Gulfstreant DYNASMCC COMPANY

Gulfstreant DYNASMCC COMPANY Bldg C.-FAX 561-681-9392 - West Paint Beach. Florida 33406 PRELIMINARY INVOICE ParUModel #: GIIB AC Serial No./Tail No.: 151 / N909JE Mail Remittance To: Gulfstream Aerospace Corporation P.O. Box 730349 Dallas. Texas 75373-0349 Overnight Remiaance To: Gulfstream Aerospace Corporation (Box # 730349) Go JP Morgan Chase Bank. NA ATTN: Dallas National Wholesale Lockbox TX1-0029 14800 Frye Road Ft. Worth, TX 76155 Bill To: HYPERION AIR, INC. 3800 SOUTHERN BLVD SUITE 204 WEST PALM BEACH, Florida 33406 United States Title: HYPERION AIR, INC. Wire Remittance To: Gulfstream Aerospace Corporation JP Morgan Chase Bank. NA Chicago. IL 60670 7112000954 3/15/2012 CH200 Invoice Number. Invoice Date: Customer ID: P.O. Number. Repair Station: In Date: Out Date: Payment Type: Payment Terms: FAA CRS PB8R624N 02/06/2012 03/23/2012 Net 30-Open terms INVOICE SUMMARY FOR WORK ORDER NUMBER: SC10420 lime & Materials Flat Rate Total Labor USD: $27,009.12 $161,722.63 $188,731.75 Parts USD: $91,680.83 $6,500.00 $98,180.83 Services USD: $33,067.13 S0.00 $33,067.13 Detail Subtotal USD: $151,757.08 $168,222.63 $319,979.71 Subtotal USD: $319,979.71 Funds on Deposit USD: $0.00 Total USD: $319,979.71 For detail description of the work complied with see the Work Order Detail report. Unless (ahem' GAC_WorkOrderPreliminaryInvoicespt indicated, all financial values listed in this document are in US Dollars (USD). Page 1 of 98 Printed: 3/23/2012 4:28:32P) BAY. EFTA01080493 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Item: 1 Airframe Gulfstream GLIB Scheduled N909JE Team Manager: Sean Brown Customer Coordinator: Ray Kraber Pan/Model #: GIIB AC Serial No./Tail No.: 151 / N909JE TSN/TSO: CSN/CSO: 5663 Aircraft Time: 10804.3 Discrepancy: 1.1 Return to Service FAR 91.409 (f) (3) Inspection Resolution: ACTT: 10,804.3 ACTL: 5,663 DATE: March XX, 2012 I certify that this aircraft has been inspected in accordance with a Due List Inspection under the approved manufacturer's recommended inspection program, FAR 91.409 (f)(3) and is approved for return to service with regards to the maintenance accomplished. Further details of this inspection and related maintenance are on file at this repair station under the above work order. Thomas J. Choynowski, Sr. Airworthiness Inspector Gulfstream-PBI 1500-C Perimeter Road West Palm Beach, FL 33406 FAA CRS PB8R624N Step: 1.1.1 Waiting A/C Times and Cycles approval (L) Step: 1.1.2 Waiting A/C Warrant• Status / Contracts approval (L) Discrepancy: 1.2 Inbound/Outbound Inspection Resolution: Complied with inbound inspection as required. Labor USD: No Charge N/ C Step: 1.2.1 Completed Inbound/Preliminary Inspection Step: 1.2.2 Waiting Outbound Inspection approval (L) Discrepancy: 1.3 Resolution: Preflight Inspection Discrepancy: 1.4 Comply with Debrief Checklist For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 2 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080494 Bill To: HYPERION AIR, INC. Resolution: Complied with Debrief Checklist WO It: SC10420 Invoice Number: 7112000954 Step: 1.4.1 Completed Arrival/Debrief 90 Day Due List Review Accomplished. Step: 1.4.2 Completed List Operator's Airworthiness Requirements & Special Documentation Requests. Step: 1.4.3 Completed Review Technical Operations Update prior to return to service for newly released bulletins and advise operator. Discrepancy: 1.5 Tool Clearance Resolution: All tooling was returned to the toolroom. Pans USD: No Charge Parts: Ref. No. Part number: Description Quantity 1.5 #1 740031 Wing wedge templete Left N/C Discrepancy: 1.6 Cover & Protect Resolution: Cover & Protected as required. Labor USD: No Charge N/ C Discrepancy: 1.7 Resolution: N/A Service Chemical Toilet/Clean Galley Discrepancy: 1.8 ArrivaUDeparture Assist & Video Aircraft Resolution: Arrival/Departure Assist & Video Aircraft as required. Discrepancy: 1.9 Sample Hydraulic Fluids Resolution: Sampled Hydraulic Fluids as required. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 3 of 98 Printed: 3/23/2012 4:20:32P) Ftst X EFTA01080495 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 1.10 Remove Valuables & Secure. Resolution: Na Discrepancy: 1.11 Comply with Service Team Manager Checklist Resolution: Discrepancy: 1.12 Fluids Used (OiLs/Skydrol) - (Materials Only) Resolution: Billed as required. Discrepancy: 1.13 STM / Quality review of work order and logbook entry prior to departure Resolution: Discrepancy: 1.14 Towing (Does not include Hangar Moves) Resolution: Towed as required. Labor USD: No Charge N/ 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_WorkOrderPrelintinaryInvoicespt Page 4 of 98 Printed: 3/23/2012 4:28:32P) Flee X EFTA01080496 Bill To: HYPERION AIR, INC. WO*: SC10420 Invoice Number: 7112000954 Discrepancy: 1.15 Resolution: Na HazMat - Identify & provide a manifest, and a Shipper's Declaration for Dangerous Goods for all hazardous materials that are loaded aboard any aircraft. FAR Part 121 or 135 Operators will provide a hazardous material notification letter required by FAR 135.505 (e) prior to maintenance at this Repair Station iaw FAR 145.206 (a) (b). If there is to be loading of hazardous materials it shall be complied with by Hazmat trained authorized GDAS-PBI personnel only. Discrepancy: 1.16 Aircraft Cleaning Resolution: N/A Discrepancy: 1.17 Billable Consumables & Shop Supplies Resolution: as required. Billing Method Hours Rate Total Pans USD: Flat Rate $4,000.00 Total USD: $4,000.00 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 5 