on the Differential Pressure Guage is out. The upper half of the Radar Stab IRU select switch just forward of the IRU MSU are loop. Resolution: Discrepancy: 6.7 Squawk from flight test - Standby fuel gauge totalizer is indicateing 2001bs lower than the LT and RT fuel gauges and there is a 150lbs difference between total fuel on EICAS primary and systems page compared to STBY totalizer gauge - EICAS and SYSTEMS page ind same Resolution: Step: 6.7.1 Waiting While deluding aircraft noticed that EICAS read 27501bs It and rt and 54001bs total and approval (L) standby ind read 27501bs It and rt but 44001bs total. The standby ind LOW FUEL light came on with 26001bs It and rt(suppose to be 6501bs). Discrepancy: 6.8 Squawk from flight test • LED light burned out on Rate of Climb / FPM (3 digit from LT) on pressurization controller Resolution: Discrepancy: 6.9 Squawk from flight test - With both engines and APU running and both converters on DC volts on the Right-Left-AUX or ESS selected indicate 47.8VDC Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 9 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA00609742  Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 6.10 Squawk from flight test - At FL250 with Batteries only, DC volts on ABEX fluctuates 36.9 to 47.9 v Resolution: Discrepancy: 6.11 Squawk from flight test - RTU 1 there is a cyan line across display on screen - splits screen in half Resolution: Discrepancy: 6.12 Squawk from flight test - On RNAV approach VNAN worked and then became unavailable on approach Resolution: Discrepancy: 6.13 Squawk from flight test - Standby engine instrument gauge is indicating all "88118"s on RT HP gauge Resolution: Discrepancy: 6.14 Squawk from flight test - HF radios operated normally but NO SELCAL Resolution: Discrepancy: 6.15 EGPWS/Terrain database outdated Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WodcOrderPreliminarylnvoicespt Page 10 of 57 Printed: 4/18/2013 11:38:5IAD Ftst X EFTA00609743  Bill To: JEGE, INC. WO ft: SC13175 Invoice Number: Discrepancy: 6.16 Squawk from flight test - aft LAV reading light is Mop Resolution: Discrepancy: 6.17 Squawk from flight test - cabin management display at VIP , galley screen Mop Resolution: Discrepancy: 6.18 Squawk from flight test - perform ops test of nose camera Resolution: Discrepancy: 6.19 Satphone is inop Resolution: Item: 7 Interior Team Manager: Sean Brown Pan/Model 0: Customer Coordinator: Ray Kraher AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 7.1 Squawk [ruin flight test - FWD LAV water does not pump Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page I I of 57 Printed: 4/18/2013 11:38:5IAli Rd X EFTA00609744  Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Discrepancy: 7.2 Squawk from flight test - LH galley aft cutting board does not latch Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 0.87 @ $118.00 $102.66 Pans USD: Time and Material $1.86 Total USD: $104.52 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 7.2#1 MINI-LATCH SELBY-LATCH WHITE NICKEL 1 $1.86 $1.86 Step: 7.2.1 Completed Removed galley drawer and galley latch. All work performed IAW GIV MM 25-20-00. Discrepancy: 7.3 Squawk from flight test - RH #5 window shade does not fully close Resolution: Discrepancy: 7,4 Squawk from flight test - pax air gaspers loose, takes two hands to close the outlet Resolution: Discrepancy: 7,5 Squawk from flight test - fwd cabin door angle wing does not hit headliner when closed. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 2.10 @ $118.00 $247.80 Total USD: $247.80 Step: 7.5.1 Waiting Removed fwd pocket door, inspected pop-up door closeout mechanics, found no defects Insp at this time, lubricated mechanical areas as required, re-installed fwd door and pop-up door closeout still would not fully close. Further evaluation is needed. All work performed IAW GIV MM 25-20-00. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 12 of 57 Printed: 4/15/2013 11:38:5IA) Ftst X EFTA00609745  Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Item: 8 Mechanical Team Manager: Sean Brown Pan/Model #: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 8.1 The No. 1 engines Outboard igniter plug is worn Resolution: Remove engine #1 ignitor plug #2 P/N Y183-5 S/N 1204. Instaled new engine #1 ignitor plug #2 P/N Y183-5 S/N 12047184. JAW RR EMM 74-21-03. Parts USD: No Charge N/C Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.1 #1 Y183-5 PLUG, IGNITOR 1 $0.00 $0.00 Discrepancy: 81 The No. 2 engines Outboard igniter plug is worn Resolution: Remove Engine #2 ignitor #2 P/N Y183-5 S/N 0601749. Installed new Engine #2 ignitor #2 P/N Y183-5 S/N 12047194. JAW RR EMM 74-21-03. Parts USD: No Charge N/C Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.2 Y183-5 PLUG, IGNITOR 1 $0.00 $0.00 Discrepancy: 8.3 The Left engine S/N 16291, No.8 combustion liner has a 1.8" crack and part of the crossover tube shroud is missing. Pictured sent to rolls royce. Resolution: With further investigation on the No.8 combution liner on the left engine S/N 16291, found the cranks to be within limits JAW the Rolls Royce TAY611-8 EMM chapter 71.00.00, and no further action is needed. With further investigation found the crossover tube to only have minor errosion and some carbon build up No further action is required on this item. All work performed JAW the Rolls Royce TAY611.8 EMM chapter 71.00.00. Discrepancy: 8.4 The Right engine S/N 16292, No.4 combustion liner has 4 cracks. (1.0", 3.2", 4.0", and 5.6") and over 30 HPT stage one bases LE cracked. Pictured sent to rolls royce. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 13 of 57 Printed: 4/18/2013 11:38:51A? Ftst X EFTA00609746  Bill To: JEGE,INC. WO #: SC13175 Invoice Number: Resolution: With further investigation of the No.4 combution liner of the right engine S/N 16292 found the cracking to only be 25% of what was originally determined. Total circumferential cracking was found to be less than 40% and no further special inspections will be needed for this item. All work was performed JAW the Rolls Royce TAY611-8 EMM chapter 71.00.00. Two HPT stage 1 Blade tips was found to be cracked on the LE with the crack protruding into the airfoil 0.050" (1.25mm). All work was performed IAW the Rolls Royce TAY611.8 EMM Task 71.00.00.210.001 (9)(a)(iii). Re-Inspect the blades within 400 hours (8,928.0 TSN) or 400 cycles (4,335 CSN) whichever occurs first. This crack can protrude into the airfoil up to a length of 0.315" (8.00 mm) Discrepancy: 8.5 Squawk from flight test - rubber stripping on leading edge of LT and RT MLG doors are torn Resolution: Removed damaged sections of rubber seal P/N GASl3AN-1.41from around L/H and R/H MLG bays, and installed new seal P/N GAS13AN-1-41 I/A/W GIV AMM 20-42-00 Billing Method Hours Rate Total Labor USD: Time and Material ST 2.08 @ $118.00 $245.44 Pans USD: Time and Material $109.18 Total USD: $354.62 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.5 #1 GASl3AN-1.41 SEAL, BUTTONED STRIP, WHEEL I $109.18 $109.18 WELL DOOR (5' SECTION) Discrepancy: 8.6 Squawk from flight test - Copilots seat is difficult to move in fore-aft position Resolution: Removed copilot seat and inspected seat track and rollers. Found no defects. Lubed seat track and rollers. Moved seat fore and aft with satisfactory results. Reinstalled copilot seat. Ref: GIV ALUM 25-11.00. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.00 @ $118.00 $236.00 Total USD: $236.00 Discrepancy: 8.7 Squawk from flight test - Gear emergency reset handle not safetied (D-ring) Resolution: Safetied Gear Emergency Reset Handle (D-ring) IAW GIV AMM 32-00-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.70 @ $118.00 $200.60 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WoikOrderPreliminarylnvoice.rpt Page 14 of 57 Printed: 4/18/2013 11:38:5 IAD Rd X EFTA00609747  Bill To: JEGE, INC. WO 9: SC13175 Invoice Number: Total USD: $200.60 Discrepancy: 8.8 Squawk front flight test - Flaps shudder felt when flaps selected to 39 degrees Resolution: Discrepancy: 8.9 Squawk from flight test - screw needs tightening on panel behind pilots seat below CB panel Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 0.50 @ $118.00 $59.00 Total USD: $59.00 Discrepancy: 8.10 Squawk from flight test - on the ground the flaps would intermittenly move from 20 to 39 degrees and 10 to 20 when selected. Resolution: Billing Method flours Rate Total Labor USD: Time and Material ST 20.92 @ $118.00 $2,468.56 Total USD: $2,468.56 Discrepancy: 8.11 Squawk from flight test - power levers have 1/2 knob split at 15000ft and 80%HP (It lever is fwd) Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 15 of 57 Printed: 4/182013 11:38:51A) Rd X EFTA00609748  Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 8.12 Squawk from flight test - while climbing through FL 430 with LT Pack OFF the RT Pack was 25psi (should be 27-33psi) Resolution: Discrepancy: 8.13 Squawk from flight test - while climbing through FL 430 with RT Pack OFF the LT Pack was 23psi (should be 27-33psi) Resolution: Discrepancy: 8.14 Squawk from flight test - One O2 mask in LAV and LT and RT AFT rear did not drop during test Resolution: Verified that aft left,aft right and lay oxygen masks would not deploy. Adjusted mask lid holding spring clips on all 3 mask boxes. Performed funtional check of the 3 locations. Ops checked good. No further defects noted. Billing Method Hours Rate Total Labor USD: Time and Material ST 4.36 @ $118.00 $514.48 Total USD: $514.48 Discrepancy: 8.15 Squawk from flight test - service hydraulic replenisher Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 1.20 @ $118.00 $141.60 Pans USD: Time and Material $319.92 Total USD: $461.52 Parts: Ref. No. P:nt number: Description Quantity Sell price USD Extended USD 8.15 500B4QT SKYDROL OIL IN QUART CANS 6 $53.32 $319.92 Discrepancy: 8.16 Squawk from flight test - At FL400 and climbing, RT engine MCI' was 1.79 but could only indicate 1.78 before LP RPM has an exceedance Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 16 of 57 Printed: 4/18/2013 11:38:5 IA) Rd X EFTA00609749  Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Discrepancy: 8.17 While compling with APU GTCP36.100(G) Borescope the following was found. The plenum is cracked, the nozzle guide vane TE's are erroded and cracked, and the turbine wheel tips are erroded. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 1.47 @ $118.00 $173.46 Services USD: No Charge N/ C Total USD: $173.46 Services: Ref. No. Description Quantity Sell Price USD Extended USD 8.17 #1 REPAIR 1.00 $0.00 $0.00 Part Ref: GTCP36-100G APU (3800062-9-1) Step: 8.17.1 Completed Removed APU generator P/N I1598CAV373-105 SIN 129A0171 I/A/W G1V AMM 24-01-01 and sent APU out for repair. Discrepancy: 8.18 While tightening screw for squawk 8.9 found that the inboard metal protector (located on panel behind copilots seat) for the coplilots seat is bent and is cutting into copilot seat back rest. Resolution: Billing Method flours Rate Total Labor USD: Time and Material ST 1.50 @ $118.00 $177.00 Total USD: $177.00 Discrepancy: 8.19 Squawk from flight test - There is a soft spot in floor hoard just fwd of fwd LAV (feels like blowout panel isnt secure) Resolution: Removed broken clip P/N 159B10732-13 from blowout panel forward of forward lay and replaced with new clip P/N 159B10732-13 IAW GAC Drawing 159B10732. Billing Method flours Rate Total Labor USD: Time and Material ST 4.91 @ $118.00 $579.38 Pans USD: Time and Material $86.10 Total USD: $665.48 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryinvoicespt Page 17 of 57 Printed: 4/18/2013 I I:38:51AP Flet X EFTA00609750  Bill To: JEGE, INC. WO #: SC13175 Invoice Number: Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.19 NI 159B10732-13 SPRING CLIP 2 $43.05 $86.10 Discrepancy: 8.20 Evaluate flaking paint from steel doubler and adjacent structure on L/H horizontal stab at panel 38-UPR-4. Ref to sqk 15.25 Resolution: Cleaned suspect area and after further evaluation found no defects. No further action required. Work perfromed JAW GIV SRM 51.13.00. Billing Method Flours Rate Total Labor USD: Time and Material ST 3.40 @ $118.00 $401.20 Total USD: $401.20 Discrepancy: 8.21 While working sqk 15.26 CMP 551024. Found corrsion and pitting horizontal stabilizer skin at panel 38-UPR-5. Resolution: Removed minor surface corrosion and pitting from panel opening mounting flange of panel 38-UPR-5, cadmium plated exposed surface and applied coat of primer. All work done IAW GIV SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST