EFTA01117701

Gulfstreant AO CVNAMICA 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 M 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. Ft. Worth, TX 76155 Fedwire Routing No. (ABA S.W.I.F.T. ACH Credit Routing No. (ABAJ I Invoice Number. 7113001425 Bill To: TRT LEASING Invoice Date: 4/18/2013 505 S FLAGLER DRIVE, #700 Customer ID: BT113 WEST PALM BEACH, Florida 33414 P.O. Number: United States Repair Station: FAA CRS PB8R624N In Date: 04/01/2013 Out Date: 04/26/2013 Payment Type: Net 30-Open terms Payment Terms: Title: TRT LEASING INVOICE SUMMARY FOR WORK ORDER NUMBER: SC13175 Time & Materials Flat Rate Total Labor USD: $50361.15 $1,207.50 $51,568.65 Parts USD: $158,612.26 $2,097.32 $160,709.58 Services USD: $1,600.00 $0.00 $1,600.00 Detail Subtotal USD: $210,573.41 $3,304.82 $213,878.23 Subtotal USD: 5213.878.23 Funds on Deposit USD: S0D0 Total USD: $213,878.23 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 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117701 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Item: I Airframe Gulfstream GIV Scheduled N423TT 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: 1.22 Billable Consumables & Shop Supplies Resolution: To be billed as required. Billing Method Flours Rate Total Parts USD: Flat Rate $2,097.32 Total USD: $2,097.32 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 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 IAW Gulfstream G1V AMM 33-10-01. Billing Method Flours Rate Total Labor USD: Time and Material ST 4.25 @ $115.00 $488.75 Parts USD: Time and Material $28.57 Total USD: $517.32 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 6.1 #1 303 LAMP 1 $1.75 $1.75 6.1 #2 PRIM0-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: Performed HF Communication System No.1- Operational Check. No defects noted. All work performed LA.W. GIV M.M. 23-03-00. OW CMP-231114. 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 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117702 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Billing Method Flours Rate Total Labor USD: Time and Material ST 3.55 @ $115.00 $408.25 Total USD: $408.25 Step: 6.2.1 Completed Verified discrepancy, performed HF press to test on ttl HF control head and received codes 19, 27, and 28 with the RT light illuminated. HF 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 CP lamp illuminated. Further troubleshooting required at this time. All work performed lAW G-1V 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: With aircraft outside and APU running, called New York Radio on HF frequency 13.348. No failures found. Established a clear conversation with New York. No power surges noted. This work accomplished JAW 6400 AMM 23-03-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 3.75 @ $115.00 $431.25 Total USD: $431.25 Discrepancy: 6.4 While complying with CMP 231001 Avionics-Functional Ramp Testfin.spection found that the #1 Auto Throttle reports Excessive Friction and Servo Current Failures when tested. Resolution: While compling with engine run adjustments from items 8.11, 8.16, and 8.49 selected autothrottles on and off many times to check for knob splits and engine performance and had no defects noted at any time. No further action required. Work done I.A.W. GIV M.M. chap. 22-00.00. Billing Method flours Rate Total Labor USD: Time and Material ST 3.80 @ $115.00 $437.t)0 Total USD: $437.00 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_WorkOrderPreliminarylnvoiceipt Page 3 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117703 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Step: 6.4.1 Completed Tried to run up aircraft to run ops check and found that air data speed wouldn't go below 50. Aircraft would show maint test mode but no FGC maint blue cas would appear and maint would not appear on either DU. Checked for blockages in pitot but found none. Tried different configurations but couldn't get airspeed to drop below 50 as called out in CMP. Further troubleshooting required. All work done JAW GIV MM 22-00-00 Step: 6.4.2 Completed Verified discrepancy: Performed L Arr Servo -Functional test several times and a I AT fails test at step B. (16) ( AT 1 SERVO TEST ) RH Engine throttle lever seems to bind after travel to fall Fwd stop and on its way back it stops driving back then jumps back and makes a loud clunk when disconnects and displays Amber Excessive friction Cas Msg.. Performed Aff resistance servo ring out cheks good. Performed DC power servo output monitoring test, while .VI' are in test and moving they should maintain 7 to 8 Vdc while moving. At start of test voltage is good (8 Vdc) while throttles are moving towards Fwd stop and then on return trip RH throttle sticks and voltage drops to 3 Vdc and 1.H throttle continues to travel until RH throttle jumps and disengages & voltage jumps back up to 8 Vdc, and we get ( Amber Excessive friction Cas Msg ). Requested P & A of R11 AR Servo PIN-7009025.913, S/N-88080272. Awaiting customer approval. All work performed I.A.W. GIV M.M. 22-00-00 and CMP 223005. Discrepancy: 6.5 While complying with CMP 231001 Avionics-Functional Ramp TesUInspection found that the #2 Auto Throttle reports Servo Current Failure. Resolution: C/W CMP-223005 ( L Aff Servo-Functional Check. Could not duplicate or verify discrepancy at this time. All work performed I.A.W. GIV M.M. 22-00-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.42 0, $115.00 $163.30 Total USD: $163.30 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 OL 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. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.50 @ $115.00 $172.50 Parts USD: Time and Material $54.06 Total USD: $226.56 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 6.6 #1 OL3335 LAMP 10 $5.15 $51.50 6.612 GE387 BULB 2 $1.28 $2.56 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 4 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117704 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 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 150Ibs difference between total fuel on EICAS primary and systems page compared to STBY totalizer gauge - EICAS and SYSTEMS page ind same Resolution: Customer elects no further action at this time. Deferred IAW EJM GIV MEL 28-2-1 Category C Due 5.6.2013. "M" procedures complied with. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.75 @ $115.00 $201.25 Parts USD: No Charge N/ C Total USD: $201.25 Step: 6.7.1 Completed While deluding aircraft noticed that EICAS read 27501bs It and rt and 5400lbs total and standby ind read 27501bs It and rt but 44001bs total. The standby ind LOW FUEL light came on with 2600lbs It and rt(suppose to be 6501bs). Step: 6.7.2 Completed Verified discrepancy. Standby fuel indicator is bad PN: 1159SCP460-101. All work done IAW GIV MM 28-06-00 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 Billing Method Flours Rate Total Labor USD: Time and Material ST 130 @ $115.90 $172.50 Labor USD: Time and Material OT 015 @ $173.90 543.25 Total USD: $215.75 Step: 6.8.1 Completed Verified Discrepancy. Found lighting to be faulty on controller. PN: 1159SCF407-7. All work done IAW GIV MM 21-02-01 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: Customer elects no further action. Deferred IAW EJM GIV MEL 24-10-3 Category• C Due 5.6.2013 Billing Method Hours Rate Total Labor USD: Time and Material ST 3.00 @ $115.00 $345.00 Labor USD: Time and Material OT 015 @ $173.00 $43.25 Total USD: $388.25 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 5 of 35 Printed: 5/1/2013 4:33:33PF Ref: I: EFTA01117705 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Step: 6.9.1 Completed Checked on battery and found EPMP to be operating normally on external power cart. Needs to be checked on Engine. All work done IAW GIV MM 24-03-02 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. Billing Method Hours Rate Total Labor USD: Time and Material ST 4.75 @ $115.00 $546.25 Labor USD: Time and Material OT 0.62 @ $173.00 $107.26 Total USD: $653.51 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 FM selected in the EPMP. Further action required on this squawk when maintenance schedule provides Hydraulic cart to aircraft and/or outside engine runs. If DC Volts fluctuation is duplicated, avionics can compare the UC volts from the Pilots CB panel test ports. Performed this work IAW 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 IAW 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: 6.12 Squawk from flight test - On RNAV approach VNAV worked and then became unavailable on approach Resolution: Customer elects no further action. Deferred IAW EJM GIV MEL 34-34-6 Category C Due 5.6.2013 Billing Method Hours Rate Total Labor USD: Time and Material ST 4.25 @ $115.00 $488.75 Labor USD: Time and Material OT 0.25 @ $173.00 $43.25 Total USD: $532.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 6 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117706 Bill To: TRT LEASING WO #: SCI3175 Invoice Number: 7113001425 Step: 6.12.1 Completed Performed a VOR operational check. After several minutes of monitoring both VORI and VOR2, found VOR2 display to become intermittant. Swapped #1 and #2 Nay Receivers in nose equipment rack. The intermittant VOR display followed to the #1 VOR position. Swapped both Nay Receivers back to their original postions. Nay Receiver #2 is intermittant. Nav Receiver #2 P/N 622-7194-201 SIN 3647. Performed this work lAW GIV AMM 34-02-02. Discrepancy: 6.13 Squawk from flight test - Standby engine instrument gauge is indicating all "8888"s on RT HP gauge Resolution: Customer elects no further action. Deferred IAW EJM GIV MEL 77.1 Category C Due 5-6-2013 Billing Method Hours Rate Total Labor USD: Time and Material ST 1.00 @ $115.00 $115.00 Labor USD: Time and Material OT 0.25 @ $173.00 543.25 Total USD: $158.25 Step: 6.13.1 Completed Verified discrepancy. Found backlighting on three cells to display MS making cells appear to be inop. PN: I 159SCF412-11. All work done lAW GIV MM 77-14-00 Discrepancy: 6.14 Squawk from flight test HF radios operated normally but NO SELCAL Resolution: With aircraft outside and APU running, called New York Radio on HF #2 and requested a SELCAL call on FPEQ. The aircraft received SELCAL with no failures. SELCAL checks good. Performed this work IAW 6400 AMM 23.03-00 Billing Method Hours Rate Total Labor USD: Time and Material ST 1.25 @ $115.00 $143.75 Total USD: $143.75 Discrepancy: 6.15 EGPWSfferrain database outdated Resolution: Updated EGPWS/Terrain database to version 467 lAW Service Bulletin, ATA # 965.0976/1690-34-104 Publication # 012-0687-204and 965.1676.34.105 Publication # 012-0687-205. Service Letter Publication # EGPWS-MKV-MKVII-52. No defects noted. Billing Method flours Rate Total Labor USD: Time and Material ST 2.07 @ $115.00 $238.05 Total USD: $238.05 Discrepancy: 6.16 Squawk from flight test - aft LAV reading light is inop 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. 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 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117707 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Billing Method Hours Rate Total Labor USD: Time and Material ST 3.00 @ $115.00 $345.00 Parts USD: Time and Material $1.96 Total USD: $346.96 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 6.16 #1 1308 LAMP 1 $1.96 $1.96 Step: 6.16.1 Completed Verified discrepancy. Found bulb to be bad and also socket loose. All work done IAW GIV 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 IAW GIV AMM 33-00-00. Discrepancy: 6.17 Squawk from flight test - cabin management display at VIP , galley screen loop Resolution: Operator requested no further action be taken on this discrepancy. Deferred IAW EJM GIV MEL NEF 25-27 Billing Method Flours Rate Total Labor USD: Time and Material ST 0.15 @ $115.00 $17.25 Labor USD: Time and Material OT 0.10 @ $173.00 $17.30 Total USD: $34.55 Step: 6.17.1 Completed Verified discrepancy. Found panel to have faulty LCD display. PN: 101001-763 SN: 10307 All work done IAW GIV MM 25-00-01 Discrepancy: 6.18 Squawk from flight test - perform ops test of nose camera Resolution: Customer elects no further action. Deferred IAW EJM GIV MEL 25-16 Category D Due 8-24-2013 Billing Method Hours Rate Total Labor USD: Time and Material ST 2.25 @ $115.00 $258.75 Total USD: $258.75 Step: 6.18.1 Completed Verified discrepancy. Found camera not to have video at all monitors. Found PN: AVS100-50-28T-CH in CMP. Unknown what PN is on the camera. All work done lAW G1V MM 25-00-00 Discrepancy: 6.19 Satphone is loop Resolution: Operator requested no further action be taken on this discrepancy. Customer elects no further action. Deferred IAW EJM GIV MEL 23-8 Category D Due 8.24-2013 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 Page 8 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117708 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Labor USD: Time and Material ST 0.25 @ $115.00 $28.75 Total USD: $28.75 Item: 7 Interior Team Manager: Sean Brown ParVModel 0: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSNICSO: Aircraft Time: 8.567.0 / 3.964 Discrepancy: 7.1 Squawk from flight test - FWD LAV water does not pump Resolution: Customer elects no further action. Deferred LAW KIM GIV MEL 38-2 Category D Due 8-24-2013. "M" procedures complied with. Billing Method Flours Rate Total Labor USD: Time and Material OT 0.25 @ $173.00 $43.25 Total USD: $43.25 Discrepancy: 7.2 Squawk from flight test - LH galley aft cutting board does not latch Resolution: Removed L/H aft lower galley drawer, L/H 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. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.12 @ $115.00 $128.80 Parts USD: Time and Material $1.86 Total USD: $130.66 Pans: 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: Could not duplicate discrepancy , window shade operates normally as required.No further action taken at this time. 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_WorkOrderPreliminaryInvoice.rpt Page 9 of 35 Printed: 5/1/2013 4:33:33PF Ref: I: EFTA01117709 Bill To: TRT LEASING WO #: SCI3175 Invoice Number: 7113001425 Billing Method Flours Rate Total Labor USD: Time and Material ST 0.25 @ $115.00 $28.75 Total USD: $28.75 Discrepancy: 7.4 Squawk from flight test - pax air gaspers loose, takes two hands to close the outlet Resolution: Adjusted passenger air gaspers as required for proper operation IAW GIV MM 25-20-00. Ops. checks good. Billing Method Flours Rate Total Labor USD: Time and Material ST 0.25 @ $115.00 $28.75 Total USD: $28.75 Discrepancy: 7.5 Squawk from flight test - fwd cabin door angle wing does not hit headliner when closed. Resolution: Operator requested no further action be taken on this discrepancy. Deferred IAW EJM GIV MEL NEF 25-27 Billing Method Flours Rate Total Labor USD: Time and Material sr 2.10 @ $115.00 $241.50 Labor USD: Time and :Material OT 0.25 @ $173.00 $43.25 Total USD: $284.75 Step: 7.5.1 Completed Removed fwd pocket door, inspected pop-up door closeout mechanics, found no defects 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 lAW GIN' MM 25.20.00. Item: 8 Mechanical Team Manager. Sean Brown Part/Model #: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TS0: CSNICS0: 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. IAW RR EMM 74-21-03. Parts USD: No Charge NI C For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_Work0rderPreliminaryInvoicespt Page 10 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117710 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Pans: Ref. No. Pan number: Description Quantit • Sell price USD Extended USD 8.1 #1 Y183-5 PLUG, IGNITOR 1 $0.00 $0.00 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. Parts USD: No Charge N/ C Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.2 #1 Y183-5 PLUG, IGNITOR I $0.00 $0.00 Discrepancy: 83 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 IAW 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. 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 IAW 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 TAY6I1-8 EMM Task 71.10.10.200.001 (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 GAS13AN-1-41from around L/H and R/H MLG hays. and installed 1104 seal P/N GAS13AN-1-41I/A/W GIV AMM 20-42-00 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 I I of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117711 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Billing Method Flours Rate Total Labor USD: Time and Material ST 2.08 @ $115.00 $239.20 Parts USD: Time and Material $109.18 Total USD: $348.38 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 83 #1 GASI3AN-1-41 SEAL, BUTTONED STRIP, WHEEL 1 $109.18 $109.18 WELL DOOR (5' SECTION) Discrepancy: 84 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. Luhed seat track and rollers. Moved seat fore and aft with satisfactory results. Reinstalled copilot seat. Ref: GIV AMM 25.11.00. Billing Method Flours Rate Total Labor USD: Time and Material ST 2.00 @ $115.00 $230.00 Total USD: $230.00 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 Flours Rate Total Labor USD: Flat Rate $57.50 Total USD: $57.50 Discrepancy: 8.8 RII - Squawk from flight test - Flaps shudder felt when flaps selected to 39 degrees Resolution: RH - 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. Billing Method Howl Rate Total Labor USD: Time and Material ST 4.27 @ $115.00 $491.05 Labor USD: Time and Material OT 0.07 @ $173.00 512.11 Total USD: $503.16 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 12 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117712 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Discrepancy: 8.9 Squawk from flight test - screw needs tightening on panel behind pilots seat below C/B panel Resolution: REF 8.18. Tightened screw as required IAW GIV SRM 51.41.00. Billing Method Hours Rate Total Labor USD: Time and Material ST 0.50 @ $115.00 $57.50 Total USD: $57.50 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. Billing Method Flours Rate Total Labor USD: Time and Material ST 30.59 @ $115.00 $3,517.85 Labor USD: Time and Material OT 0.07 @ $173.00 $12.11 Total USD: $3,529.96 Discrepancy: 8.11 Squawk from flight test - power levers have 1/2 knob split at 15000ft and 80%HP (It lever is fwd) Resolution: RII Item / Adjusted LH engine throttle rigging as required to correct knob split IAW GIV MM 71.00.00. No defects noted.Ops checks good on ground run up. Updated CMP 732002, 732012. Billing Method Flours Rate Total Labor USD: Time and Material ST 11.00 @ $115.00 $1,265.00 Labor USD: Time and Material OT 0.22 @ $173.00 $38.06 Total USD: $1,303.06 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 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117713 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 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. LAW GIV AMM 36-01-01. C/W CMP 361008 Bleed Air System R/H Operational Test. Ops and leak check is good. No discrepancies noted at this time. All work I.A.W. GIV M/M 36-00-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 12.25 @ $115.00 $1,408.75 Parts USD: Time and Material $837.04 Total USD: $2.245.79 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.12 #1 S8990-114 SEAL 2 $0.52 $1.04 8.12 02 856504-5 FILTER 2 $418.00 $836.00 Step: 8.12.1 Completed C/W CMP 361007 Bleed Air System LAi Operational Test. No discrepancies noted at this time. All work I.A.W. GIV M/M 36-00-00. 