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080497 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 1.18 Resolution: N/A Major Alterations regulatory compliance requirements to be completed by installer as indicated on FAA form 8110-3. Copy and paste from attached statements as needed and edit as required. COMPLY WITH REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d). COMPLIED WITH THE REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d), via GROUND TEST REPORT -REPORT No. CEXXXXXXXX REV. X, ( IN SUPPORT OF STC XXXXXXXXX ) and GR4R216M REPAIR STATION INTERFERENCE TESTING REQUIREMENTS POST MAJOR ALTERATIONS COMPLIANCE FORM. COMPLY WITH REQUIREMENTS OF FAR 25.1529, INSTRUCTIONS FOR CONTINUED AIRWORTHINESS. REF XXXXX MANUAL, P/N XXXXXXX REV. X, FOR INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AND BLOCK 8 OF FAA FORM 337, DATED XX/XX/XXXX. COMPLY WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01.04 AND FAR 25.1353 (B) COMPLIED WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01.04 AND FAR 25.1353 (B) BY ENSURING ROUTING WAS IN ACCORDANCE AC43.13-1B, CHANGE 1 CHAPTER 11, SECTION S. Discrepancy: 1.19 Update Weight & Balance Resolution: N/A For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 6 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080498 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Discrepancy: 1.20 Exterior Paint and Weight & Balance Requirements. Review scope of aircraft exterior paint touch-up/repairs, and skin replacements resulting in paint reapplication, and determine affect on weight and balance. For surfaces where paint is stripped and reapplied or added on top of existing paint on an area greater than 36 square feet the thickness values will be documented before and after painting . If average thickness values remain the same, weight and balance revision is not required. For surfaces painted with an area greater than 36 square feet and before and after paint thickness average varies, QC review for possible weight and balance revision will be required. * Thickness will be plotted on an aircraft drawing derived from AMM chapter 6 or other suitable sketch, attached to the work order and measurements taken on a two square foot grid. * Reference CAMPS 4000, paragraph 3.5.1 for paint restrictions to flight control surfaces and RVSM certified aircraft. * Reference CAMPS 4000, total average thickness shall not exceed 6 mils. * Per GAC Mass Properties Engineering, paint thickness of 5 mils equals .055 pounds per square foot. * If after QC review, weight change is greater than 2 pounds or .05% of MAC, the weight and balance report will require recomputation. Resolution: N/A Discrepancy: 1.21 Resolution: N/A "Advise customer of preservation requirements per ATA Chapter 10 of the relevant maintenance manuals for Airframe, Engines, and APU; review requirements in relation to scheduled Date Promised and later potential Date Completed; and perform maintenance or preservation actions as directed by the customer and documented as a Work Order Squawk. Item: 6 Avionics Team Manager: Sean Brown Customer Coordinator: Ray Kraber ParUModel AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 6.1 MED emergency light does not illuminate when EMER LT switch is turned on or in the AUTOMATIC mode. Works when switch is placed in MANUAL Resolution: Performed operational check. Found MED emergency light works in manual but not automatic. Gained access to MED emergency lights. Found G-switch tripped. Reset G-switch. Performed operational check. Checks good. All work performed IAW G-II AMM chapter 33.02-00. 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_WoikOrderPreliminarylnvoice.rpt Page 7 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080499 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Billing Method Hours Rate Total Labor USD: Time and Material ST 2.83 @ $115.00 $325.45 Total USD: $325.45 Discrepancy: 6.2 AFT entryway light inop. Resolution: Item: 8 Mechanical Team Manager: Sean Brown Customer Coordinator: Ray Kraher Part/Model SI: AC Serial No./Tail No.: TSN/TS0: CSN/CS0: Aircraft Time: Discrepancy: 8.1 Extra time for removing BUL-1 & BUL-2 so that BUL-3 can be removed for elevator removal. Note: these panel not on removal sheet for elevators. Resolution: Complied with info only. Billing Method Hours Rate Total Labor USD: Flat Rate $920.00 Total USD: $920.00 Discrepancy: 8.2 While complying with CMP# 272015, Right aileron removal/installation, found most screws corroded/rusted. Quantity : ( 100 ) ( P/N: NAS 1203.3) screws, ( 40 ) ( P/N: NAS 1203-5 ) screws. NOTE: Quantity included's rusted/corroded Left aileron R&R panel screws. Resolution: Installed new screws as reuired. P/N NAS 1203.3 and NAS 1203.5. lAW GIIB AMM 27-00-00 and 20-00-00. Labor USD: Parts USD: Total USD: Billing Method Hours Rate Total Flat Rate $230.00 Time and Material $300.32 $530.32 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_Work0rderPrelintinaryInvoicespt Page 8 of 98 Printed: 3/23/2012 4:28:32PD Rd X EFTA01080500 Bill To: HYPERION AIR, INC. Parts: Ref. No. Pan number: WO It: SC10420 Description Invoice Number: 7112000954 Quantity Sell price USD Extended USD 8.281 NASI203-3 BOLT 100 $0.26 $26.00 8.2 #2 NASI203-5 BOLT 50 $0.26 $13.00 8.2 #3 GAS550E3S9 SCREW 10 $4.12 8$471..2420 8.2 #4 GAS550E3S10 SCREW 4 $1.81 8.2 #5 NAS583-II BOLT 4 $24.66 $98.64 8.2 #6 NAS583-I3 BOLT 2 $15.68 $31.36 8.2 #7 NAS583-I4 BOLT 2 $23.77 $47.54 8.2 #8 NAS583-I6 BOLT 2 $17.67 $35.34 Discrepancy: 8.3 While comply with CMP 272810 Rudder