EFTA01117701.pdf

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