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: 856514.5 and installed new P/N: 856504-5 filter. LAW GIV AMM 36.01.01. C/W CMP 361007 Bleed Air System L/H Operational Test. Ops and leak check is good. No discrepancies noted at this time. All work I.A.W. GIV NUM 36.00.00. Billing Method Flours Rate Total Labor USD: Time and Material ST 7.75 @ $115.00 $891.25 Labor USD: Time and Material OT 0.40 @ $173.00 $69.20 Total USD: $960.45 Step: 8.13.1 Completed CAW CMP 361008 Bleed Air System RAI Operational Test. No discrepancies noted at this time. All work I.A.W. GIV M/M 36-00-00. Discrepancy: 8.14 Squawk from flight test • One O2 mask in LAI, 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 Flours Rate Total Labor USD: Time and Material ST 11.86 @ $115.00 $1,363.90 Total USD: $1,363.90 Discrepancy: 8.15 Squawk from flight test - service hydraulic replenisher 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 35 Printed: 5/1/2013 4:33:33PF Ref: I: EFTA01117714 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Resolution: Filled hydraulic replenisher tank with skydroll VA/W GIV AMM 12.01.05 Billing Method Flours Rate Total Labor USD: Time and Material ST 1.20 @ $115.00 $138.00 Parts USD: Time and Material $319.92 Total USD: $457.92 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.15 #1 500B4QT SKYDROL OIL IN QUART CANS 6 $53.32 $319.92 Discrepancy: 8.16 Squawk from flight test - At FL400 and climbing, RT engine MCT was 1.79 but could only indicate 1.78 before LP RPM has an exceedance Resolution: RII Item / Performed Airflow Control System - Test. Adjusted RT airflow control regulator and actuator as required. Ops test is good no defects noted IAW RR TAY611.8 MM 71.00.00. This updates CMP 750006. Billing Method Flours Rate Total Labor USD: Time and Material ST 19.25 @ $115.00 $2,213.75 Total USD: $2.213.75 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. Billing Method flours Rate Total Labor USD: Time and Material ST 14.14 @ $115.00 $1,626.10 Labor USD: Time and Material OT 0.12 @ $173.00 $20.76 Parts USD: Time and Material $1,113.88 Total USD: $2,760.74 Pans: Ref. No. Pan number: Descri ion Quantity Sell price USD Extended USD 8.17 #1 AM590415.6 NUT 6 $16.48 $98.88 8.17 #2 1595443-1 VESTIBULE INSERT I $1,015.00 $1,015.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 15 of 35 Printed: 5/1/2013 4:33:33PF Ref: I: EFTA01117715 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Step: 8.17.1 Completed Removed APU generator P/N 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: 8.18 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: Removed metal protector, flatened to remove bend and reinstalled metal protector as required IAW GIV SRM 51.70.00. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.50 @ $115.00 $172.50 Total USD: $172.50 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 159810732.13 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 @ $115.00 $564.65 Parts USD: Time and Material $86.10 Total USD: $650.75 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.19 #1 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 IAW GIV SRM 51-13-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 3.40 @ $115.00 $391.00 Total USD: $391.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 16 of 35 Printed: 5/1/2013 4:33:33PF Ref: I: EFTA01117716 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Discrepancy: 8.21 While working sqk 15.26 CMP 551024. Found corrsion and pitting horizontal stabilizer skin at panel 3S-I'PR-S. Resolution: Removed minor surface corrosion and pitting from panel opening mounting flange of panel 38-UPR-S, cadmium plat e tl exposed surface and applied coat of primer. All work done IAW GIV SRM 51-13-10. Billing Method Flours Rate Total Labor USD: Time and Material ST 9.58 @ $115.00 $1,101.70 Total USD: $1,101.70 Step: 8.21.1 Completed Nlechanicaly removed minor surface corrosion and pitting front panel opening mounting flange and cadmium plated exposed surface. All work done 1AW GIV SRM 51.13.10. Discrepancy: 8.22 While working sqk 15.26 CMP 551023. Found corrsion and pitting horizontal stabilizer skin at panel 39-UPR-5. Resolution: Removed minor surface corrosion and pitting from panel opening mounting flange of panel 39-UPR-S, cadmium plated exposed surface and applied coat of primer. All work done IAW GIV SRM 51-13.10. Billing Method Flours Rate Total Labor USD: Time and Material ST 8.58 @ $115.00 $986.70 Labor USD: Time and Material OT 0.82 @ $173.00 $141.86 Total USD: $1,128.56 Step: 8.22.1 Completed 1Mechanicaly removed minor surface corrosion and pitting front panel opening mounting flange and cadmium plated exposed surface. All work done IAW GIV SRM 51-13-10. Discrepancy: 8.23 RII - While working CMP 551023 sqk 15.25. Found horizontal stab thrust blocks to be worn out of limits. Resolution: Added .014" 2024-T3 shim to horizontal stabilizer rub block on RH side to have a .013" gap on each side of horizontal stabilizer to vertical stabilzer rub block. Work done IAW GIV M.M. chapter 55.10-00, and GIV CMP# 551001, step C-13 (lin to C-14. Billing Method Flours Rate Total Labor USD: Time and Material ST 9.03 @ $115.00 $1,038.45 Labor USD: Time and Material OT 0.07 @ $173.00 $12.11 Total USD: $1,050.56 Step: 8.23.1 Completed Added .014" 2024-T3 shim to horizontal stabilizer rub block on RH side to have a .013" gap on each side of horizontal stabilizer to vertical stabilzer rub block. Work done lAVt. GIV M.M. chapter 55.10.00, and GIV CMP# 551001, step C-13 thru to C-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_Work0rderPreliminaryInvoice.rpt Page 17 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117717 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Discrepancy: 8.24 #2 Engine EPR Flex line chaffing against fixed cowl. (Flagged) Resolution: Adjusted orientation of #2 Engine EPR Flex Line IAW GIV AMM 77-01-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 3.28 @ $115.00 $377.20 Total USD: $377.20 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. Billing Method Flours Rate Total Labor USD: Time and Material ST 3.55 @ $115.00 $408.25 Parts USD: Time and Nlatcrial $514.56 Total USD: $922.81 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.25 #1 AS12847 CLAMP 12 $18.54 $222.48 8.25 #2 AS12817 CLAMP 12 $9.79 $117.48 8.25 #3 AS12816 CLIP 5 $16.36 $81.80 8.25 #4 AS12846 CLIP 5 $18.56 $92.80 Step: 8.25.1 Completed Removed 12 corroded clamps P/N AS12847 and ASI2817 and S 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 TAY6II-8 MM 71-00-00. Discrepancy: 8.26 While performing wing HI-lite Collar (left) inspection CMP code 571011 found collar cracked at LBL 44.0 Resolution: Removed cracked HI-lite Collar at LBL 44.0, and installed new Coller P/N HST70-8. All maintenance performed IAW Gulfstream GIV ASC 446 AM1. Billing Method flours Rate Total Labor USD: Time and Material ST 0.47 @ $115.00 $54.05 Total USD: $54.05 Discrepancy: 8.27 While gaining access to cracked Hi-Lite Collar at LBL 44.0 found fasteners wet with hyd fluid at top of wing box section left and right of BL-0 Resolution: Tightened HYD lines at LBL 20 as required per GIV MM 20-70-10. No defect was noted. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 18 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117718 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Billing Method Flours Rate Total Labor USD: Time and Material ST 9.03 @ $115.00 $1,038.45 Total USD: $1,038.45 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. Billing Method Flours Rate Total Labor USD: Time and Material ST 632 @ $115.00 $726.80 Parts USD: Time and Material $116.32 Total USD: $843.12 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.28 #1 D10036D06 UNION. PERMASWAGE 1 $51.50 $51.50 8.28#2 D10036D06 UNION. PERMASWAGE 1 $51.50 $51.50 8.28 #3 6061T6-.375X.028 TUBING, ALUMINUM-3/8 2 $6.66 $1332 Step: 8.28.1 Completed Cut and removed 6" section with dent from fuel line P/N: I159P42012-022FP6 at RBS255.5 of RAI wing. Spliced in new 6" section of tubing on fuel line P/N:1159P42012-022FP6 at RI35255.5 of R/H wing. All work done lAW CAMPS 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 .012in. 