removal. Found upper bonding wire broken at vert stab Resolution: Removed broken upper rudder bonding wire at vert stab P/N MS25083-2BB13 and replaced with new bonding wire P/N MS25083-2BB13 IAW GIIB AMM 20-00-00. Billing Method Flours Rate Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $10.30 Total USD: $240.30 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8381 MS25083-2BBI3 JUMPER-ELEC BONDING,I3 IN I $10.30 $1030 Discrepancy: 8.4 While complying with CIHN's 575030/575025 , Wing to fuselage interior LefURight inspection, found ALL screws rusted/corroded. Most needed screwbusters for removal which amounted to considerable time over CMP aloted time. Screws needed as follows: P/N: MS24694s50 : Qty: 330 P/N: 1159B21241-71 Qty: 1 P/N: 1159B21241-78 Qty: 1 P/N: 1159B21241-33 Qty: 1 P/N: 1159B21241-73 Qty: 1 P/N: 1159B21241-81 Qty: 1 P/N: 1159B21241-35 Qty: 1 Resolution: Removed and discarded corroded screws and installed new screws.P/N: M524694550 : Qty: 330 P/N: 1159B21241-71 Qty: 1 P/N: 1159B21241-78 Qty: 1 P/N: 1159B21241-33 Qty: 1 P/N: 1159B21241-73 Qty: 1 P/N: 1159821241.81 Qty: 1 P/N: 1159B21241-35 Qty: 1 All work done i/a/w G-II B SRM ch 51.41.00. No further defects 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_WorkOrderPrelititinaryInvoicespt Page 9 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080501 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Labor USD: Pans USD: Total USD: Parts: Ref. No. 8.4 11 Billing Method Flat Rate Time and Material Part number: M524694 S50 Hours Rate Total $460.00 $78.00 $538.00 Description Quantity Sell price USD Extended USD SCREW-MACHINE,FLAT CSK HEAD 300 $0.26 $78.00 Discrepancy: 8.5 Change float valve mid point on right wing per customer. Resolution: Remove vent float valve P/N 159SC-P-006 S/N1010. Install a New float valve P/N 159SCP006-1 S/N 4771. Install new O rings under mount screw heads. All work performed IAW GLIB AMM 28.02.00. Billing Method Hours Rate Total Labor USD: Time and Material ST 15.88 @ $115.00 $1,826.20 Labor USD: Time and Material OT 0.13 @ $173.00 $22.49 Parts USD: Time and Material $2,557.27 Total USD: $4,405.96 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.511 1159SCP006-1 PUMP 1 $1,925.35 $1,925.35 8.5 13 HTI83-3-2 SCREW 3 $197.76 $593.28 8.514 GASI3AF6 O-RING 3 $12.88 $38.64 Step: 8.5.1 Step: 8.5.2 Step: 8.5.3 Completed Remove float valve mid point on right wing P/N159SC-P-006 S/N 1010. Work LAW GLIB MM 28-02-00 Completed Positioned new float valve in place, P/N 11S9SCP006.1, S/N 4771, and tightened mounting screws. Float valve will have to be removed in order to install 3 o-rings that are to be placed under mounting screws. Refer to Gulfstream BB IPC 28-10-00 figure 6, sheet 1, item 3. O-rings are on order. Completed Install 3 o rings under float valve mounting screw heads IAW (MB AMM 28-01.01. Discrepancy: 8.6 Nine rivnuts need replaced on R/H wing wedge panel. Required drilling of screws due to rivnuts spinning. Resolution: Removed and replaced nine rivnuts on the R/I4 wing wedge panel. Installed new rivnuts P/N GAN512B3-166 wet with sealant. Had to gain acess to fuel tank area to remove drilled out rivnuts All work done IAW G-IIB SRM 51.41-00. Labor USD: Labor USD: Pans USD: Total USD: Parts: Ref. No. Billing Method Time and Material Time and Material Time and Material Part number: Hours Rate Total ST 13.44 @ $115.00 $1,545.60 OT 4.35 @ $173.00 $752.55 $273.47 $2,571.62 Description Quantity Sell price USD Extended USD BLIND NUT 8.6 11 GAN512B3-166 10 $1.52 For detail description of the work complied with see the Work Order Detail report. $15.20 Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 10 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080502 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.6 #2 GAN512B3-216 NUT 10 $6.10 $61.00 8.6 #3 GAN512B3-266 RIV-NUT 10 $15.88 $158.80 8.6 #4 PR1422-B-2 SEALANT, PRC, CARTRIDGE 1 $38.47 $38.47 Step: 8.6.1 Step: 8.6.2 Step: 8.6.3 Completed Disconnected the 5 hydraulic lines to gain access to the sponson access cover 22-SR-2 all lines are capped and or plugged. RLP Completed Removed access cover 22-SR-2 on outboard side of sponson Completed Removed all spinning and bad donuts on the RAI wing wedge panel IAW G-IIB AMM 5140.00. Discrepancy: 8,7 Left wing flap tracts A,B,C, and D have corrosion on roller bearing surfaces. Resolution: Removed corrosion from flap track bearing surfaces on tracks A,B,C and D JAW (MB CPCM 20.50.01.Measured tracks A,B,C and D for thickness as required JAW Gulftream drawing SE05811901. See item 8.88 for details on track C. All others check good. Performed brush cadmium plating repair to all exposed surfaces of flap tracks A,B,C and D IAW Gulftream drawing SE05811901.Cleaned and protected tracks and surrounding area, masked-off track bearing surface, applied two coat epoxy primer 2012 and surface primer, applied top coat, JAW. GAMPS 4000. Labor USD: Pans USD: Total USD: Billing Method Hours Rate Total Flat Rate $6,900.00 Time and Material Parts: Ref. No. Part number: 8.7 #1 PRI440-B-1/2 Step: 8.7.1 Completed Step: 8.7.2 Completed Step: 8.7.3 Completed Step: 8.7.4 Completed $153.12 $7,053.12 Description Quantity Sell price USD SEALANT, PRC,CARTRIDGE 4 538.28 Extended USD Removed corrosion front flap track bearing surfaces on tracks A,B,C and D IAW GIIB CPCM 20-50-01. Measure tracks A,B,C and Dfor remaining thickness. Performed brush cadmium plating repair to all exposed surfaces of flap tracks A,B,C and D IAW Gulftream drawing SE05811901. Cleaned and protected tracks and surounding