Gulfstreant

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$471.24 20 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 need paint removed to see part and serial numbers. Resolution: Removed paint on data tags (10 ea.) on flight controls to see part and serial numbers. All work performed IAW GAMPS 4000. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Total USD: $460.00 Discrepancy: 8.54 CMP GLIB 321810 BLEED L WHEEL BRAKES. See 12.51 & 12.52 Resolution: COMPLIED WITH CMP GIIB 321810 BLEED L WHEEL BRAKES. No defects noted. Work done IAW CMP 321810 & GIIB M/M 32-04-01. Complied with GIIB CMP 321815 Brake (Right) - Bleeding Procedure. No defects noted. Work done IAW CMP 321815 & GIIB M/M 32-04-01. 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 26 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080518 Bill To: HYPERION AIR, INC. WO #: SC10420 Discrepancy: 8.55 CMP GlIB 321315 Antiskid Control System - Functional Test. Invoice Number: 7112000954 See 12.51 & 12.52 Resolution: COMPLIED WITH CMP GIIB 321315 Antiskid Control System - Functional Test. No defects noted. Work done IAW CMP 321315 & GIIB M/M 32-04-02. Billing Method Hours Rate Total Labor USD: Flat Rate $172.50 Total USD: $172.50 Discrepancy: 8.56 CMP GIIB 321305 Wheel Brake (GIIB) - Functional Test. See 12.51 & 12.52 Resolution: COMPLIED WITH CMP GIIB 321305 Wheel Brake ((MB) - Functional Test. No defects noted. Work done WV CHIP 321305 & GIIB M/M 32.04.01. Billing Method IOW!, Rate Total Labor USD: Flat Rate $287.50 Total USD: $287.50 Discrepancy: 8.57 L/H wing upper sponson plate is corroded. Resolution: Removed sealent from around UH wing sponson plate. All work performed IAW GlIB MM 51-10.00. Treated and primed all bare metal. Resealed sponson plate.Evaluated remaining thickness of sponson after corrosion removal and found to bw within limits and acceptable for continued service IAW GAC drawing 5E45802903 limitations as stated in GAC engineering disposition CS278586.Performed cadmium plating repair on L/H upper sponson plate. All work done JAW Standard Repair/Corrosion of Sponson Plates DWG No. 5E45802903 REV.D Billing Method flours Rate Total Labor USD: Time and Material ST 20.60 @ $115.00 $2,369.00 Labor USD: Time and Material OT 2.77 @ $173.00 $479.21 Services USD: Time and Material $400.00 Total USD: $3,248.21 Services: Ref. No. Description Quantity Sell Price USD Extended USD 8.57 #1 SERVICE 1.00 $400.00 $400.00 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 27 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080519 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Step: 8.57.1 Step: 8.57.2 Completed Removed sealent from around Lift wing sponson plate. All work performed IAIV GlIB MM 51-10-00. Completed Treated and primed all bare metal. Resealed sponson plate. Performed cadmium plating repair on Ull upper sponson plate. AU work done IAIV Standard Repair/Corrosion of Sponson Plates DWG No. 5E45802903 REV.D Discrepancy: 8.58 Several spots inboard of L/H wing leading edge need sealant. Resolution: Replaced missing sealant IASI/ GIIB SRM 51-22-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.42 @ $115.00 $393.30 Total USD: $393.30 Discrepancy: 8.59 While complying with CMP#575005 , Found Hydraulic line chaffing against structure at L/H wing trailing edge outboard of flap well. Resolution: Repostioned Hydraulic line and wrapped with protective wrap. All work done IAW GlIB AMM 20.00.00.Checks good. No further action required. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Total USD: $460.00 Discrepancy: 8.60 While complying with CNIP# 575005, Found a hydraulic leak has caused the under aircraft ( Keel ) sections to have Bare Metal. Resolution: Performed leak checks and found no leaks.Spoke with customer and was informed that this was an issue of the hydraulic system being over serviced. This issue was resolved prior to this visit. Paint was stripped, prepped, primed, and painted to match under item 9.1. No further action required on this item. Billing Method Hours Rate Total Labor USD: Time and Material ST 0.25 @ $115.00 $28.75 Total USD: $28.75 Discrepancy: 8.61 All fuel tank access panels removed for X-Rays require cleaning because of excessive amounts of Fuel Lube applied to panels and wing mounting surfaces. 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 28 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080520 Bill To: HYPERION AIR, INC. WO #: SC10-I20 Invoice Number: 7112000954 Resolution: Cleaned and Installed all fuel panels removed for x-ray IAW CUB AMM 57-00.00. Performed pressure check with no defects noted. Billing Method flours Rate Total Labor USD: Flat Rate $1,150.00 Total USD: 81,150.00 Discrepancy: 8.62 Right winglet attach pin holes have corrosion in attach bores. 5 places on wing and 8 on winglet. No corrosion found on pins. Corroded holes marked. Ref 12.66 inspection. Resolution: Accomplished right winglet sleeve bore hole repairs to the vertical (wing side) attachments and the horizontal (winglet side) attachments. All work was performed by reference of the Gulfstream Aerospace repair drawings No. 5E35809903 rev. "C" entitled, Sleeve installation - winglet attachment, Cres. Map of vertical (wing side) repairs are as follows. Fwd. Inhd. 2nd. oversize new set (.9370 - 9390) PN SE35809903-19. SE35809903.39. Center outbd. remains at original standard size. Inbd. center & inbd. Aft , Fwd. outbd. & Aft. outbd. are at 1st. oversize new set (.9057 - .9077) PN - SE35809903.15 & SE35809903.35. Map of horizontal (winglet side) repairs are as follows. Top row from Fwd. to Aft. (5 total) are 1st. oversize set (.9057 - .9077) PN - SE35809903-17 & SE35809903-37. Lower row Fwd. No. 1, 2 , 3 & 5 remain at original standard size. No. 4 and 5 are 1st oversize set (.9057 - .9077) PN - SE35809903- 17& 5E35809903-37. Billing Method Hours Rate Total Labor USD: Time and Material ST 36.63 @ $115.00 $4,212.45 Labor USD: Time and Material OT 2.74 @ $173.00 $474.02 Pans USD: Time and Material $6,493.49 Total USD: $11,179.96 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.62 #1 SE35809903-15 SLEEVE 1 $70.00 $70.00 8.62#2 SE35809903-19 SLEEVE I $123.60 $123.60 8.62 #3 SE35809903-35 SLEEVE 1 $226.00 4226.00 8.62 #4 SE35809903-39 SLEEVE 1 472.10 $72.10 8.62 #5 SE35809903-15 SLEEVE 8 $70.00 $560.0() 8.62 #6 SE35809903-35 SLEEVE 8 $226.00 $1,808.00 8.62#7 SE35809903-19 SLEEVE I $123.60 $123.60 8.62 #8 SE35809903-39 SLEEVE I S72.10 $72.10 8.62#9 NASI165-43L BOLT 8 $131.43 8.62 #10 SE35809903-17 SLEEVE 12 $1,051.44 $30.21 $362.52 8.62 #11 SE35809903-37 SLEEVE 12 $129.42 $1,553.04 8.62 #12 NASI165-42L BOLT 5 $39.00 $195.00 8.62 #14 NASI165E43B BOLT 8 $43.68 8.62 #I5 NAS1165E40B BOLT 3 $5.46 $18.24 $54.72 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 29 of 98 Printed: 3/23/2012 4:28:32P) Ret X EFTA01080521 Bill To: HYPERION AIR, INC. WO*: SC10420 Invoice Number: 7112000954 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.62 #16 GAS55IB3C9 SCREW 100 $1.21 $121.00 8.62 #18 P5870-B-2 SEALANT I $56.69 $56.69 Discrepancy: 8.63 While complying with CNIP*575091, ( Ailerons leading edge and ballast weight corrosion inspection ) Found protective paint finish on both ailerons leading edge ballast's cracking/missing. Resolution: Removed light corrosion on ballast weight as required. Treated and primed IAW GLIB SRM 51-13-20. Billing Method Flour> Rate Total Labor USD: Flat Rate $460.00 Total USD: $460.00 Discrepancy: 8.64 While complying with CNIP*575086 ( Ailerons leading edge and ballast weight corrosion inspection ) Found corrosion on sections 4&5 ( sections noted on aileron ) of LH aileron's ballast weight leading edges and attachment fasteners. Resolution: Removed light corrosion on ballast weight as required. Treated and primed JAW GIIB SRM 51-13.20. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Total USD: $460.00 Discrepancy: 8.65 While complying with CNIP#575086 ( Ailerons leading edge and ballast weight corrosion (LEFT) inspection ) Found middle static wick on aileron cracked. Resolution: Installed new static wick P/N 2-16SC-1 , S/N N/A IAW GIIB AMNI 23.60.00. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Total USD: $460.00 Discrepancy: 8.66 Found on the Cabin threshold a potted insert needs to be replace. 