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 Billing Method Flours Rate Total Labor USD: Time and Material ST 4.50 @ $115.00 $517.50 Labor USD: Time and Material OT 0.02 @ $173.00 $3.46 Parts USD: Time and Material $38,000.00 Total USD: $38,520.96 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.29 #1 1159SCC212-15 ACTUATOR.FLAP DRIVE, L- 1 $38,000.00 $38,000.00 OUTBOARD 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 19 of 35 Printed: 5/1/2013 4:33:33PF Ref: I: EFTA01117719 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 71/300/425 Step: 8.29.1 Completed Remove worn LH actuator PN 1159SCC 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 intermittent) found that the I.11 inboard flap actuator failed the Ballnut End Play check. Endplay is .057in., limit is .012in. Resolution: RII - Remove Inbd flap actuator PN 1159SCC211-13 SN 44-514 and installed an overhauled actuator 1'N 1159SCC211-15 SN 58.1461as per GIV MM 27-06-00. No defect was noted. REF Item 15.42 for actual work performed Billing Method flows Rate "Final Labor USD: Time and Material ST 4.50 @ $115.00 $517.50 Labor USD: Time and Material OT 0.02 @ $173.00 $3.46 Parts USD: Time and Material $38,000.00 Total USD: $38,520.96 Pans: Rel. No. Part number: Description Quantity Sell price USD Extended USD 8.30 PI 1159SCC2I1-15 ACTUATOR, FLAP DRIVE, INBD 1 $38,000.00 $38,000.00 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 .012in. 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 JAW GIV MM 27.06.1N1. REF item 15.45 for actual work performed Billing Method Hours Rate Total Labor USD: Time and Material ST 4.50 @ $115.00 $517.50 Labor USD: Time and Material OT 0.02 @ $173.00 $3.46 Parts USD: Time and Material $38,023.79 Total USD: $38,544.75 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 831 #3 1159SCC212-16 ACTUATOR, FLAP DRIVE, R- I $38,000.00 $38,000.00 OUTBOARD 831 84 NAS1104-30D BOLT 3 $7.93 $23.79 Discrepancy: 8.32 RII - While T/S the squawk (8.10) for the flaps moving intermittenly found that the RH inboard nap actuator failed the Ballnut End Play check. Endplay is .030in., limit is .012in. 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 20 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117720 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Resolution: RH - COMPLIED WITH CMP GIV 275006 Inboard Flap Actuator (Right) - Removal / Installation. Removed R/H Inb Flap Actuator PN 1159SCC211-13, SN 60-390 and installed an overhauled actuator PN 1159SCC211-15, SN 91.848. Work JAW GIV MM 27-06-00. REF 15.44 for actual work performed Billing Method Hours Rate Total Labor USD: Time and Material ST 4.28 @ $115.00 $492.20 Labor USD: Time and Material OT 0.42 @ $173.00 $72.66 Parts USD: Time and Material $38,000.00 Total USD: $38,564.86 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 832 #2 1159SCC211-15 ACTUATOR, FLAP DRIVE, INBD 1 $38,000.00 $38,000.00 Discrepancy: 8.33 Found several chips and a soft spot that light can be seen through on the radome nose, under the errosion boot. Resolution: Removed Radome P/N 1159B21040-87K, S/N 211. Installed repaired Radome P/N 1159B21040-S7K, S/N 211. Radome repaired by Jetcraft Aerostructures, Inc. under W.O. 1304014. All maintenance performed JAW GIV AMM 53.10.10. Updated CMP 535005. Billing Method [lours Rate Total Labor USD: Time and Material ST 12.75 @ $115.00 $1,466.25 Services USD: No Charge N/ C Total USD: $1,466.25 Step: 8.33.1 Completed Complied with CMP 535005 Radome- Removal/Installation step A. through B.(6). Removed Radome P/N 1159821040-S7K, S/N 211. All maintenance performed lAW GIV AMM 53-10-10. Step: 8.33.2 Completed Complied with CMP 535005 Radome- Removal/Installation step C. through D. (3).Complete.s CMP Installed repaired Radome P/N 1159821040-S7K, S/N 211. Radome repaired by Jetcraft Aerostructures, Inc. under W.O. 1304014. All maintenance performed lAW GIV AMM 53-10-10. 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 R/H 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 Billing Method Flom Rate Total Labor USD: Time and Material ST 3.75 @ $115.00 $431.25 Parts USD: Time and Material $562.00 Total USD: $993.25 Pans: Ref. No. Pan number: Description Quantit r Sell price USD Extended USD For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 21 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117721 Bill To: TRT LEASING WO #: SCI3175 Invoice Number: 7113001425 Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.34 #1 1159SCC228-23 ROLLER - FLAP 1 $562.00 $562.00 Discrepancy: 8.35 RII - The LH flap's "B" tracks AFT, outboard bearing is bad (1159SCC226-7) Resolution: RH - Removed Lill flap track B outboard roller bearing P/N I I59SCC226-7. Install new L/H flap track B outboard roller bearing P/N I159SCC426.9 IAW GIV AMM 27-06-00. Updated CMP 275117 Billing Method Flours Rate Total Labor USD: Flat Rate $460.00 Parts USD: Time and Material $770.44 Total USD: $1,230.44 Pans: Ref. No. Pan number: Description Quantit • Sell price USD Extended USD 8.35 #2 1159SCC426-9 BEARING TRACK ROLLER EXT - 1 $770.44 $770,44 FLAP Step: 8.35.1 Completed Complied with GIV CMP 275117 wing flap roller (1.eftr 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 1AW GIV CMP 275117 & GIV NUM 27.06-00. Discrepancy: 8.36 The LH flap track "A" has corrosion Resolution: Removed light surface corrosion and pitting from VII flap track "A" . Cad plated exposed surface IAW GIV SRM 51.21.26. Primed and painted. All Work performed IAW GAC drawing SE05811901. Billing Method Flours Rate Total Labor USD: Time and Material ST 10.59 @ $115.00 $1,217.85 Labor USD: Time and Material OT 0.07 @ $173.00 $12.11 Parts USD: Time and Material $69.01 Services USD: Time and Material $1,600.00 Total USD: $2,898.97 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.36 #1 LUBRI-BOND-220 LUBRICANT, 12 OUNCE AEROSOL I $69.01 $69.01 SPRAY Services: Ref. No. Description Quantity Sell Price USD Extended USD 8.36 #1 SERVICE 1.00 $1,600.00 $1,600.00 Step: 8.36.1 Completed Removed light surface corrosion and pitting from IJH flap track "A" LAW GIV AMM 27.06-00. Step: 8.36.2 Completed Cad plated exposed surface IAW GIV SRM 51-21-26. Discrepancy: 8.37 The I.H flap track "B" has corrosion 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 22 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117722 