area, masked-off track bearing surface, applied two coat epoxy primer 2012 and surface primer, Prep. tracks to top coat. IAW. CAMPS 4000. $153.12 Discrepancy: 8.8 Right wing flap tracts A,B,C, and D have corrosion on roller bearing surfaces. Resolution: Removed corrosion from flap track bearing surfaces on tracks A,B,C and D IAW GlIB CPCM 20.50.01.Measured tracks A,B,C and D for thickness as required IAW Gulftream drawing SE05811901, with no defects noted. Performed brush cadmium plating repair to all exposed surfaces of flap tracks A,B,C and D [ASV Gulftream drawing SE05811901.Masked off flaps tracks A B C and D, washed with solvent and primed with 2012 primer, and applied topcoat IAW GAC CAMPS 4000. Billing Method Hours Rate Total Labor USD: Flat Rate $6,900.00 Total USD: $6,900.00 For detail description of the work complied with see the Work Order Detail report. GAC_WorkOrderPrelintinaryInvoice.rpt Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). Page I I of 98 Printed: 3/23/2012 4:28:32P) Flet X EFTA01080503 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Step: 8.8.1 Step: 8.8.2 Step: 8.8.3 Step: 8.8.4 Step: 8.8.5 Completed Removed corrosion from flap track bearing surfaces on tracks A,B,C and D IAW GIIB CPCM 20-50-01. Completed Measure tracks A,B,C and Dfor remaining thickness. Completed Performed brush cadmium plating repair to all exposed surfaces of flap tracks A,B,C and D IMV Gulftream drawing SE05811901. Completed Cleaned and protected tracks and surounding area, masked-off track bearing surface, applied two coat epoxy primer 2012 and surface primer, Prep. tracks to top coat. IAW. CAMPS 4000. ( Written in ERROR this step belongs under item 8.7 ) Refer to squawk 8.7.4. Completed Masked off flaps tracks A B C and D, washed with solvent and printed with 2012 primer ready to spray paint. Discrepancy: 8.9 L/H wing wedge has 18 drilled off screw heads because rivnuts were spining. Resolution: Removed and replaced eighteen rivnuts on the UH wing wedge panel. Installed new rivnuts P/N GAN512B3-166 wet with sealant. Had to gain acess to fuel tank area to remove drilled out rivnuts All work done IAW G-IIB SRM 51.41.00. Billing Method Hours Rate Total Labor USD: Flat Rate $2,300.00 Pans USD: Time and Material $117.00 Total USD: $2,417.00 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.9#1 GAB511GA3-7 HI-BOLT I $2.06 $2.06 8.9 #2 PR1422-B-2 SEALANT, PRC, CARTRIDGE I $38.47 $38.47 8.9 #3 GAN512B3-166 BLIND NUT 25 $1.52 $38.00 8.9 #4 PR1422-B-2 SEALANT, PRC, CARTRIDGE I $38.47 $38.47 Step: 8.9.1 Completed Removed all spinning and bad rhnuts on IJH wing wedge IAW G-IIB MOM 51-40-00. Discrepancy: 8.10 Aileron trim tab has cracked skin in the area of the inner and outter hinges on the bottom side of the tab. Resolution: Trimmed aileron tab hinge skin areas as required IAW Gulfstream drawing SE35813107. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Total USD: $460.00 Discrepancy: 8.11 R/H elevator, top, inbd, hinge cover attach screw hole, heli-coil is bad. Resolution: Replaced bad R/H elevator, top, inbd, hinge cover attach screw hole, hell-coil with a new one JAW CAMPS 2212. Checks good. Billing Method Flours Rate Total Labor USD: Flat Rate $460.00 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_WorkOrderPrelititinaryInvoicespt Page 12 of 98 Printed: 3/23/2012 4:28:32P) our X EFTA01080504 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Total USD: $460.00 Discrepancy: 8.12 L/H elevator No.3 hinge, attach bolt bore is corroded. Resolution: Removed corrosion as required and remeasured L/H elevator No.3 hinge, attach bolt bore. Hole measurement is within limits. Work performed IAW GLIB MM 27-01-00. and SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Total USD: $460.00 Discrepancy: 8.13 R/H elevator, oubd top skin, has a spot of corrosion. Resolution: Removed light corrosion spot on R/H elevator outbd top skin, Sanded treated and primed top coat as required IAW GB' gamps 4000 Billing Method Hours Rate Total Labor USD: Flat Rate $345.00 Total USD: $345.00 Step: 8.13.1 Completed Removed and blend out light surface corrosion from the R/H elevator, upper surface Treated bare metal, and spot primer as required. IAN'. SRM.51-13-20. Discrepancy: 8.14 R/H wing upper sponson plate is corroded. Resolution: Mechanically removed corrosion from edges of the R/H upper sponson plate, Strip heavy paint for a better look IAW. GAC. 5E45802903. Removed all old sealant from around sponson plate. Treated and primed all bare metal. Resealed sponson plate. All work done IAW Standard Repair/Corrosion of Sponson Plates DWG No. 5E45802903 REV.D. Performed cadmium plating repair on R/H upper sponson plate. All work done IAW Standard Repair/Corrosion of Sponson Plates DWG No. SE45802903 REV.D Billing Method Hours Rate Total Labor USD: Time and Material ST 17.65 @ $115.00 $2,029.75 Labor USD: Time and Material OT 433 @ $173.00 $749.09 Services USD: Time and Material $400.00 Total USD: $3,178.84 Services: Ref. No. Description Quantity 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_WorkOrderPrelintinaryInvoicespt Page 13 of 98 Printed: 3/23/2012 4:28:32P) Ftst X EFTA01080505 Bill To: HYPERION AIR, INC. Services: Ref. No. Description 8.14 #1 Step: 8.14.1 Step: 8.14.2 Step: 8.14.3 WO It: SC10420 Invoice Number: 7112000954 Quantity Sell Price USD Extended USD SERVICE I.00 $400.00 $400.00 Completed Completed Completed hlechanically removed corrosion front edges of the R/H upper sponson plate, Strip heavy paint for a better look JAW. GAC.SE,15802903. Removed all old sealant