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 30 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080522 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Resolution: Installed cabin threshold potted insert P/N TYE2001-04-08. All work performed IAW GHB MM 25.20.00. No defects noted. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.05 @ $115.00 $350.75 Total USD: $350.75 Discrepancy: 8.67 LJH flap, outbd yoke upper bushing phenolic is debonded from the bushing. Bushing needs to be replaced. Resolution: Removed damaged flap "C" track yoke assembly ( PN - 1159CM20621-3) and discarded. Installed a new replacement yoke assembly ( PN - 1159CM 20621-3). Also removed and replaced the flap "C" track Support Assembly PN - 1159CSM20836-1) 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. Billing Method Hours Rate Total Labor USD: Flat Rate $3,450.00 Parts USD: Time and Material $3,147.28 Total USD: $6,597.28 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.67 #4 1159CSM20836-1 SUPPORT ASSY,TRACK C-ACT $628.30 $628.30 YOKE 8.67 #5 NASI921B04-02 BLIND RIVET 300 $1.22 $366.00 8.67 #6 NAS1921604-03 RIVET 200 $1.37 $274.00 8.67 #8 NASI9211004-02 RIVET 300 $3.68 $1,104.00 8.67 #9 NAS1921M04-03 RIVET 200 $2.85 $570.00 8.67 #10 NAS6605-58 BOLT, HEX HEAD, CLOSE TOL, 2 $11.93 $23.86 UNDRILLED 8.67 #I I 11590 S20005.35 WASHER 2 $89.32 $178.64 8.67 #12 NIS21042L5 NUT, SELF-LOCKING RING BASE 2 $1.24 $2.48 Discrepancy: 8.68 UH elevator hinge fitting A-7 bushing ID is No-Go. New bushing (P/N 115915'420094-25) is included in "install kit". Resolution: Removed old bushing and installed new bushing P/N 1159CSM20094 as required IASI/ 27-00-00. Parts included in 72 Month kit. Billing Method Houri. Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 For detail description of the work complied with see the Work Order Detail report. GAC_WorkOrderPrelintinaryInvoicespt Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). Page 31 of 98 Printed: 3)23/2012 4:28:32PD Rst X EFTA01080523 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 8.69 R/H aileron #1 hinge fitting inbd hole 1.3 is corroded. (Clean, Treat, and remeasure). Resolution: Removed corrosion, treated and remeasured the R/H aileron #1 hinge fitting inbd hole 1-3. Hole is within limits. Work performed IAW GIIB MM 27-02-00 and SRM 51.13-10. Billing Method Hours Rate Total Labor USD: Flat Rate $690.09 Total USD: $690.00 Discrepancy: 8.70 R/H aileron #1 hinge fitting aileron to wing, hole 1-2 is corroded. (Clean, Treat, and remeasure). Resolution: Removed corrosion, treated and remeasured the R/H aileron #1 hinge fitting hole 1-2. Hole measurment is within limits. Work performed IAW GIIB MM 27-02-00 and SRM 51-13-10. Billing Method Flours Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.71 L/H aileron #1 hinge fitting center attach hole 1.2 is corroded. (Clean, Treat, and remeasure). Resolution: Removed corrosion, treated and remeasured the L/H aileron #1 hinge fitting hole 1-2. Hole measurment is within limits. Work performed IAW GIIB MM 27-02-00 and SRM 51-13.10. Billing Method Hours Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.72 L/H aileron #3 wing attach fitting bolt hole, upper and lower bushings are corroded. P/N GAB10C5-12. 2ea Resolution: Removed corroded L/H aileron #3 wing attach fitting upper and lower hat bushings P/N's GABI0C5-12 and replaced with new hat bushings P/N's GABI0CS-12 IAW GAC Drawing # SE05000901-T. Checks good. 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 32 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080524 Bill To: HYPERION AIR, INC. WO*: SC10420 Invoice Number: 7112000954 Labor USD: Parts USD: Flat Rate $690.00 Time and Material $39.34 Total USD: $729.34 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.72 #1 GABI0CS-12 BUSHING 2 $19.67 $39.34 Discrepancy: 8.73 Found small amounts of corrosion in 10 bores of the LAI winglet attach hardware holes. Resolution: Accomplished left winglet sleeve bore hole repairs to the vertical (wing side) attachments and the horizontal (winglet side) attachments. All work was performed by reference of the Gulfstream Aerospace repair drawings No. 5E35809903 rev. "C" entitled, Sleeve installation - winglet attachment, Cres. Map of vertical (wing side) repairs are as follows. Fwd. Inbd. & Aft inbd. 1st oversize new set (.9057 - 9077) PN - 5E35809903-15. SE35809903-35. Center inbd. remains at original standard size. Fwd. outbd. center & Aft , are at 1st. oversize new set (.9057 - .9077) PN - SE35809903-15 & SE35809903.35. Map of horizontal (winglet side) repairs are as follows. Top row from Fwd. No. 1, 2, 4, and 5 are at 1st. new oversize set (.9057 - .9077) PN SE35809903-17 & SE35809903-37. Top row No. 3 remains at original standart size. Lower row No. 2,3,4,&5 remain at original standard size. Lower No. 1 is at 1st oversize new set (.9057 - .9077) PN - SE35809903-17 & 5E35809903-37. Labor USD: Pans USD: Total USD: Billing Method Hours Rate Total Flat Rate No Charge $2,300.00 N/ C $2,300.00 Discrepancy: 8.74 Left inbd flight spoiler bellcrank assy to be sent to Savannah for insp. Resolution: Replaced the LAI inboard flight spoiler bellcrank with a "repaired" bellcrank P/N II59SB30144-11. Refer to item 12.150 for Removal and installation of bellcrank. Billing Method Hours Rate Total Services USD: Time and Material $1,800.86 Total USD: $1,800.86 Services: Ref. No. Description Quantity Sell Price USD Extended USD 8.74 #1 Vendor Supplied Labor 1.00 $1,800.86 $1,800.86 Pan Ref: 11595B30144-11 CRANK ASSY Discrepancy: 8.75 All three A/C oxygen bottles need new "O" rings at air line nut because they are worn. 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 33 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080525 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Resolution: Removed "0" rings on all 3 oxygen cylinder air lines and installed new o-rings P/N MS22012-6 lAW G-IIB AMM 35.00.00. Labor USD: Pans USD: Total USD: Parts: Billing Method Hours Rate Total Time and Material ST 6.81 @ $115.00 $783.15 Time and Material $48.04 $831.19 Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.75 #1 M522012-6 PACKING RING 4 $8.70 $34.80 8.75 #3 MS28775-006 PACKING-PORT FITTING,3/16 LINE 4 $0.26 $1.04 8.75 #4 M528778-5 O-RING, TUBE FITTING 4 $3.05 $12.20 PREFORMED Discrepancy: 8.76 Rudder hinge #1 bearing is rough and corroded. Resolution: Removed old bearing P/N MS28913.5C and replaced with a new bearing P/N MS289I3-5C on rudder hinge #1 IAW GAC engineering drawing # SEO5000901 -T. Checks good. Labor USD: Paris USD: Total USD: Parts: Ref. No. Billing Method Hours Rate Total Flat Rate Time and Material $460.00 $113.82 $573.82 Pan number: Description Quantity Sell price USD Extended USD 8.76 #1 M528913-SC BEARING 1 $113.82 $113.82 Step: 8.76.1 Completed Removed bearing retainer and bearing on rudder hinge #1 lAW GAC engineering drawing # SEO5000901 -T. Discrepancy: 8.77 Rudder hinge #2 bearing is rough and corroded. Resolution: Removed old bearing PIN MS28913.5C and replaced with new bearing P/N M528913-5C on rudder hinge #2 lAW GA(' drawing # SEO5000901-T. Checks good. Labor USD: Pans USD: Total USD: Parts: Billing Method Hours Rate Total Flat Rate Time and Material $460.00 $133.07 $593.07 Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.77 #1 M528913-5C BEARING 1 $113.82 $113.82 8.77#2 M520615-5M16 RIVET, MONEL UNIVERSAL HEAD 25 $0.77 $19.25 For detail description of the work complied with see the Work Order Detail report. Unless otherwi GAC_WorkOrderPrelintinaryInvoice.rpt indicated, all financial values listed in this document are in US Dollars (USD). Page 34 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080526 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Step: 8.77.1 Completed Removed bearing retainer and bearing front rudder hinge #2. Step: 8.77.2 Completed Removed bearing retainers and bearing from rudder hinge #3. (written in Error refer to squawk 8.78.11 Discrepancy: 8.78 Rudder hinge #3 bearing is rough and corroded. Resolution: Removed old bearing P/N M528913.5C and replaced with a new bearing P/N NIS28913-5C on rudder hinge #3 IAW (AC drawing SEO500090-T. Checks good. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $113.82 Total USD: $573.82 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.78 NI MS28913-SC BEARING 1 $113.82 $113.82 Step: 8.78.1 Completed Removed bearing retainers and bearing from rudder hinge #3 IAW GAC drawing # SEO500090-T. Discrepancy: 8.79 Rudder hinge #1 attach bolt, airframe side, hole is oversized. Resolution: After re-evaluation and further inspection of Rudder # 1 airframe hinge attach point found hinge point fitting to be within limits IAW GlIB MM 27.02.00 requirements. No further action required. Billing Method Hours Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.80 Rudder hinge #2 attach bolt, airframe side, hole is oversized. Resolution: After re-evaluation and further inspection of Rudder # 2 airframe hinge attach point found hinge point fitting to be within limits IAW GlIB MM 27.03.00 requirements. No further action required. Billing Method Hours Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.81 Rudder hinge #2 rudder fitting upper hole 2-2 is No-Go. 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 35 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080527 Bill To: HYPERION AIR, INC. WO It: SCI0420 Invoice Number: 7112000954 Resolution: Removed upper hat bushing 2.2 on rudder hinge fitting #2 PN. 1159SB30210-43 and installed a new bushing PN.1159SB30210-43 IAW (MC drawing # 5E05000901-T. Checks good. Billing Method Flours Rate Total Labor USD: Flat Rate $690.00 Pans USD: Time and Material $12.88 Total USD: $702.88 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.81 #1 11595B30210-43 BUSHING 1 $12.88 $12.88 Discrepancy: 8.82 Rudder hinge #3 attach bolt hole 3.4 is No-Go. Resolution: Accomplished rudder No. 3 hinge attachment bore hole repair by reference of the Gulfstream Structural engineering drawing No. SE05000901 rev. "N" entitled, STD - repair - control surface hinge fittings. Match cut fitting bore hole to accept a new replacement 1st oversize attachment bolt PN - NAS6604D138X (0.2647). Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $924.37 Total USD: $1,384.37 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.82 #1 SEO5000901-913D1-26 BUSHING I $666.87 $666.87 8.82 #2 NAS6604DI38X BOLT 1 $257.50 $257.50 Discrepancy: 8.83 Rudder hinge #4 attach bolt ears, hat bushings 4.2 are No-Go. Resolution: Removed hat bushings on rudder hinge #4 P/N GABIOE7.6 and installed new bushings PN. GABI0E7-6 as required JAW (MC drawing # SE05000901-T. Checks good. Billing Method Flours Rate Total Labor USD: Flat Rate $690.00 Pans USD: Time and Material $59.74 Total USD: $749.74 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.83 #1 GABI0E7-6 BUSHING 2 $29.87 $59.74 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_WorkOrderPrelintinarylmoice.rpt Page 36 of 98 Printed: 3/23/2012 4:28:32PP Rd X EFTA01080528 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Discrepancy: 8.84 Rudder torque tube sleeve 4-3 are No-Go and corroded. Resolution: Corrosion was found on the surface of the inner torque tube sleeve was cleaned and treated by reference of the Gulfstream Aerospace engineering drawing 5E05417902 rev. "D" entitled, Material Removal Limits - Vertical Stabilizer Torque Tube. The torque tube bushing (sleeve) was replaced with new. Reference 72 mo. inspection for replacement of bushing. Billing Method Hours Rate Total Labor USD: Flat Rate $690.00 Parts USD: Time and Material $1,227.33 Total USD: $1,917.33 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.84 NI 1159CSM20091-3 SLEEVE 1 $128.96 $128.96 8.84 #2 1159BM20959-11 PIN 1 $143.92 $143.92 8.84 #3 NAS6604H4 BOLT HEX HD-CL TOL,DRILLED HD 8 $2.99 $23.92 8.84 #4 NAS334CP23 BOLT 5 $3.09 $15.45 8.84 #5 NAS334CP22 BOLT 3 $13.39 $40.17 8.84 #8 NAS3004-14 BOLT 2 $330.88 $661.76 8.84 #9 HL218.10.17 HILOK 3 $44.45 $13335 8.84 #10 HL2I8-8-12 HILOK 3 $26.60 $79.80 Discrepancy: 8.85 Rh Flight spoiler actuator fwd bearing pin is burred/defective. Resolution: Complied with by replacing the bad RH flight spoiler actuator and installing a Modified RH flight spoiler actuator P/N 1159SCH250-30, REF Item S/N 1731. Work performed IAW GlIB MM 27-02-00. 12.151 Billing Method Hours Rate Total Labor USD: No Charge NI C Pans USD: Time and Material $16.506.90 Total USD: $16,506.90 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.85 #2 I159SCH250-30 ACTUATOR, HYDRAULIC FLIGHT I $16,500.00 $16,500.00 SPOILER (R/H) 8.85 #3 NASI612-6A O-RING 8 40.48 $3.84 8.85 #4 NASI612-8A SEAL 6 40.51 $3.06 Discrepancy: 8.86 Rh flight spoiler actuator rear ball bearing is seized. Resolution: Complied with by replacing the bad RH flight spoiler actuator and installing a Modified RH flight spoiler actuator P/N 1159SCH250-30, S/N 1731. Work performed IAW GlIB MM 27-02-00. REF Item 12.151 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_WorkOrderPrelintinaryInvoice.rm Page 37 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080529 Bill To: HYPERION AIR, INC. Labor USD: No Charge WO*: SC10420 Invoice Number: 7112000954 N/ C Discrepancy: 8.87 Lh Flight spoiler actuator fwd bearing pin is burred/defective. Resolution: Complied with by replacing the bad LH flight spoiler actuator and installing a Nlodilicd LH flight spoiler actuator P/N 1159SCH250-29, S/N 2002. Work performed IAW (MB MM 27.02-00. REF Item 12.148 Labor USD: No Charge N/ (' Discrepancy: 8.88 Left "C " Flap track lower inbd and outbd failed measure check after corrosion removal (Ref. to item 8.7) Resolution: Reworked and refinished left "C" flap track IAW Gulftream drawing 5E05811901. Flap track is acceptable for continued normal operation per eng. despo CS278586. No further action required on this item. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.50 @ $115.00 $172.50 Total USD: $172.50 Discrepancy: 8.89 Rh outboard flap actuator cannon plug has 2 bare wires. Resolution: Inspected the R/H outboard flap actuator cannon plug wires and found no broken wire strands. Installed heat shrink sleave over the wire on RH outboard flap actuator cannon plug. All work was done JAW Gulfstream GLIB AMM 20.10.01. Billing Method !lours Rate Total Labor USD: Time and Material ST 1.00 @ $115.00 $115.00 Total USD: $115.00 Discrepancy. 8.90 Resolution: While inspecting the rudder trim actuator found it to he sticking in the full left and full right positions. 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 38 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080530 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 8.91 Found the elevator Auto Pilot servo FWD cable to be damaged and its bellcrank cable guide to be deeply grooved. Resolution: Removed tension and disconnected elevator autopilot servo cable and removed cable guide and inspected Cable and bell crank found no damage on cable assy. or bellcrank. Blended out groove on cable guide. Installed cable and components. All work performed IAW GIIB MM 22.00.00. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.12 @ $115.00 $358.80 Pans USD: No Charge N/ C Total USD: $358.80 Step: 8.91.1 Completed Removed tension and disconnected elevator autopilot servo cable and removed cable guide and inspected Cable and bell crank found no damaged on cable assy. or bellcrank. (Cable stop is on order to be replaced.) AU work performed IAW GIIB MM 22-00.00. Discrepancy: 8.92 Found the Left AFT elevator trim cable (1159O20080.27) to be kinked when tension was released from it. Resolution: Visually Inspected cable and found to have a slight bend with no sharp bend (no kinks). Inspected cable with a lox magnifier and found no damage to any strands at the bend area. No other defects noted. All work performed IAW GDR MM 27.00.00. No further action required pertaining to this item. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.80 @ $115.00 $207.00 Pans USD: Time and Material $63.74 Total USD: $270.74 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.9291 1159C20080-27 CABLE ASSEMBLY (SWAGED) 1 $63.74 $63.74 Discrepancy: 8.93 Right "C " Flap track lower inbd and outbd failed measure check after corrosion removal (Ref. to item 8.8) Resolution: Reworked and refinished right "C" flap track IAW Gulftream drawing SE05811901. Flap track is acceptable for continued normal operation per eng. despo CS278586. No further action required on this item. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.00 @ $115.00 $115.00 Total USD: $115.00 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 39 of 98 Printed: 3/23/2012 4:28:32P) Flee X EFTA01080531 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Discrepancy: 8.94 Left aileron hinge #2 inner and outer slip bushings were frozen and need to be replaced. Resolution: Installed two new slip bushings P/N GAB10G6.0500 on inner and outer left aileron hinge. Parts supplied with 72 mnt kit. All work done IAW GlIB AMM 27-10-00. Billing Method Labor USD: Flat Rate Hours Rate Total $460.00 Total USD: $460.00 Discrepancy: 8.95 Right aileron hinge #1 hole 1.1 is to small. Go gauge and bolt will not fit. Needs to be replaced. Resolution: Found small burr in hole, deburred as required. Assyembled with new hardware from 72 Mnt kit. All work done IAW GLIB AMM 20-00-00 and 27.00.00. Billing Method Flours Rate Total Labor USD: Time and Material OT 0.27 @ $173.00 546.71 Total USD: $46.71 Discrepancy: 8.96 Left outbd horizontal to elevator gap seal retainer, all screws are corroded. Resolution: Replaced all left elevator outboard gap seal screws on horizontal rear beam P/n MS27039.1.09 al work in accordance with GlIB amm chapter 27.01.00 Billing Method Hours Rate Total Labor USD: Time and Material ST 2.50 @ $115.00 $287.50 Pans USD: Time and Material $4.16 Total USD: $291.66 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.96 #1 MS27039-1-09 SCREW, MACHINE PAN HEAD 16 $0.26 $4.16 STRUCTURAL Discrepancy: 8.97 Left center horizontal to elevator gap seal retainer is corroded and all screws are corroded. Resolution: Replaced all left elevator center gap seal screws on horizontal rear beam Pin MS27039-1-09 al work in accordance with (:IIB amm chapter 27.01.00 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 40 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080532 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Labor USD: Time and Material ST 2.00 @ $115.00 $230.00 Parts USD: Time and Material $4.16 Total USD: $234.16 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.97 #1 MS27039-1-09 SCREW, MACHINE PAN HEAD 16 50.26 STRUCTURAL $4.16 Discrepancy: 8.98 Left elevator hinge fitting bearing A-10 is grooved and needs to be replaced. Resolution: Removed grooved Left elevator hinge fitting bearing A-10 P/N M528913-10C and installed new Left elevator hinge fitting bearing A-10 P/N M528913.10C IAW GAC drawing # GAB14E. Checks good. Billing Method Flours Rate Total Labor USD: Flat Rate $230.00 Parts USD: Time and Material $504.91 Total USD: $734.91 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.98 #1 MS28913-10C BEARING 1 $504.91 $504.91 Discrepancy: 8.99 Right elevator hinge fitting bearing A-10 is grooved and needs to be replaced. Resolution: Removed grooved Right elevator hinge fitting bearing A-10 P/N M528913-10C and installed new Right elevator hinge fitting bearing A-10 P/N M528913-10C LAW GAC drawing # GAB14E. Checks good. Billing Method Hours Rate Total Labor USD: Flat Rate $230.00 Parts USD: Time and Material $504.91 Total USD: $734.91 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.99 #1 MS28913-10C BEARING 1 $504.91 $504.91 Discrepancy: 8.100 Left inbd horizontal to elevator gap seal retainer is corroded and screws are corroded. Resolution: Replaced all left elevator inboard gap seal screws on horizontal rear beam P/n MS27039.1.09 al work in accordance with GlIB amm chapter 27.01.00 Billing Method Houri. 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_WorkOrderPrelintinaryInvoice.rpt Page 41 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080533 Bill To: HYPERION AIR, INC. WON: SC10420 Invoice Number: 7112000954 Labor USD: Parts USD: Flat Rate $230.00 Time and Material $4.42 Total USD: $234.42 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.100 81 MS27039-1-09 SCREW, MACHINE PAN HEAD STRUCTURAL 17 $0.26 $4.42 Discrepancy: 8.101 Right outbd horizontal to elevator gap seal, all screws are corroded. Resolution: Replaced all right elevator outboard gap seal screws on horizontal rear beam P/n MS27039.I.09 al work in accordance with GlIB amm chapter 27-01-00 Labor USD: Parts USD: Total USD: Parts: Ref. No. Billing Method Hours Rate Total Flat Rale Time and Material Pail number: $230.00 $4.16 $234.16 Description Quantity Sell price USD Extended USD 8.101 81 MS27039.1.09 SCREW, MACHINE PAN HEAD STRUCTURAL 16 $0.26 $4.16 Discrepancy: 8.102 Right center horizontal to elevator gap seal, all screws are corroded. Resolution: Replaced all right elevator center gap seal screws on horizontal rear beam P/n MS27039.1.09 al work in accordance with GlIB amm chapter 27.01.00 Billing Method Labor USD: Flat Rate Flours Rate Total $230.00 Total USD: $230.00 Discrepancy: 8.103 Right inbd horizontal to elevator gap seal, all screws are corroded. Resolution: Replaced all right elevator inboard gap seal screws on horizontal rear beam P/n MS27039-1-09 al work in accordance with GLIB amm chapter 27.01.00 Labor USD: Parts USD: Billing Method Houri. Rate Total Flat Rate $230.00 Time and Material $4.42 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 42 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080534 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Total USD: $234.42 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD SCREW, MACHINE PAN HEAD 17 $0.26 $4.42 STRUCTURAL 8.103 #1 MS27039.1.09 Discrepancy: 8.104 Right elevator hinge fitting hole A-9 inner and outer hat bushings are No-Go and need to be replaced. Resolution: Removed bad hat bushings, cleaned and installed New hat bushings P/N 1159CSM20095-5 at the A9 location IAW GAC Drawing # 5E05000901-T and GHB MM 27-10-00. Ref contingency sheet. Billing Method Hours Rate Total Labor USD: Flat Rate $690.00 Parts USD: Time and Material $370.80 Total USD: $1,060.80 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.104 #1 1159CSM20093-5 BUSHING I $185.40 $185.40 8.104#2 1159CSM2009S-5 BUSHING I $185.40 $185.40 Discrepancy: 8.105 Right elevator hinge fitting bushing A-7 is corroded. New part in install kit. Resolution: Replaced the right elevator hinge fitting bushing A-7 (corroded bushing) with a new bushing p/n 1159CSM20094-25. All work was done IAW G-IIB m/m 27.01.00. (Installation to accomplished under item # 12.122 CMP 272315. Ref contingency sheet. Billing Method Houri. Rate Total Labor USD: Flat Rate $690.00 Parts USD: Time and Material $54.59 Total USD: $744.59 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.105 #1 1159CSM20094-25 SLEEVE I $54.59 $54.59 Discrepancy: 8.106 LH IB Flight Spoiler Bell Crank Rod End has siezed bearing. Resolution: Removed the Ia/H inboard flight spoiler bellcrank pushrod P/N 1159C20262-3 and installed a "New" pushrod P/N 1159C20262-3 with rod end bearings inclusive. Refer to item 12.150 for Removal and installation of push rod. Billing Method Houri. 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 43 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080535 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Labor USD: Pans USD: Flat Rate $115.00 Time and Material $529.40 Total USD: $644.40 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.106 #1 1159C20262-3 PUSH ROD I S529.40 $529.40 Discrepancy: 8.107 LH OB Flight Spoiler Bell Crank Rod End has seized bearing. Resolution: Replaced the L/11 outboard flight spoiler bellcrank pushrod with "New" rod P/N 1159C20262-3. Refer to item 12.149 for Removal and installation of push rod. Billing Method Hours Rate Total Labor USD: Flat Rate $115.00 Paris USD: Time and Material $529.40 Total USD: $644.40 Parts: Ref. No. Part number: Description ()nitwit> Sell price USD Extended USD 8.107 #1 1159C20262-3 PUSH ROD I S529.40 $529.40 Discrepancy: 8.108 RH IB Flight Spoiler Bell Crank Rod End has siezed bearing. Resolution: Replaced the R/H inboard flight spoiler bellcrank pushrod with "New" rod P/N 1159C20262-3. Refer to item 12.152 for Removal and installation of push rod. Billing Method Flours Rate Total Labor USD: Flat Rate $115.00 Paris USD: Time and Material $529.40 Total USD: $644.40 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.108 #1 1159C20262-3 PUSH ROD 1 $529.40 $529.40 Discrepancy: 8.109 R/H elevator trim tab hinge #2 lower hat bushings are corroded. Resolution: Removed corroded R/H elevator trim tab hinge #2 lower hat bushings (2 each) P/N's 1159CSM20155-1 and replaced