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Resolution: Removed light surface corrosion and pitting from L/H flap track "B" Cad plated exposed surface IAW GIV SRM 51.21.26. Primed and painted. All Work performed IAW GAC drawing 5E05811901. Billing Method Hours Rate Total Labor USD: Time and Material ST 13.31 @ $115.00 $1,530.65 Labor USD: Time and Material OT 0.07 @ $173.00 $12.11 Total USD: $1,542.76 Step: 8.37.1 Completed Removed light surface corrosion and pitting front LAI flap track "B" IAW GIV AMM 27.06.00. Step: 8.37.2 Completed Cad plated exposed surface IAW GIV SRM 51-21-26. Discrepancy: 8.38 The LH flap track "C" has corrosion Resolution: Removed light surface corrosion and pitting from Lai Dap track "C". Cad plated exposed surface LAW GIV SRM 51.21.26. Primed and painted. All Work performed IAW GAC drawing 5E05811901. Billing Method Flours Rate Total Labor USD: Time and Material ST 9.34 @ $115.00 $1,074.10 Labor USD: Time and Material OT 0.07 @ $173.00 512.11 Total USD: $1,086.21 Step: 8.38.1 Completed Removed light surface corrosion and pitting from LAI flap track "C" LAW GIV AMM 27.06.00. Step: 8.38.2 Completed Cad plated exposed surface IAW GIV SRM 51-21-26. Discrepancy: 8.39 The LH flap track "D" has corrosion Resolution: Removed light surface corrosion and pitting from L/H flap track "D". Cad plated exposed surface IAW GIV SRM 51.21.26. Primed and painted. All Work performed IAW GAC drawing SE05811901. Billing Method Flours Rate Total Labor USD: Time and Material ST 10.60 @ $115.00 $1,219.00 Labor USD: Time and Material OT 0.07 @ $173.00 $12.11 Total USD: $1,231.11 Step: 8.39.1 Completed Removed light surface corrosion and pitting from LJH flap track "I)" IAW GIN' AMM 27.06.00. Step: 8.39.2 Completed Cad plated exposed surface IAW GIV SRM 51-21-26. Discrepancy: 8.40 The RH flap track "A" has corrosion Resolution: Removed light surface corrosion and pitting from R/H flap track "A". Cad plated exposed surface IAW GIV SRM 51.21.26. Primed and painted. All Work performed IAW GAC drawing SE05811901. 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_Work0rderPreliminaryInvoicespt Page 23 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117723 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Billing Method Flours Rate Total Labor USD: Time and Material ST 5.87 @ $115.00 $675.05 Labor USD: Time and Material OT 2.32 @ $173.00 $401.36 Total USD: $1,076.41 Step: 8.40.1 Completed Removed light surface corrosion and pitting from R/H flap track "A" LAW GIV AMM 27.06.00. Step: 8.40.2 Completed Cad plated exposed surface IASI, GIV SRM 51-21-26. Discrepancy: 8.41 The RH flap track "B" has corrosion Resolution: Removed light surface corrosion and pitting from R/H flap track "B". Cad plated exposed surface IAW GIV SRM 51.21.26. Primed and painted. All Work performed IAW GAC drawing SE05811901. Billing Method Hours Rate Total Labor USD: Time and Material ST 12.77 @ $115.00 $1,468.55 Labor USD: Time and Material OT 2.07 @ $173.00 $358.11 Total USD: $1,826.66 Step: 8.41.1 Completed Removed light surface corrosion and pitting from R/H flap track "B" IAW GIV AMM 27.06.00. Step: 8.41.2 Completed Cad plated exposed surface IAW GIV SRM 51-21-26. Discrepancy: 8.42 The RH flap track "C" has corrosion Resolution: Removed light surface corrosion and pitting from R/H flap track "C". Cad plated exposed surface JAW GIV SRM 51-21-26. Primed and painted. All Work performed IAW GAC drawing 5E05811901. Billing Method Flours Rate Total Labor USD: Time and Material ST 8.60 @ $115.00 $989.00 Labor USD: Time and Material OT 0.57 @ $173.00 $98.61 Labor USD: Time and Material WI 2.00 @ $230.00 $460.00 Total USD: $1,547.61 Step: 8.42.1 Completed Removed light surface corrosion and pitting from R/H flap track "C" JAW GIV AMM 27-06-00. Step: 8.42.2 Completed Cad plated exposed surface IASI, GIV SRM 51-21-26. Discrepancy: 8.43 The RH flap track "D" has corrosion Resolution: Removed light surface corrosion and pitting from R/H flap track "D". Cad plated exposed surface JAW GIV SRM 51.21.26. Primed and painted. All Work performed JAW GAC drawing SE05811901. 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_WorkOrderPreliminaryInyoicespt Page 24 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117724 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Labor USD: Time and Material ST 8.70 @ $115.00 $1,000.50 Labor USD: Time and Material OT 0.07 @ $173.00 $12.11 Labor USD: Time and Material DT 1.50 @ $230.00 $345.00 Total USD: $1,357.61 Step: 8.43.1 Completed Removed light surface corrosion and pitting from R/H flap track "D" JAW GIV AMM 27.06.00. Step: 8.43.2 Completed Cad plated exposed surface lAW 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. Billing Method [lours Rate Total Labor USD: Time and Material ST 8.90 @ $115.00 $1,023.50 Labor USD: Time and Material OT 0.07 @ $173.00 $12.11 Parts USD: Time and Material $481.99 Total USD: $1,517.60 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.44 #1 1159WM20235-3 BUSHING 2 $224.66 $44932 8.44#2 NAS1312-23 BOLT 1 $31.42 $31.42 8.44 #3 NLS21083N12 NUT $1.25 $1.25 Step: 8.44.1 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: 8.45 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. Billing Method Flours Rate Total Labor USD: Time and Material ST 8.54 @ $115.00 $982.10 Labor USD: Time and Material OT 0.25 @ $173.00 $43.25 Parts USD: Time and Material $481.99 Total USD: $1,507.34 Pans: ReE No. Part number: Description Quantity Sell price USD Extended USD 8.45 #1 1159WM20235-3 BUSHING 2 $224.66 $44932 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 25 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117725 Bill To: TRT LEASING WO #: SCI3175 Invoice Number: 7113001425 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.45 82 NASI312-23 BOLT I $31.42 $31.42 8.4583 MS21083N12 NUT I $1.25 $1.25 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 27-00-00 Labor USD: No Charge N/ C Step: 8.46.1 Completed Preped and sealed panel on vertical stab. Panel edge sealant ready for paint. IAW GIV AMM 20-00-00 Step: 8.46.2 Completed Sealed panels on the upper vertical on the left and right. Closed left 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 MN! 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. Billing Method Flours Rate Total Labor USD: Time and Material ST 4.00 @ $115.00 $460.0(1 Total USD: $460.00 Discrepancy: 8.48 Squawk from flight test - during climb #2 engine LP went into RED, pilots had to manually pull throttle back Resolution: Duplicate Squawk Ref. 8.16 Discrepancy: 8.49 Squawk from flight test - #1 engine was hotter than #2 by 80+ degrees Resolution: RII Item / Complied with CMP 750005 Performed Airflow Control System - Test. Adjusted LT airflow control regulator and actuator as required. Ops test is good no defects noted IAW RR TAY611-8 MM 71.00.00. Billing Method Flours Rate Total Labor USD: Time and Material OT 0.50 @ $173.00 $86.50 Total USD: $86.50 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 26 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117726 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Discrepancy: 8.50 It/II lower wing skin has corrosion near panel 22-FT-11 Resolution: Remove corrosion from R/H lower wing skin near panel 22-FT-11. Prime and paint. Work done IAW GIV SRM 51.13-20. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.58 @ $115.00 $181.70 Labor USD: Time and Material OT 0.25 @ $173.00 $43.25 Parts USD: Time and Material $576.49 Total USD: $801.44 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.50 #1 EA960-F ADHESIVE I $576.49 $576.49 Discrepancy: 8.51 R/H lower wing skin has corrosion near panel 22-FT-14 Resolution: Remove corrosion from ELM lower wing skin near panel 22-FT-14. Prime and paint. Work done IAW GIV SRM 51.13.20. Billing Method Flours Rate Total Labor USD: Time and Material ST 133 @ $115.00 $152.95 Labor USD: Time and Material OT 0.25 @ $173.00 S43.25 Total USD: $196.20 Discrepancy: 8.52 R/H lower wing skin has corrosion near panel 22-FT-15 Resolution: Remove corrosion from R/H lower wing skin near panel 22-FT-15. Prime and paint. Work done IAW GIV SRM 51-13.20. Billing Method flours Rate Total Labor USD: Time and Material ST 1.58 @ $115.00 $181.70 Total USD: $181.70 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 27 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117727 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Discrepancy: 8.53 R/H lower wing skin has corrosion near panel 22-FT-7 Resolution: Remove corrosion from R/Ii lower wing skin near panel 22-FT-7. Prime and paint. Work done IAW GIV SRM 51.13.20. Billing Method Hours Rate Total Labor USD: Time and Material ST 6.62 @ $115.00 $761.30 Labor USD: Time and Material OT 1.25 @ $173.00 $216.25 Total USD: $977.55 Discrepancy: 8.54 While C/W CMP 275123 sqk 8.34. CMP 275123 preferres that corresponding roller be replaced at same time. Resolution: The roller bearing has no defects and does not require to be replaced IAW GIV MM 27-06.00. No further action required Discrepancy: 8.55 While C/W CMP 275117 sqk 8.35. CMP 275117 preferres that corresponding roller be replaced at same time. Resolution: The roller bearing has no defects and does not require to be replaced IAW GIV MM 27-06-00. No further action required Discrepancy: 8.56 While removing R/H wing fuel panel 22-Fr-1 for sqk 15.32. Found ground mesh on panel to he torn. pn 1159WM40076.13 Resolution: Removed torn mesh gasket P/N 1159WM40076.13 and installed a NEW mesh gasket P/N 1159WM40076-13 as required IAW GIV MM 28.11.00. Billing Method Flouts Rate Total Parts USD: Time and Material $107.12 Total USD: $107.12 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.56 #1 1159WM40076-13 GASKET 1 $107.12 $107.12 Discrepancy: 8.57 Squawk from flight test - MED seal was squealing during flight For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 28 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117728 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 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. Billing Method Flours Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.58 Refuel aircraft to 50001bs Resolution: Refuel aircraft to requested 5000lbs in accordance with GIV Partial Refueling Procedures; Maintenance Manual Chapter 28-04-00. Labor USD: No Charge N/ C 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-1IAW GIV MM 28.11.00. Billing Method Flours Rate Total Parts USD: Time and Material $6.78 Total USD: $6.78 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.59 #1 NAS1580V4T10 SCREW 1 $6.78 $6.78 Step: 8.59.1 Completed Ordered fuel panel screw p/n- NAS1580V4T10 per GIV IPC 57-20-00. Ref item # 15.62. Awaiting for pan. Discrepancy: 8.61 While repacking cabin 02 masks found R/H forward and middle cabin masks to have the circle clips missing marked affected masks with orange streamers ) 289.601.228 Resolution: Removed Two (2) forward and Two (2) Middle R/H cabin masks P/N: 289.601.228 with not S/N's and replaced with new cabin masks P/N: 289-601-228 with not S/N's; All work done IAW GIV AMM 35-00-00. Billing Method Noun Rate Total labor USD: Time and Material ST 3.50 @ $115.00 $402.50 Parts USD: Time and Material $314.60 Total USD: $717.10 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 29 of 35 Printed: 5/1/2013 4:33:33PF Ref: I: EFTA01117729 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Pans: Ref. No. Part number: Descri ion Quantity Sell price USD Extended USD 8.61 #1 289-601-228 MASK ASSEMBLY 4 $78.65 $314.60 Discrepancy: 8.63 R&R the LT and RT 12th stage solenoid A and B valve filter Resolution: Removed the LT and RT 12th Stage Servo Controllers to gain access to A and B HP Control Valve filters. Removed A and B Servo Controllers valve filters P/N: 856504-5 and installed new P/N: 856504-5 filters in both Servo Controllers and re-installed both Lt and Rt 12th Stage Servo Controllers. Leak and Operational check needs to be performed on both Lt and Rt 12th Stage Servo Controllers. All work done IAW GIV AMM 36.01.01. Updated CMP's 361078, 361077. Refer to item 8.67 for Panel installation and Leak and Op's checks. Billing Method Flours Rate Total Labor USD: Time and Material ST 8.58 @ $115.90 $986.70 Labor USD: Time and Material OT 0.10 @ $173.90 $17.30 Total USD: $1,00,1.00 Step: 8.63.1 Completed Removed the LT and RT 12th Stage Servo Controllers to gain access to A and B HP Control Valve filters. Removed A and B Servo Controllers voile filters P/N: 856504-5 and installed new P/N: 856504-5 filters in both Servo Controllers and re-installed both 1.t and Rt l2th Stage Servo Controllers. Leak and Operational check needs to be performed on both Lt and Rt 12th Stage Servo Controllers. All work done lAW GIV AMM 36411.01. Updated CMP's 361078, 361077. Discrepancy: 8.64 LH horizontal stab skirt panel 109-BUL-SLH found teflon strip peeled oft Resolution: Re-Attached Teflon Strip On Skirt Panel 109-BUL-SLH For Left Hand Horizontal. All Maintenence Performed In Maintenence To GIV AMM 20.00.00. Billing Method Flours Rate Total Labor USD: Time and Material ST 7.55 @ $115.00 $868.25 Total USD: $868.25 Discrepancy: 8.65 LH horizontal stab 37-LE-1 panel (INBD L.E.) found deriorated seal. Resolution: Removed Worn Seal From L/H Horizontal Leading Edge InBoard Panel 37-LE-1 and Replaced With New Seal P/N 1159CS20258-21. All Maintenence Performed In Reference To GIV AMM 20-00-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 4.92 @ $115.00 $565.80 Parts USD: Time and Material $17.30 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 30 of 35 Printed: 5/1/2013 4:33:33PF