front around sponson plate. Treated and primed all bare metal. Resealed sponson plate. All work done IAW Standard Repair/Corrosion of Sponson Plates DWG No. SE45802903 REV.D Performed cadmium plating repair on R/H upper sponson plate. All work done IAW Standard Repair/Corrosion of Sponson Plates DWG No. 5E45802903 REV.!) Discrepancy: 8.15 R/H wing flap has 2 spots of corrosion. (Marked) Resolution: Removed light surface corrosion from R/H flap upper surface [outboard flap track &mid track]. Cleaned treated bare metal, primer and top coat as required. All work performed IAW. GAMPS 4000. Billing Method Hours Rate Total Labor USD: Flat Rate $1,150.00 Total USD: $1,150.00 Step: 8.15.1 Completed Removed and blend out light surface corrosion front the R/H Flap, upper surface around #4 track, Treated bare metal, and spot primer as required. IAN'. SRhl.51.13.20. Discrepancy: 8.16 R/H wing flap outbd Yoke is cracked in radius. Resolution: Removed damaged flap "C" track yoke assembly ( PN - 1159CM20621-3) and discarded. Installed a new replacement yoke assembly ( PN - 1159CM 20621-3) by reference of the Gulfstream IIB M/M chapter 27.06.00 entitled, Flap Actuator Yoke - Inspection. During this install, no defects were noted at this time. Labor USD: Pans USD: Total USD: Parts: Ref. No. Billing Method Hours Rate Total Flat Rate $460.00 Time and Material Part number: Description YOKE ASSY, FLT CONT - FLAP DRIVE YOKE ASSY, FLT CONT - FLAP DRIVE $988.80 $1,448.80 Quantity Sell price USD 8.16 #2 I 159CM20621-3 8.16 #3 1159CM20621-3 Extended USD $494.40 $494.40 $494.40 $494.40 Step: 8.16.1 Completed Removed damaged flap "C" track yoke assembly ( PN I159CM20621.3) and discarded. Installed a new replacement yoke assembly ( PN - 1159CM 20621-3) by reference of the Gulfstreant IIB M/N1 chapter 27-06-00 entitled, Flap Actuator Yoke • Inspection. During this install, no defects were noted at this time. Discrepancy: 8.17 R/H flap, outbd L/E flapper doors are binding on each other. Resolution: Ajusted flap door as required IAW GII AMM 27-00-00. Ops checks good.No further action required. 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_WorkOrderPrelintinaryInvoicespt Page 14 of 98 Printed: 3/23/2012 4:28:32P) Ftst X EFTA01080506 Bill To: HYPERION AIR, INC. Labor USD: Flat Rate Total USD: WO It: SC10420 Invoice Number: 7112000954 $460.00 $460.00 Discrepancy: 8.18 R/H flap, outbd yoke upper bushing phenolic is debonded from the bushing. Bushing needs to be replaced. Resolution: Removed and replaced the flap "C" track Support Assembly PN 1159CSM20836-1) by reference of the Gulfstream 11B NUM chapter 27.06.00 entitled, Flap Actuator Yoke - Inspection. During this install, no defects were noted at this time. Labor USD: Parts USD: Total USD: Parts: Billing Method Flat Rate Time and Material Hours Rate Total $3,450.00 $840.93 $4,290.93 Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.18 #4 I159CSM20836-1 SUPPORT ASSY,TRACK C-ACT 1 $628.30 $628.30 YOKE 8.18 #6 ADLF8-4005 BUSHING 2 $62.28 $124.56 8.18 #7 1159C20615-5 WASHER I $46.87 $46.87 8.18 #8 I159C20615-11 WASHER I $41.20 $41.20 Step: 8.18.1 Step: 8.18.2 Completed Completed Drilled out existing solids and huck rivets for 20 inches to gain access. Peeled back skin and inspected bolt heads and found both bolt heads mushroomed over front install. Removed fwd bolt and bagged as required. All work done LAM GLIB x.27.06-00. Removed damaged flap "C" yoke support assembly (PN -1159CSN120836-1) from flap assembly and installed a new replacement "C" yoke support assembly (PN - 1159CSM20S36-1) by reference of the Gulfstream IIB NUM chapter 27.06.00 entitled, wing flap yoke fittings - removal / installation. Discrepancy: 8.19 UH elevator trim tab has cracked skin in the area of the inner and miller hinges on the top side of the tab. Resolution: Trimmed IJH elevator outbd trim tab hinge skin area as required IAW Gulfstream drawing SE05516001. Labor USD: Total USD: Billing Method Flat Rate Hours Rate Total $460.00 $460.00 Discrepancy: 8.20 LAI aileron trim tab is missing its data plate. Resolution: Completed Traveler RS-QCT-0069 Rev.05. No defects noted on trim tah.Installcd new data plate 1AW traveler RS-QCT-0069 Rev.05. No further action required. For detail description of the work complied with see the Work Order Detail report. Unless otherwi GAC_WorkOrderPrelintinaryInvoicespt indicated, all financial values listed in this document are in US Dollars (USD). Page 15 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080507 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Billing Method Hours Rate Total Labor USD: Time and Material ST 0.25 @ $115.00 $28.75 Labor USD: Time and Material OT 017 @ $173.00 $46.71 Pans USD: Time and Material $5.97 Services USD: Time and Material $1,135.00 Total USD: $1116.43 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.20#1 1159F300411-11 NAMEPLATE 1 $5.97 $5.97 Services: Ref. No. Description Quantity Sell Price USD Extended USD 8.20 NI SERVICE 1.00 51,135.00 $1,135.00 Discrepancy: 8.21 The left side, outbd wing altachfitting located at FS 345.875 has exposed bare metal and needs to be painted to prevent corrosoin. Resolution: Painted the left side, outbd wing attachfitting located at FS 345.875 with epoxy primer IAW CAMPS 4000. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Total USD: $.160.00 Discrepancy: 8.22 The left side wing to fuselage rib., located at FS 365.500, is cracked at the bottom of the rib, through the nut plate. Resolution: Fabricated and installed doubler repair as required. All work accomplished per Gulfstream IIB, Structural Repair Manual, 51.70.00. Billing Method Hours Rate Labor USD: Time and Material ST 7.67 @ $115.00 Labor USD: Time and Material OT 0.27 @ $173.00 Total USD: Total $882.05 $46.71 $928.76 Discrepancy: 8.23 LH fuselage to wing leading edge anti-ice duct has broken bonding wire. P/N: MS25083.1BB4. Resolution: Removed broken bonding wire P/N: MS25083-1BB4 from LH fuselage to wing leading edge anti-ice duct and installed new bonding wire P/N: M$15083-1BB4 IAW GAMPS 2605. Resistance check good. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 16 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080508 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Labor USD: Pans USD: Billing Method Hours Rate Total Flat Rate $172.50 Time and Material $56.70 Total USD: $229.20 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.23 #2 PS870-B-1/2 SEALANT 6 OZ CARTRIDGE 654 I $56.70 $56.70 SEMKIT, 3.5 FL. OZ Discrepancy: 8.24 Strap on bottom of fuselage behind nose gear rusted Resolution: Billing Method Hours Rate Total Labor USD: Flat Rate $1,725.00 Total USD: $1,725.00 Step: 8.24.1 Step: 8.24.2 Completed Removed light surface corrosion on strap at bottom of fuselage behind nose gear. All work performed IAW (NIB MM 51-10-00. Completed Performed brush cadmium plating of belly strap aft of nose gear door lAW Gil-B CPCMM 20.50.05 6.D. Discrepancy: 8.25 R/H aileron boost bell crank bottom wing plate has groove carved into it from bell crank bushing. Ref Cmp 12.36 Resolution: After further inspection found not to grooved but to be a shim.No further action required on this item. Billing Method Hours Rate Total Labor USD: Flat Rate $287.50 Total USD: $287.50 Discrepancy: 8.26 R/H aileron boost bell crank has signs of chafing on top wing plate and bell crank. Ref CMP 12.36 Resolution: Cleaned area of wing plate and treated, Installed bell crank and measured for proper clearence.All work done 'ASV Gil II AIM 27-00.00 and 20.00.00. No further action required. Billing Method Hours Rate Total Labor USD: Flat Rate $287.50 Total USD: $287.50 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_Work0rderPrelintinaryinvoicespt Page 17 of 98 Printed: 3/23/2012 4:28:321:1 Ftst X EFTA01080509 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 8.27 R/H aileron boost bell crank has four bearings that are stiff and grinding. Ref CMP 12.36 Resolution: Replaced the right aileron boost bellcrank assy. with a "Repaired" bellcrank assembly P/N 1159CM20216-6 NSN and P/N 11590'420217-2 NSN. Refer to item 12.36 for removal and installation of the R/11 aileron boost bellcrank assy. Labor USD: Services USD: Total USD: Services: Ref. No. Billing Method Hours No Charge Time and Material Description Rate Total N/ C $3,004.49 $3,004.49 Quantity Sell Price USD Extended USD 8.27 #2 Vendor Supplied Labor 1.00 $1,753.56 $1,753.56 Part Ref: I1S9CM20216-2 aileron boost bellcrank 8.27 #3 REPAIR 1.00 $1,250.93 $1,250.93 Part Ref: I1S9CM20217-2 BELLCRANK ASSEMBLY Discrepancy: 8.28 Upper and lower bearing on UH aileron boost bellcrank is chiped. Resolution: Reinspected L/H aileron boost bellcrank bearings and determined that the retaining plates on the bearings are not chipped but is actually a design feature in manufacturing. No further action required pertaining to this item. Labor USD: No Charge N/ C Discrepancy: 8.29 CMP GLIB 803013 Engine Starter Assembly (Left) - Removal / Installation Resolution: COMPLIED WITH CMP GIIB 803013 Engine Starter Assembly (Left) - Removal / Installation. Removed Left Engine Starter Assy P/N 383700-1-1 S/N P-16758 for spline lubrication and inspection and re-installed StarterP/N 383700-1.1 S/N P-16758 IAW G-2B AMM 80.01.00 with no defects noted. Billing Method flours Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.30 CMP GHB 803012 Engine Starter Splines (Left) - Lubrication / Inspection For detail description of the work complied with see the Work Order Detail report. GAC_WorkOrderPreliminaryInvoicespt Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). Page 18 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080510 Bill To: HYPERION AIR, INC. WO*: SC10420 Invoice Number: 7112000954 Resolution: COMPLIED WITH CMP GIIB 803012 Engine Starter Splines (Left) - Lubrication/ Inspection with satisfactory results IAN G2-B AMM 80-01-00. Billing Method Flours Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.31 Nylon plugs (anti torsion bumper) on L/H aileron actuator worn and need replacing. ( 4 ea ) Resolution: Removed 4 worn plugs and installed 4 new plugs P/N 87048 on UH aileron actuator lAW GIIB AMM 27-00-00. Billing Method Flours Rate Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $90.64 Total USD: $320.64 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 831 NI 87048 PLUG 4 $22.66 $90.64 Discrepancy: 8.32 R/Ii aileron actuator anti torsion bumpers(4) need replaced. P/N 87048 Ref CMP 12.37 Resolution: Removed 4 worn plugs and installed 4 new plugs P/N 87048 in the R/14 aileron actuator IAW GIIB AMM 27-00-00. Billing Method Hours Rate Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $90.64 Total USD: $320.64 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 83211 87048 PLUG 4 $22.66 $90.64 Discrepancy: 8.33 Left outbd flight spoiler bellcrank assy to be sent to Savannah for insp. Resolution: Replaced the L/H outboard flight spoiler bellcrank assy. with repaired bellcrank P/N 1159CM20209-5. Refer to item 12.153 for Removal and installation of bellcrank assn. Billing Method Hours 