with new hat bushings (2 each) P/N's 1159CSM20155-1 IAW GAC Drawing # SE05000901-T. Checks good. Billing Method Hours 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_WorkOrderPrelintinaryInvoicespt Page 44 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080536 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Parts USD: Time and Material $86.52 Total USD: $546.52 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.10981 1159CSM2015S-1 BUSHING 2 $43.26 $86.52 Discrepancy: 8.110 LJH LB flight spoiler is missing bushing 4-3. P/N 11595B30210.49. Part included in "install kit". Resolution: Removed old hardware, cleaned attach point holes and greased all New hardware and slip bushings. Installed a New bushing P/N 11595B30210-49 provided in the 72month install kit. Work performed IAW GIIB MM 27-02-00. Ref contingency sheet. Pans USD: No Charge N/ C Discrepancy: 8.111 R/H O/B flight spoiler O/B bearing is halfway out of spoiler attach point. Resolution: Reinstalled R/H O/B flight spoiler O/B hearing back into place and secured as required IAW GLIB AMM 20-00-00. Checks good. Billing Method Hours Rate Total Labor USD: Time and Material ST 0.85 @ $115.00 597.75 Total USD: $97.75 Discrepancy: 8.112 Right middle flap drive has grooves in it and requires changing. Resolution: Duplicate item See item 8.117 for details. Discrepancy: 8.113 Left O/B flight spoilers have rust on steel plate on top surfaces. Resolution: REMOVED , light corrosin ,and rust on top surfaceO/B flihgt spoiler , treated and primed top coat as required I AW GIV gamps 4000. 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_WorkOrderPrelintinaryInvoicespt Page 45 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080537 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Labor USD: Time and Material ST 735 @ $115.00 $845.25 Labor USD: Time and Material OT 1.50 @ $173.00 $259.50 Total USD: $1.104.75 Step: 8.113.1 Completed RIB elevator , outbd top skin , has spot of corrosion, removed light corrosion and sanded as required.Area ready for primer. All work IAW Gamps 4000. Discrepancy: 8.114 Right O/B flight spoilers have rust on steel plate on top surfaces. Resolution: REMOVED light corrosion on spoiler top surface, treated and primed as required IAW GIV CAMPS 4000 Billing Method Flours Rate Total Labor USD: Time and Material ST 6.25 @ $115.00 $718.75 Labor USD: Time and Material OT 1.44 @ $173.00 $249.12 Total USD: $967.87 Discrepancy: 8.115 L/H ground spoiler has chiping paint and corrosion in numerious locations. Resolution: Sanded 14/H ground spoiler [bottom surface around hinges and top inboard edge.] where paint was chipping and removed light corrosion, treated, primed, painted ,clear coat as required All work performed JAW CAC. CAMPS 4000. Billing Method Hours Rate Total Labor USD: Time and Material ST 533 @ $115.00 $612.95 Labor USD: Time and Material OT 0.50 @ $173.00 $86.50 Total USD: $699.45 Step: 8.115.1 Completed REMOVED light corrosion and paint chiping in numerious areas on 1./Il ground spoiler IAW GOB 51.10-00. Discrepancy: 8.116 L/H flight spoiler actuator rear bearing is seized. Resolution: Complied with by replacing the bad LH flight spoiler actuator and installing a Modified LH flight spoiler actuator P/N 1159SCH250-29, S/N 2002. Work performed IAW CHB MM 27.02.00. REF Item 12.148 Billing Method Hours Rate Total Labor USD: Pans USD: No Charge Time and Material N/C $19,912.00 Total USD: $19,912.00 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_WorkOrderPrelintinaryInvoicesm Page 46 of 98 Printed: 3/23/2012 4:28:32PD Ftst X EFTA01080538 Bill To: HYPERION AIR, INC. WO*: SC10420 Invoice Number: 7112000954 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.116 NI 1159SCH250-29 ACTUATOR, HYDRAULIC FLIGHT 1 $19,912.00 $19,912.00 SPOILER (LAO Discrepancy: 8.117 R/H wing, second from outbd flap drive rod is scored. Resolution: Removed R/H wing outbd flap drive shaft P/N 1159SCC213-15 , S/N unreadable. Installed new flap shaft P/N 1159SCC213-15 , S/N 2591 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 $4,984.00 Total USD: $5,214.00 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.117 NI 1159SCC2I3-15 SHAFT 1 $4,984.00 $4,984.00 Discrepancy: 8.118 R/H 0/B flight spoiler O/B hat bushings bushing 6.2 on wing attach fitting failed no go gauge (Ref 12.23) . Resolution: Removed bad bushings. Prepped and installed new bushings P/N 11595B30210-29 lAW Gulfstream Drawing SE05000901 rev.T. Billing Method Hours Raw Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $64.48 Total USD: $524.48 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.118 NI 11595B30210-29 BUSHING 2 $32.24 $64.48 Discrepancy: 8.119 R/H ground spoiler has paint missing and light corrosion in numerious locations Resolution: Sanded and primed R/I4 ground spoiler that had paint missing, removed light corrosion ,treated and primed and painted as required JAW GAC Gamps 4000. Billing Method Hours Rate Total Labor USD: Time and Material ST 4.75 @ $115.00 $546.25 Total USD: $546.25 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_WorkOrderPrelintinaryInvoicespt Page 47 of 98 Printed: 3/23/2012 4:28:32PD Rd X EFTA01080539 Bill To: HYPERION AIR, INC. WO It: 5C10420 Invoice Number: 7112000954 Discrepancy: 8.120 One oxygen bottle requires new packing at attach nut. Resolution: Removed and replaced "o" ring on oxygen bottle attach nut. Take note that new "o" ring is made of teflon and difficult to MS22012-6 new "o" ring was installed IAW G-II B AMM 35.00.00. Checks good. Billing Method Hours Rate Total Labor USD: Time and Material ST 0.25 @ $115.00 $28.75 Pans USD: Time and Material $52.20 Total USD: $80.95 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.120 #1 MS22012-6 PACKING RING 6 $8.70 $5210 Discrepancy: 8.121 IJH aileron inboard hinge has bad bearing.Bearing is falling apart. Resolution: Bearing was already removed for NDT.See item 12.11 for details. Removed old bearing PN. MS28913-6C and installed new bearing P/N M528913-6C in L/H aileron inboard hinge as required IAW GAC drawing # GAB14E. Billing Method Hours Rate Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $321.32 Total USD: $551.32 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.121 #2 MS20427M5-11 MONEL RIVET 20 $1.93 $38.60 8.121 #3 MS20427h15-18 RIVET, MONEL 100 DEGREE 25 $2.15 $53.75 COUNTERSUNK 8.121 #4 MS28913-6C BEARING 1 $228.97 $228.97 Discrepancy: 8.122 During NDT Inspections Multiple Spots Of Corrosion Were Found In L/H Center Chanel Skegg and FWD R/H Breastplate Inboard Hi-Lok Fastners. Resolution: Removed Hi-Lok Fastners From IJH Center Chanel Skegg and FWD R/H Breastplate Inboard, Cleaned And Removed Surface Corrosion. Installed Hi-Lok Fastners Wet With PRC 1422 B2. All Maintenence Performed In Reference To GLIB AMM 57.00.00. Billing Method Hours Rate Total Labor USD: Time and Material ST 12.76 @ $115.00 $1,467.40 Pans USD: Time and Material $17.72 Total USD: $1,485.12 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 48 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080540 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.122 #1 HLI9PB8-12 HILOK 1 58.24 $8.24 8.122 #2 GAB51084-10 BOLT 3 53.16 $9.48 Discrepancy: 8.123 Flaps require rigging, due to actuator removal. Resolution: Complied with flap rigging. Work done I/A/W GLIB MM chapter 27-06-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.00 @ $115.00 $230.00 Total USD: $230.00 Step: 8.123.1 Step: 8.123.2 Completed Installed both flaps and soft rigged. No hyd. or power was avaiable and flaps require final rigging. Completed Complied with flap rigging. Work done I/A/W GIIB MM chapter 27.06.00. Discrepancy: 8.124 NDT of all hardware over 3/8" 2 each P/Ns. NAS6610D56 1159CM20223-1 1159CM20264-1 Resolution: Complied with NDTof 2 each PN. NAS6610D56, 2 each PN. 1159CM20223-1 ,and 2 each PN. 1159CM20264-1 bolts as required. NDT Performed by E&I under PO12-00574 / Work Order EIA12-6039. No defects noted.. Discrepancy: 8.125 Rill flight spoiler attach hardware missing. Resolution: Installed new hardware P/Ns 1159CM20265-1, AN4C11, NAS1149C0463R and MS17826.4. All work done IAW Gulfstream AMM 27-00-00. Parts USD: Parts: No Charge N/ C Ref. No. Part number: Description Quantit 8.125 #1 1159CM20265-1 DOWEL I 8.125 #2 AN4C 1 1 BOLT MACHINE-CRES,DRILLED I SHK 8.125 #3 NASI149C0463R WASHER-FLAT CRES I 8.125 N4 MSI7826-4 NUT I Discrepancy: 8.126 Corrosion found on surface of left and right wing wedges . 