Ref: I: EFTA01117730 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Total USD: $583.10 Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.65 #1 1159CS20258-21 SEAL 1 $17.30 $1730 Discrepancy: 8.66 RH horizontal stab 38-LE-1 panel (INBD L.E.) found deriorated sea►. Resolution: Removed Worn Seal From R/H Horizontal Leading Edge InBoard Panel 37-LE-1 and Replaced With New Seal P/N 1159C520258-21. All Maintenence Performed In Reference To GIV AMM 20-00-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 4.93 @ $115.00 $566.95 Pans USD: Time and Material $17.30 Total USD: $584.25 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.66#1 1159CS20258-21 SEAL 1 $17.30 $1730 Discrepancy: 8.67 As per CMP 361077 & 361078, Leak and Op's check due of both Lt and Rt 12th Stage Servo Controllers. Panels (29/30-UPR-2) require installation after leak check. Resolution: Complied with CMP 361007 and 361008 Bleed Air System 1.11I and R/H Operational Test. Ops and leak check is good. No discrepancies noted at this time. All work I.A.W. GIV M/M 36-00-00. Item: 9 Paint Team Manager: Sean Brown ParVModel 0: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSNITSO: CSNICSO: Aircraft Time: 8,567.0 / 3,964 Discrepancy: 9.1 Rai lower wing skin has corrosion near panel 22-FT-7 Resolution: duplicate item to 8.53 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 31 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117731 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Item: 10 Outstanding Parts, Materials, and / or Services Team Manager: Sean Brown ParVModel 0: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TS0: CSNICS0: Aircraft Time: 8,567,0 / 3.964 Discrepancy: 10.4 Service from 8.37 Resolution: Services USD: No Charge NI C Services: Ref. No. Description Quantity Sell Price USD Extended USD 10.4#1 SERVICE 1.00 $0.00 $0.00 Discrepancy: 10.5 8.33 Resolution: Services USD: No Charge NI C Services: Ref. No. Description Quantity Sell Price USD Extended USD 10.5#1 SERVICE 1.00 $0.00 $0.00 Item: 12 Aircraft Records and Logbook Research Only Team Manager. Sean Brown ParVModel 0: Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TS0: CSN/CS0: Aircraft Time: 8.567.0 / 3,964 Discrepancy: 12.2 No log entry found for the removal of NLG rod end P/N 1159HM40120-1 and the installation of 1)/N 1159SCL567-3. Mandatory CB 183 was on 10/24/06. Resolution: Item was compled with by Duncan Aviation on 10/24/06 under W/O FK8BA. No further action taken. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.00 @ $115.00 $115.00 Labor USD: Time and Material OT 0.10 @ $173.00 $17.30 Total USD: $132.30 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_Work0rderPreliminaryInvoicespt Page 32 of 35 Printed: 5/1/2013 4:33:33P/ Ref: I: EFTA01117732 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Discrepancy: 123 No log entry or tag was found for APU Fire bottle cartridge P/N AE30903823 S/N AENI-23 installed on August 3. 2005. Resolution: Researched records and found Tag for APU Fire bottle cartridge . No further action taken. Billing Method Flours Rate Total Labor USD: Time and Material ST 2.25 @ $115.00 $258.75 Labor USD: Time and Material OT 0.10 @ $173.00 $17.30 Total USD: $276.05 Discrepancy: 12.4 No log entry• was found for NLG Axle Assy. P/N 1159LM40544-7 S/N BFG6056NTW installed on June 3, 1999. Resolution: Researched records and found Tag for NLG Axle. No further action taken. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.25 @ $115.00 5143.75 Total USD: $143.75 Discrepancy: 12.5 No 8130 found for Moe& Co-pilot side window attach bolts. Replaced on 12/11/98. Resolution: Found 8130 for the Pilot'& Co-pilot side window attach bolts. Replaced on 12/11/98. The parts were installed New. No further action required. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.00 @ $115.00 $115.00 Labor USD: Time and Material OT 0.10 @ $173.00 517.30 Total USD: $132.30 Discrepancy: 12.6 No 8130 found for isolator IJH Aft Fwd. S/N 2998 installed on 12/11/98. Resolution: Found 8130 for the L/H Aft Fwd. S/N 2998 installed on 12/11/98. The part was installed New. No further defects taken. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.00 @ $115.00 $115.00 Labor USD: Time and Material OT 0.10 @ $173.00 $17.30 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_WorkOrderPreliminarylnvoiceipt Page 33 of 35 Printed: 5/1/2013 4:33:33PF Ref: I: EFTA01117733 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Total USD: $132.30 Discrepancy: 12.7 No 8130 found for isolator L/H Aft aft S/N 2982 installed on 12/11/98. Resolution: Found 8130 for the isolator L/H Aft aft S/N 2982 installed on 12/11/98. The part was installed New. No further defects noted. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.00 @ $115.00 $115.00 Labor USD: Time and Material OT 0.10 @ $173.00 $17.30 Total USD: $132.311 Discrepancy: 12.8 No 8130 found for isolator Rill Aft Fwd. S/N 2993 installed on 12/11/98. Resolution: Found 8130 for isolator R/II .1ft Fwd. S/N 2993 installed on I2/11/98.The part was installed New. No further action taken. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.00 @ $115.00 $115.00 Labor USD: Time and Material 0.10 @ $173.00 $17.30 Total USD: $132.31) Discrepancy: 12.9 No 8130 found for isolator R/H Aft Aft. S/N 2994 installed on 12/11198. Resolution: Found 8130 for isolator R/11 Aft Aft. S/N 2994 installed on 12/11/98. The part was installed New. No further action taken. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.00 @ $115.00 $115.00 Labor USD: Time and Material OT 0.10 @ $173.00 SI7.30 Total USD: $132.30 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 34 of 35 Printed: 5/1/2013 4:33:33P/ Ref: I: EFTA01117734 Bill To: TRT LEASING WO #: SC13175 Invoice Number: 7113001425 Discrepancy: 12.10 No 8130 or log entry found for nose wheel steering installed on 10/11/06. Resolution: The same steering unit PN. 1159SCL200.43 SN.1003 was only removed and installed for a corrosion inspection on 10.11-06 and no maintenance was performed on steering unit. No 8130 is required. No further action taken at this time. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.50 @ $115.110 $172.50 Labor USD: Time and Material OT 0.20 @ $173.00 $34.60 Total USD: $207.10 Discrepancy: 12.11 AD74.08.09 R3 Lavatory Paper and Linen Waste Receptacle Enclosure Access Door and Disposal Door Inspection is due in 126.7 Hours Resolution: This item is not due at this time. No further action taken. Communications conceming disputed debts, including a check or other instrument tendered as full satisfaction of a debt, must be forwarded to: Gulfstream Aerospace Attn: Credit Manager M/S B-05 PO BOX 2206, Savannah, GA 31402 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 35 of 35 Printed: 5/1/2013 4:33:33P) Ref: I: EFTA01117735