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_WorkOrderPreliminaryInvoicespt Page 19 of 98 Printed: 3/23/2012 4:28:32P) Ftst X EFTA01080511 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Services USD: Time and Material $1,322.88 Total USD: $1,322.88 Services: Ref. No. Description Quantity Sell Price USD Extended USD 833 #1 Vendor Supplied Labor 1.00 $1,322.88 $1,322.88 Part Ref: 1159CM20209-5 CRANK ASSEMBLY Discrepancy: 8.34 Right outbd flight spoiler bellcrank assy to be sent to Savannah for insp. Resolution: Replaced the R/H outboard flight spoiler bellcrank P/N 1159CM20209-6 and installed "repaired" bellcrank P/N 1159CM20209-6. Refer to item 12.149 for Removal and installation of bellcrank. Services USD: No Charge N/ C Discrepancy: 8.35 Right inbd flight spoiler bellcrank assy to be sent to Savannah for insp. Resolution: Replaced the R/H inboard flight spoiler bellcrank with a "repaired" bellcrank P/N 1159CM20208-2. Refer to item 12.152 for Removal and installation of bellcrank. Billing Method Hours Rate Total Services USD: Time and Material $1,995.50 Total USD: $1,995.50 Services: Ref. No. Description Quantity Sell Price USD Extended USD 835 #2 Vendor Supplied Labor 1.00 $1,995.50 $1,995.50 Part Ref: 1159CM20208-2 CRANK ASSEMBLY Discrepancy: 8.36 IJH elevator hinge #2, hinge to airframe through hole (2-3) is burred on one end. Needs to be de-burred. Resolution: Removed burr as required and remeasured 1./H elevator hinge #2, hinge to airframe through hole (2-3) Hole measurement is within limits. Work performed 1AW GLIB MM 27-01.00. and SRM 51.13-10. Billing Method Hours 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_Work0rderPreliminaryInvoice.rpt Page 20 of 98 Printed: 3)23/2012 4:28:32P) Rd X EFTA01080512 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 8.37 R/H elevator hinge #4, outbd bushing (4-2) is No-Go. P/N 1159CSM20118.19. Resolution: Removed bad hat bushing and cleaned inner surface. Prepped and installed new bushing P/N 1159CSM20118-19 JAW Drawing SE055000901 rev.T. No further action required. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Parts USD: Time and Material $170.28 Total USD: $630.28 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 837 #1 1159CSM20118-19 PAD ASSY,ELEV HINGE-FLT CUNT 1 $170.28 $170.28 Discrepancy: 8.38 R/H elevator trim tab hinge #1 bearing is frozen. Resolution: Removed corroded Rill elevator trim tab hinge #1 bearing P/N MS14101.4 and replaced with new bearing P/N MS14101-4 IAW GAC drawing GAB14E. Checks good. Billing Method Houri. Rate Total Labor USD: Flat Rate $460.00 Parts USD: Time and Material $18.85 Total USD: $478.85 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 838 #1 MS14101-4 BEARING,PLAIN,SELF LUB & I $18.85 $18.85 ALIGN Discrepancy: 8.39 R/H elevator trim tab hinge #2 bearing is frozen. Resolution: Removed R/H elevator trim tab hinge #2 bearing P/N MS14101-4 and replaced with new bearing P/N MS14101.4 IAW GAC drawing GAB14E. Checks good. Billing Method flours Rate Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $18.85 Total USD: $478.85 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 839 #1 MSI4101-4 BEARING,PLAIN,SELF LUB & I $18.85 $18.85 ALIGN 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 21 of 98 Printed: 3/23/2012 4:28:32PP Rd X EFTA01080513 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Discrepancy: 8.40 R/H elevator trim tab, outbd push pull rod, aft rod end is frozen. Bearing P/N REP4M6. Nut P/N AN316.6R. Resolution: Removed the R/H elevator trim tab outboard push pull rod's aft corroded rod end P/N UNK S/N NSN and installed a new rod end / bearing P/N MS21151.SC S/N NSN and new nut P/N AN316-6R S/N NSN. Refer to Gulfstream Drawing 1159C20455 Rev. D for work performed. Billing Method Flours Rate Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $76.48 Total USD: $536.48 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.40 #1 MS21151-8C ROD END WITH KEY-WAY I $76.22 $76.22 8.4082 AN316.6R NUT 1 $0.26 $0.26 Discrepancy: 8.41 R/H elevator trim tab #3 hinge bearing is corroded. Resolution: Removed corroded Rai elevator trim tab hinge #3 bearing P/N MS14101.4 and replaced with new bearing P/N MS14101-4 IAW GAC drawing GAB14E. Checks good. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $18.85 Total USD: $478.85 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.41 #1 MSI4101-4 BEARING,PLAIN,SELF LUB & I $18.85 $18.85 ALIGN Discrepancy: 8.42 R/H elevator trim tab hinge #1 bushings are corroded. Resolution: Removed corroded RAI elevator trim tab hinge #1 lower hat bushings P/N's 1159CSM20155-1 ( 2 each) and replaced with new hat bushings P/N's 1159CSM20155.1 ( 2 each ) IAW GAC Drawling # SE05000901-T. Checks good. Billing Method flours Rate Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $122.52 Total USD: $582.52 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.42 #1 1159CSM20155-1 BUSHING 2 $43.26 $86.52 8.42#2 GABI0F4-4 BUSHING I $36.00 $36.