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 49 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080541 Bill To: HYPERION AIR, INC. WO*: SC10420 Invoice Number: 7112000954 Resolution: Removed surface corrosion on both left and right side surface of wing wedge areas JAW G-IIB SRM 51.13.10. Treated and primed areas JAW G-IIB SRM 51-07-10. Checks good. Billing Method Flours Rate Total Labor USD: Time and Material ST 3.50 @ $115.00 $402.50 Total USD: $402.50 Discrepancy: 8.127 Left aileron outboard attach point bushings need reamed prior to bolt installation. Resolution: After further investigation found that reaming is not required. Cleaned and lubricated the attach fitting hole and bolt. Installed New bolt P/N NAS6605D50 as required. Work performed IAW GIIB MM 27-02-00. Ref contingency sheet. Discrepancy: 8.128 Left elev. trim tab cracked on inbd trailing edge . Resolution: Removed cracked left elevator trim tab P/N 1159CSH20500-1 S/N 147, with 10,804.3 TSN, 5,663 CSN. Installed "serviceable" as removed from G-II S/N 055 trim tab P/N 1159CSH2O500.1 S/N 57, with 18,947.2 TSN 7,651 CSN. All work performed IAW GIIB AMM 27-04-00. Ref squawk 12.124 for CMP 272510. Parts USD: No Charge Parts: Ref. No. Part number: Description Quantity TAB ASSY, TRIM, ELEVATOR DISCHARGER, STATIC WICK 8.128 #1 1159CSH20500-1 8.128 #2 2-165C-1 Step: 8.128.1 Completed 1 N/C Inspected LH Elevator trim tab hinge fittings on trim tab P/N I159CSH20500.1 S/N T57 IAW (MB AMM 27-04-00. Found bushings 3-1 and 3-2 to be out of tolerance. Removed bad bushings P/N I1S9C'SM20155.1 and P/N1159(SNI20155-5 and installed new hat bushings P/N 1159CSM20155-1 and P/N I159CSM20155.5 removed from damaged LH elevator trim tab PiN 1159CSH2O500.1 SIN 147 hinge fittings 3.1 and 3-2. All work was performed IAW GAC drawing # SE05000901-T. Discrepancy: 8.129 Perform Ops check of all flight controls as required. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 3.50 @ $115.00 $402.50 Total USD: $402.50 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_WorkOrderPrelintinaryInvoicespt Page 50 of 98 Printed: 3/23/2012 4:28:32P) Ftst X EFTA01080542 Bill To: HYPERION AIR, INC. WO It: 5C10420 Invoice Number: 7112000954 Discrepancy: 8.130 The RH elevator trim tab actuator's outboard bellows is torn Resolution: Removed tom boot from the Right Elevator trim tab actuator P/N: 1201-10. Installed a new actuator boot P/N: 1201.10. Work was done IAW GIIB AMM Ch.27-04-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 5.00 @ $115.00 $575.00 Pans USD: Time and Material $796.60 Total USD: $1,371.60 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.130 NI 1201-10 BELLOW 1 $796.60 $796.60 Discrepancy: 8.131 Free air temp gauge pegs out all the time (located on center overhead panel) Resolution: Removed OAT sensor P/N-MS28038-1 S/N-12329, from Fwd RH nose area . Installed NEW OAT sensor P/N-M528038-1 S/N-00138. Performed ops check IAW GIIB AMM 34-02-00. No defects noted. Updated CMP 342515. Billing Method Hours Rate Total Labor USD: Time and Material ST 9.00 @ $115.00 $1,035.00 Pans USD: Time and Material $1,115.60 Total USD: $2,438.10 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.131 #3 102-00035-1 OAT TEMP BULB 1 $1,115.60 $1,115.60 Step: 8.131.1 Completed Verified discrepancy removed OAT sensor connector , reading remains the same. Telling us the sensor is in a open-defective state. Removed OAT sensor from Fwd RHS nose area P/N-M528038-1 S/N-I2329 and checked on bench I.A.W. G IIB M.M. 34-02-00 Performed OAT system - Inspection Check / Bulb resistance vs Temperature Chart , and temp bulb fails. Placed OAT Temp bulb P/N-MS28038-I S/N-I2329 on order and reinstalled OAT Temp Bulb back in mit and strermered part in acil, awaiting pans delivery ETA early Am. All work performed I.A.W. GIIB M.M. 34-02-00. Discrepancy: 8.132 APU door motor intermittent. Resolution: Removed APU door actuator P/N GYLC9482-1 S/N 33 and installed overhauled APU door actuator P/N GYLC9482-2 S/N 592 IAW GIIB AMM 49-00-00. Ops check good. See steps for details. Labor USD: No Charge Parts USD: No Charge Pans: Ref. No. Pan number: Description Quantity 8.13281 GYLC'9482-2 ACTUATOR N/C 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_WorkOrderPrelintinaryInvoice.rpt Page 51 of 98 Printed: 3/23/2012 4:28:32PD our X EFTA01080543 Bill To: HYPERION AIR, INC. WO*: SC10420 Invoice Number: 7112000954 Step: 8.132.1 Step: 8.132.2 Step: 8.132.3 Completed Inspected APU door motor, wiring and linkage NO DEFECT'S NOTED. Operated APU door several times with no faults noted. Could not duplicate. Ops check good. AM work done 'ASV GLIB MM 49-10-00 Completed Removed APU door actuator P/N GYLC9482-1 S/N 33 and installed overhauled APU door actuator P/N GYLC9482-2 S/N 592 IAW 6IM AMM 49.00.00. Actuator stops need safetied. Completed Safetied actuator stops on APU door actuator. Performed Ops check on APU door actuator lAW GIM AMM 49.00.00. Ops check good. Discrepancy: 8.133 1../II elevator trim tab actuator outboard boot is torn in several places. Resolution: Billing Method Houri. Rate Total Labor USD: Time and Material ST 030 @ $115.00 $57.50 Total USD: $57.50 Step: 8.133.1 Completed Removed left elevator trim tab actuator mounts for access to change the bellows. Removed outboard bellow, new bellow arriving at noon on 3/22/2011. Ref C llu MM 27-04-00. Discrepancy: 8.134 Left main gear side brace actuator up line saturated and leaking. Resolution: Billing Method Flours Rate Total Pans USD: Time and Material $398.77 Total USD: $398.77 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.134 #1 1159H20200-83 HOSE ASSEMBLY 1 $398.77 $398.77 Item: 9 Paint Team Manager: Sean Brown Customer Coordinator: Ray Kraber Pan/Model #: AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 9.1 Resolution: Labor USD: Pans USD: Paint as required, bare metal and after inspection. Billing Method Hours Rate Total Flat Rate No Charge $2,500.00 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 52 of 98 Printed: 3/23/2012 4:28:32P) Ftst X EFTA01080544 Bill To: HYPERION AIR, INC. Total USD: Parts: Ref. No. 9.1 #1 Part number: Description HURON 5000 PHONTON GREY EFFECT ACTIVATOR WO It: SC10420 Invoice Number: 7112000954 9.1 #2 Step: 9.1.1 P1251 HN 1935 $2,500.00 Quantity 1 Waiting SAND AREAS treated and primed as required gamps 4000 Insp I Item: 10 Outstanding Parts, Materials, and / or Services Team Manager: Sean Brown Customer Coordinator: Ray Kraber Part/Model #: AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 10.1 72 month kit - order in advance. Resolution: Complied with Discrepancy: 10.2 Outstanding services waiting. Resolution: Billing Method Services USD: Time and Material Total USD: Services: Hours Rate Total $5,792.58 $5,792.58 Ref. No. Description Quantity Sell Price USD Extended USD 10.2 #4 Vendor Supplied Labor 1.00 $2,226.72 $2,226.72 Part Ref: 1159CM20209-6 CRANK ASSEMBLY 10.2 #1 SERVICE 1.00 $3,215.86 $3,215.86 10.2 #2 SERVICE 1.00 $0.00 $9.90 10.2 #3 SERVICE 1.00 $350.00 $359.90 Discrepancy: 10.3 Resolution: Service for man extra manpower. Services USD: No Charge Services: Ref. No. Description 103 #1 SERVICE Quantity 1.00 N/ C 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 53 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080545 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 10.4 Parts pulled not turned green,(check with weekend crew) Resolution: Billing Method Hours Rate Total Pans USD: Total USD: Parts: Ref. No. Time and Material Part number: Description $609.39 Extended USD Quantity $609.39 Sell price USD 10.4 #5 2-165C-1 DISCHARGER, STATIC WICK 1 $75.80 $75.80 10.4 #3 1159CM20228-17 BUSHING 1 $263.21 $263.21 10.4 #2 1159CM20228-17 BUSHING 1 $263.21 $263.21 10.4 #1 MS29513-214 PACKING PREFORMED-O RING 1 $0.41 $0.41 10.4 #4 MS27039-1-09 SCREW, MACHINE PAN HEAD 16 $0.26 $4.16 STRUCTURAL 10.4 #7 MS25083-1BB4 JUMPER, ELEC BONDING - 4 INCH 1 $2.60 $2.60 Discrepancy: 10.5 Resolution: Cushatter appun ed m ertime. Billing Method Labor USD: Flat Rate Total USD: Hours Rate Total $12,900.13 $12,900.13 Item: 12 Customer Supplied CMP Due List Team Manager: Sean Brown Customer Coordinator: Ray Kraber Pan/Model #: AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 12.1 Comply with Customer Supplied CMP Due List. Labor - Primary Codes $53,550.00 Labor - Mandatory Related Codes $32,110.00 Total Labor $85,660.00 Resolution: Complied with Customer Supplied CMP Due List. For detail description of the work complied with see the Work Order Detail report. GAC_WorkOrderPrelintinaryInvoicesrot Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). Page 54 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080546 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Billing Method Hours Rate Total Labor USD: Paris USD: Total USD: Parts: Ref. No. Flat Rate Time and Material Part number: Description $85,660.00 $14,503.49 Extended USD 5100.163.49 Quantity Sell price USD 12.1 #1 G3 72MONTH KIT 2 361,385,387,388,390 & SUB / 0386.0499 1 $9,893.53 $9,893.53 12.1 #3 1159CSM20091-3 SLEEVE 1 $96.72 $96.72 12.1 #4 PR I422-B-2 SEALANT, PRC, CARTRIDGE 4 $38.47 $153.88 12.1 #5 HLI9PB8-8 BOLT 30 $5.15 $154.50 12.1 #6 HL70-8 COLLAR 50 $0.90 $45.00 12.1 #7 NASI303-29D BOLT 2 $4.35 $8.70 12.1 #9 GABIOG5.00500 BUSHING 3 $74.74 $224.22 12.1 #10 1159CSM20094-17 SLEEVE 2 $282.13 $564.26 12.1 #1I MSI7825-3 NUT, STEEL CASTELLATED 2 $2.08 $4.16 SELF-LOCKING 12.1 #12 NASI305-29H BOLT I $6.08 $6.08 12.1 #13 NASI149F0532P WASHER-FLAT STEEL I $0.26 $0.26 12.1 #14 MS2I042L5 NUT, SELF-LOCKING RING BASE I $1.24 $1.24 12.1 #15 NAS6604D3I BOLT HEX HD-CL TOL,DRILLED 4 $1.87 $7.48 SHK 12.1 #16 1159CSM20118-19 PAD ASSY,ELEV HINGE-FLT CONT 1 $170.28 $170.28 12.1 #17 MS21151-8C ROD END WITH KEY-WAY I 576.22 $76.22 12.1 #18 GAN512H4 NUT-COLLAR,SHEAR SELF 50 $0.84 $42.00 LOCKING 12.1 #19 PR 1440-B-2 SEALANT, PRC, CARTRIDGE 2 $46.48 $92.96 12.1 #20 AN525-10R26 SCREW 1 $2.58 $2.58 12.1 #21 NASI149D1690H WASHER-FLAT ALUM 1 $0.74 $0.74 12.1 #22 NAS6603D29 BOLT 2 $11.60 $23.20 12.1 #23 NASI305-29H BOLT 1 $6.08 $6.08 12.1 #24 PR I422-B-2 SEALANT, PRC, CARTRIDGE 2 538.47 $76.94 12.1 #25 PR1440-B-I/2 SEALANT, PRC,CARTRIDGE 2 538.28 $76.56 12.1 #26 NASI303-27H BOLT 2 $12.47 $24.94 12.1 #27 AV30-00372 CORROSION PREVENTIVE, 13.5 1 $69.53 $69.53 OUNCE AEROSOL (12/CS) 12.1 #28 LUBRI-BOND-220 LUBRICANT, 12 OUNCE AEROSOL 1 547.87 $47.87 SPRAY 12.1 #29 PR I422-B-2 SEALANT, PRC, CARTRIDGE 4 $38.47 $153.88 12.1 #30 P5870-B-2 SEALANT 2 $56.69 $113.38 12.1831 PR1440-B-2 SEALANT, PRC, CARTRIDGE 2 $46.48 $92.96 12.1 #32 PR I422-B-2 SEALANT, PRC, CARTRIDGE 2 $38.47 $76.94 12.1 #33 AN735D48 CLAMP-ELEC BONDING,3.00 IN 1 $0.96 $0.96 12.1 #34 PRI440-B-1/2 SEALANT, PRC,CARTRIDGE 1 538.28 $38.28 12.1 #35 TRIBOLUBE-2N LUBRICANT 1 $271.92 $271.92 12.1 #36 1201-10 BELLOW 1 $796.60 $796.60 12.1 #37 1201-10 BELLOW 1 $796.60 $796.60 12.1 #38 PR1440-B-2 SEALANT, PRC, CARTRIDGE 6 $26.82 $160.92 12.1 #39 NAS6605D24 BOLT, HEX HD-CLOSE TOL, DR 2 $11.53 $23.06 SHANK 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 55 of 98 Printed: 3/23/2012 4:2&32P) Rd X EFTA01080547 Bill To: HYPERION AIR, INC. WON: SC10420 Invoice Number: 7112000954 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 12.1 #40 PR1440-B-2 SEALANT, PRC, CARTRIDGE 1 S26.82 $26.82 12.1 #41 PR1422-B-112 SEALANT,PRC,CARTRIDGE 2 $40.62 $81.24 Discrepancy: 12.2 CMP GLIB 246020 C Inverter - Frequency / Voltage Check Resolution: COMPLIED WITH CMP GIIB 246020 C Inverter - Frequency / Voltage Check with no discrepancies noted at this lime. All work performed JAW G-IIB maintenance manual 24.03.00. Labor USD: No Charge N/ C Discrepancy: 12.3 CMP GIIB 247020 L Alternator Spline - Lubrication Resolution: COMPLIED WITH CMP GIIB 247020 L Alternator Spline - Lubrication JAW GIIB MM 24-02-04. No defects noted at this time. Billing Method Flours Rate Total Parts USD: Time and Material $32.38 Total USD: $32.38 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 123 #1 NASI593-214 0 -RING 2 $0.74 $1.48 123 #2 KB21307 SEAL 2 $15.45 $30.90 Discrepancy: 12.4 CMP GHB 247025 R Alternator Spline - Lubrication Resolution: COMPLIED WITH CMP GIIB 247025 R Alternator Spline - Lubrication IAW GlIB MM 24-02-04. No defects noted at this time. Labor USD: No Charge N/ C Discrepancy: 12.5 CMP GlIB 252020 Life Vest(s) - Inspect / Re-Certify Resolution: COMPLIED WITH CMP GIIB 252020 Life Vest(s) - Inspect / Re-Certify IAW GlIB AMM 25-00-00. See squawks 12.94 thru 12.110 for life vests status. 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 56 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080548 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Labor USD: No Charge N/ C Services USD: Time and Material $487.69 Total USD: $487.69 Services: Ref. No. Description Quantity Sell Price USD Extended USD 12.5 #1 Vendor Supplied Labor 1.00 S-187.69 $487.69 Discrepancy: 12.6 CMP 611B 257530 Lavatory Compartment (Above Floor) - Inspection (AD 74-08.09) Resolution: COMPLIED WITH CMP GIIB 257530 Lavatory Compartment (Above Floor) - Inspection (AD 74.08.09). All work done per AD74-08-09-R2. No defects noted. Labor USD: No Charge N/ C Discrepancy: 12.7 CMP GLIB 261760 Portable Halon Fire Extinguisher (Cockpit No. 1) - Inspection Resolution: COMPLIED WITH CMP GIIB 261760 Portable Halon Fire Extinguisher (Cockpit No. 1) - Inspection.All work done per G-IIB amm ch 26.03.00. No defects noted Labor USD: No Charge N/ C Discrepancy: 12.8 CMP GIIB 261761 Portable Halon Fire Extinguisher (Forward Cabin) - Inspection Resolution: COMPLIED WITH CMP GIIB 261761 Portable Halon Fire Extinguisher (Forward Cabin) - Inspection. All work done per G-IIB amm ch 26-03.00. No defects noted Labor USD: No Charge N/ C Discrepancy: 12.9 CMP GIIB 261763 Portable Halon Fire Extinguisher (Baggage Compartment) - Inspection Resolution: COMPLIED WITH CMP GIIB 261763 Portable Halon Fire Extinguisher (Baggage Compartment) - Inspection. All work done per G-IIB amm ch 26.03-00. No defects noted. 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_WorkOrderPrelitninaryInvoice.rpt Page 57 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080549 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 12.10 CMP GLIB 270145 Takeoff Alarm System - Operational Test Resolution: COMPLIED WITH CMP GIIB 270145 Takeoff Alarm System - Operational Test. No defects noted. All work done IAW GIIB MM Chapt 27-02-00. Labor USD: No Charge N/ C Discrepancy: 12.11 CMP GIIB 270210 Aileron / Hinge Fitting (Left) - Inspection Resolution: COMPLIED WITH CMP GIIB 270210 Aileron/ Hinge Fitting (Left) - Inspection as required IAW GIIB AMM 27-02-00.Refer to squawks ,8.71,8.72 8.94, for discrepencies noted. NDT performed by Structual testing systems Cert # ES1R124K. No defects noted.. Labor USD: No Charge N/ C Step: 12.11.1 Step: 12.11.2 Completed Hemmed all three hinges from IJH aileron and cleaned. * Note* all hinges are in the perspective positions and clearly marked as to the inboard/out board facing side.. Completed Complied with step (3) of part B, the removal of the bearing retainers and bearings from the three hinges on the left aileron IAW G-I1 B AMM 27-02-00. Ready for NDT. Discrepancy: 12.12 CMP GIIB 270215 Aileron / Hinge Fitting (Right) - Inspection Resolution: COMPLIED WITH CMP GIIB 270215 Aileron / Hinge Fitting (Right) - Inspection as required IAW GIIB AMM 27-02-00. Refer to squawks 8.2,8.69,8.70,8.95 for discrepencies noted. NDT performed by Structual testing systems Cert. # ES1R124K. No defects noted.. Labor USD: No Charge N/ C Step: 12.12.1 Step: 12.12.2 Completed Removed all three hinges from RJR aileron and cleaned. * Note* all hinges are in the perspective positions and clearly marked as to the inboard facing side.. Completed Complied with step (3) of part B, the removal of the bearing retainers and bearings front the three hinges on the right aileron IAW B AMM 27-02-00. Ready for NDT. Discrepancy: 12.13 CMP GIIB 270220 Aileron Trim Tab Hinge Fitting - Inspection Resolution: COMPLIED WITH CMP GIIB 270220 Aileron Trim Tab Hinge Fitting - Inspection IAW GIIB 27-04-00. No defects noted. Refer to squawk 8.20 for discrepency noted while compling with this CMP. Discrepancy: 12.14 CMP GHB 270225 Elevator Hinge Fitting (Left) - Inspection Resolution: COMPLIED WITH CMP GIIB 270225 Elevator Hinge Fitting (Left) - Inspection IAW GIIB 27-01-00. Refer to squawk 8.98 for discrepancy 