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 22 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080514 Bill To: HYPERION AIR, INC. WO #: 5C10420 Invoice Number: 7112000954 Step: 8.42.1 Completed Removed corroded R/H elevator trim tab hinge #1 lower hat bushings P/N's 1159CSM20155-1 ( 2 each) and replaced with new lower hat bushings P/N's I 159CSM20155-1 ( 2 each ) IAW GAC Drawling # SE05000901-T. Checks good. Discrepancy: 8.43 L/H wing, outbd flap drive rod is scored. Resolution: Removed L/H wing outbd flap drive shaft . P/N 1159SCC213-17, S/N unreadable. Installed new flap shaft P/N 1159SCC213-17 , S/N 3232 IAW GLIB AMM 27-06-00. See item 8.123 for rigging of flaps. Billing Method Hours Rate Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $4,557.01) Total USD: $4,787.00 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.43 #1 1159SCC213-17 SHAFT, WING FLAP &SIMII/Fit 1 $4,557.00 $4,557.00 Discrepancy: 8.44 L/H wing, second from outbd flap drive rod is scored. Resolution: Removed L/H wing second from outbd flap drive shaft .P/N 1159SCC213-13, S/N unreadable. Installed new flap shaft P/N 1159SCC213-13, S/N 2034 IAW GIIB AMM 27.06.00. See item 8.123 for rigging of flaps. Billing Method Hours Rate Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $4,556.67 Total USD: $4,786.67 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.44 81 1159SCC2I3-13 SHAFT 1 54,556.67 $4,556.67 Discrepancy: 8.45 L/H elevator trim tab hinge #1 bearing is corroded. Resolution: Removed corroded L/H elevator trim tab hinge #1 bearing P/N MS14101.4 and replaced with new bearing P/N MS14101-4 JAW GAC drawing GAB14E. Checks good. Labor USD: Pans USD: Total USD: Parts: Ref. No. Billing Method Hours Rate Total Flat Rate $460.00 Time and Material $18.85 Part number: $478.85 Description Quantity 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_WorkOrderPrelintinaryInvoicespt Page 23 of 98 Printed: 3/23/2012 4:28:32PP Rd X EFTA01080515 Bill To: HYPERION AIR, INC. WO ft: SC10420 Invoice Number: 7112000954 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.45 #1 MSI4101-4 BEARING,PLAIN,SELF LUB & 1 $18.85 ALIGN $18.85 Discrepancy: 8.46 IJH elevator trim tab hinge #2 bearing is corroded / frozen. P/N MS21232-4. Resolution: Removed corroded L/H elevator trim tab hinge #2 bearing P/N MS14101.4 and replaced with new bearing P/N MS14101.4 IAW GAC drawing GAB14E. Checks good. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Paris USD: Time and Material $18.85 Total USD: $478.85 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.46 #1 MSI4101-4 BEARIN(:,PLAIN,SELF LUB & I $18.85 $18.85 ALIGN Discrepancy: 8.47 L/H elevator trim tab hinge #3 bushings are corroded. P/N 1159CSM20155.1 and P/N 1159CSM20155-5. Resolution: Removed corroded L/H elevator trim tab hinge #3 lower hat bushings P/N 1159CSM20155-land P/N 1159CSM20155-5 and replaced with new hat bushings P/N 1159CSM20155.1 and P/N 1159CSM20155-5 IAW GAC Drawing # SE05000901-T. Checks good. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Paris USD: Time and Material $98.26 Total USD: $558.26 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.47 #1 1159CSM20155-1 BUSHING 1 $43.26 $43.26 8.47 #2 1159CSM20155-5 BUSHING 1 $55.00 $55.00 Discrepancy: 8.48 UH elevator trim tab hinge #2 lower hat bushings are corroded. Resolution: Removed corroded L/H elevator trim tab hinge #2 lower hat bushings P/N's 1159CSM20155.1 and replaced with new hat bushings P/N's 1159CSM20155-1 IAW Drawing # SE05000901-T. Checks good. Labor USD: Parts USD: Billing Method flours Rate Total Flat Rate $460.00 Time and Material $86.52 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_WorkOrderPreliminaryInvoicesm Page 24 of 98 Printed: 3/23/2012 4:28:32P) Flee X EFTA01080516 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Total USD: $546.52 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.48 #1 1159CSM20155-1 BUSHING 2 $43.26 $86.52 Discrepancy: 8.49 IJH elevator trim tab hinge #2 slip bushing is out of limits. P/N SE05000901.911P1.5 (oversized). Resolution: Removed the old hardware and cleaned the attach point fittings. Greased all of the new hardware and slip bushings provided in the 72month install Kit. Installed New slip bushing P/N SE05000901-5. Work performed JAW GLIB MM 27.04.00. Billing Method Hours Rate Total Labor USD: Time and Material OT 0.27 @ $173.00 $46.71 Parts USD: Time and Material $388.64 Total USD: $435.35 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.49 #1 SE05000901-911P1-5 REPAIR BUSHING 1 $388.64 $388.64 Discrepancy: 8.50 L/H elevator trim tab hinge #2 hole 2-1 is No-Go. (Slip bushing hinge hole) Squawk 8.49 will resolve this squawk. Resolution: Removed the old hardware and cleaned the attach point fittings. Greased all of the new hardware and slip bushings provided in the 72month install Kit. Installed New slip bushing P/N SE05000901-5. Work performed IAW GIIB MM 27-04-00. REF Item 8.49 Billing Method Hours Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.51 Rill elevator trim tab hinge #3 bushings are corroded. Resolution: Removed corroded R/H elevator trim tab hinge #3 lower hat bushings P/N 1159CSM20155-land P/N 1159CSM20155.5 and replaced with new hat bushings P/N 1159CSM20155.1 and P/N 1159CSM20155-5 IAW GAC Drawing # SE05000901-T. Labor USD: Paris USD: Billing Method Houri. Rate Total Flat Rate $460.00 Time and Material $98.26 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 25 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080517 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Total USD: $558.26 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.51 #1 1159CSM20155-1 BUSHING I $43.26 $43.26 8.51 #2 II59CSM20155-5 BUSHING I $55.00 $55.00 Discrepancy: 8.52 IJH elevator trim tab hinge #3 hole 3.1 bushing is No-Go. Bushing being replaced under squawk 847. Resolution: Removed L/H elevator trim tab hinge #3 lower hat bushing 3.1 P/N 1159CSM20155.1 and replaced with new hat bushing P/N 1159CSM20155.1 IAW GAC Drawing # SE05000901-T. Checks good. See 8.47 for corrective action, bushing replacement. Billing Method Hours Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.53 Data tags on flight controls ne