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_WorkOrderPreliminaryInvoicespt Page 58 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080550 Bill To: HYPERION AIR, INC. WO*: SC10420 Invoice Number: 7112000954 Labor USD: No Charge N/ C Step: 12.14.1 Completed Complied with C111P (MB 270225 Elevator Hinge Fitting (Left) - Inspection stepB(3) thru B(6) IAW GIIB AMM 27-01-00. Discrepancy: 12.15 CMP GIIB 270230 Elevator Hinge Fitting (Right) - Inspection Resolution: COMPLIED WITH CMP GIIB 270230 Elevator Hinge Fitting (Right) - Inspection LAW GIIB 27.01.00. No defects noted. Labor USD: No Charge N/ C Step: 12.15.1 Completed Complied with CMP GIIB 270230 Elevator Hinge Fitting (RT - Inspection step10.3) thru B(6) IAW (NIB AMM 27-01.00. Discrepancy: 12.16 CMP GIIB 270235 Elevator Trim Tab / Hinge Fittings (Left) - Inspection Resolution: COMPLIED WITH CMP GIIB 270235 Elevator Trim Tab / Hinge Fittings (Left) - Inspection. Discrepancies entered under item 8. All work done per G-IIB maint manual 27.04.00. Discrepancy: 12.17 CMP GIIB 270240 Elevator Trim Tab / Hinge Fittings (Right) - Inspection Resolution: COMPLIED WITH CMP GIIB 270240 Elevator Trim Tab / Hinge Fittings (Right) - Inspection. Discrepancies entered under item 8. All work done per G-IIB maint manual 27.04.00. Discrepancy: 12.18 CMP GIIB 270245 Rudder/ Hinge • Inspection Resolution: COMPLIED WITH CMP GIIB 270245 Rudder / Hinge - Inspection [ANY (MB AMM 27-20.00. No defects noted. Labor USD: Pans USD: Step: 12.18.1 Step: 12.18.2 No Charge No Charge N/ C N/ C Completed Gained access to hinge points, removed rudder hinge fittings from rudder. Performed dimensional checks of rudder and hinge fittings. Performed IAW (NIB 27.03.00. Completed Installed lower rudder hinge fitting P/N 1159(SM20025.5 as required and safetied 1AM. (MB AMM 27-03-00. Discrepancy: 12.19 CMP (MB 270247 Rudder Torque Tube - Inspection Resolution: COMPLIED WITH CMP GIIB 270247 Rudder Torque Tube - Inspection. All Maintenence Performed In Reference To GIIB AMM 27-03-00. 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 59 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080551 Bill To: HYPERION AIR, INC. WO*: SC10420 Invoice Number: 7112000954 Labor USD: No Charge N/ C Step: 12.19.1 Completed Complied with CM? 611B 270247 Rudder Torque Tube - Inspection, step A. through B. (10). All maintenance performed IAN,' GLIB MM 27-03-00. Discrepancy: 12.20 CMP GLIB 270250 Inboard Flight Spoiler Hinge (Left) - Inspection Resolution: COMPLIED WITH CMP GIIB 270250 Inboard Flight Spoiler Hinge (Left) - Inspection. Used go no go gauges IAW GIIB AMM 27-02-00. Ref squawk 8.110 for discrepencies. Labor USD: No Charge N/ C Discrepancy: 12.21 CMP GIIB 270255 Outboard Flight Spoiler Hinge (Left) - Inspection Resolution: COMPLIED WITH CMP GIIB 270255 Outboard Flight Spoiler Hinge (Left) - Inspection. Used go no go gauges. No defects found IAW GLIB AMM 27.02-00. Discrepancy: 12.22 CMP GIIB 270260 Inboard Flight Spoiler Hinge (Right) - Inspection Resolution: COMPLIED WITH CMP GIIB 270260 Inboard Flight Spoiler Hinge (Right) - Inspection.Used go nogo gauges. No defects found IAW GLIB AMM 27-02-00. Labor USD: No Charge N/ C Discrepancy: 12.23 CMP GIIB 270265 Outboard Flight Spoiler Hinge (Right) - Inspection Resolution: COMPLIED WITH CMP GIIB 270265 Outboard Flight Spoiler Hinge (Right) - Inspection. Use go no go gauges. I 1« GIIB AMM 27-02-00. Ref squawk 8.111 for discrepencies. Discrepancy: 12.24 CMP GIIB 270271 Left Ground Spoiler Hinge - Inspection (Aircraft Having 6 Panel Speed Brakes) Resolution: COMPLIED WITH CMP GIIB 270271 Left Ground Spoiler Hinge - Inspection (Aircraft Having 6 Panel Speed Brakes) Used go no go gauges. No defects found IAW GIIB AMM 27-02-01. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WoikOrderPreliminarylnvoice.rpt Page 60 of 98 Printed: 3/23/2012 4:28:32P) Ftst X EFTA01080552 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 12.25 CMP GLIB 270276 Right Ground Spoiler Hinge - Inspection (Aircraft Having 6 Panel Speed Brakes) Resolution: COMPLIED WITH CMP GIIB 270276 Right Ground Spoiler Hinge - Inspection (Aircraft Having 6 Panel Speed Brakes) Used go no go gauges. No defects found IAW GIIB AMM 27-02-01. Labor USD: No Charge N/ C Discrepancy: 12.26 CMP GIIB 270610 Rudder Pedal Controls - Lubrication Resolution: COMPLIED WITH CMP GIIB 270610 Rudder Pedal Controls - Lubrication IAW GIIB MM 27-03-00. No defects noted at this time. Labor USD: No Charge N/ C Discrepancy: 12.27 CMP GIIB 270618 Flap Actuator Bushing (Left Inboard) - Lubrication Resolution: COMPLIED WITH CMP GIIB 270618 Flap Actuator Bushing (Left Inboard) - Lubrication. Lubrication. Work IAW GIIB MM 27-06-00 Labor USD: No Charge N/ C Discrepancy: 12.28 CMP GIIB 270619 Flap Actuator Bushing (Left Outboard) - Lubrication Resolution: COMPLIED WITH CMP GIIB 270619 Flap Actuator Bushing (Left Outboard) - Lubrication. Work IAW GIIB mm 27-06-00 Labor USD: No Charge N/ C Discrepancy: 12.29 CMP GIIB 270622 Flap Actuator Bushing (Right Inboard) - Lubrication Resolution: COMPLIED WITH CMP GIIB 270622 Flap Actuator Bushing (Right Inboard) - Lubrication IAW GIB MM 27-06-00. No defects noted at this time. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 61 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080553 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Step: 12.29.1 Step: 12.29.2 Completed Complied with CMP GIIB 270622 Flap Actuator Bushing (Right Inboard) - Lubrication, step A.through B.(2). All maintenance performed JAW GIIB MM 27.06.00. Completed Complied with CUP (MB 270622 Flap Actuator Bushing (Right Inboard) - UAW GIIB MM 27-06-00. No defects noted at this time. Discrepancy: 12.30 CMP GIIB 270623 Flap Actuator Bushing (Right Outboard) - Lubrication Resolution: COMPLIED WITH CMP GIIB 270623 Flap Actuator Bushing (Right Outboard) - Lubrication IAW GlIB MM 27.06-00. No defects noted at this time. Step: 12.30.1 Step: 12.30.2 Completed Complied with CMP GIIB 270623 Flap Actuator Bushing (Right Outboard) - Lubrication. Step A. through B.(2). All maintenance performed IAW GIIB MM 27.06.00. Completed Complied with CMP GIIB 270623 Flap Actuator Bushing (Right Outboard) - IAW GIIB MM 27-06-00. No defects noted at this time. Discrepancy: 12.31 CMP GIIB 270635 Control Surface Hinge Joints - Lubrication Resolution: COMPLIED WITH CMP GIIB 270635 Control Surface Hinge Joints - Lubrication. All Maintenence Performed In Reference To GlIB AMM 27-00-00. Discrepancy: 12.32 CMP GIIB 270720 Elevator Trim Tab Actuator (Left) - Lubrication Resolution: COMPLIED WITH CMP GIIB 270720 Elevator Trim Tab Actuator (Left) - Lubrication. All Maintenence Performed In Reference To GIIB AMM 27-04-00. Discrepancy: 12.33 CMP GIIB 270725 Elevator Trim Tab Actuator (Right) - Lubrication Resolution: COMPLIED WITH CMP GIIB 270725 Elevator Trim Tab Actuator (Right) - Lubrication. Work done IAW CMP 270725 & GIIB M/M 27-04-00. Discrepancy: 12.34 CMP GIIB 271005 Aileron Boost Bell Crank (Left) - Inspection Resolution: COMPLIED WITH CMP GIIB 271005 Aileron Boost Bell Crank (Left) - Inspection as required IAW GIIB MM 27-02-00.No defects noted. Ref contingency sheet. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WoikOrderPreliminarylnvoicespt Page 62 of 98 Printed: 3/23/2012 4:28:32P) Ftst X EFTA01080554 Bill To: HYPERION AIR, INC. WON: SC10420 Invoice Number: 7112000954 Labor USD: No Charge N/ C Step: 12.34.1 Completed Complied with section (B) 14 in procedure; the measurements are .625 on upper ID of shaft hole, lower bushing II) Ls.625 and OD Is .748 and lower hole size ID is .625 all dimensions are within hnits IAW GLIB AMM. Discrepancy: 12.35 CMP GlIB 271012 Aileron Actuator (Left) - Inspection Resolution: COMPLIED WITH CMP GIIB 271012 Aileron Actuator (Left) - Inspection and wing attach fittings measured within limits of .250-.252 IAW G-IIB AMM 27.02.00. No defects found. Discrepancy: 12.36 CMP GlIB 271014 Aileron Boost Bell Crank (Right) - Inspection Resolution: Complied with CMP GIIB 271014 Aileron Boost Bell Crank (Right) - Inspection as required IAW GIIB MM 27-02-00. Refer to squawk 8.27 for discrepency noted. Labor USD: No Charge N/ C Step: 12.36.1 Step: 12.36.2 Completed Compleate steps A-B(4) IAW (MB AMM 27-02-00. Completed Compleate steps A through B(4) IAW GIIB AMM 27-02-00 Discrepancy: 12.37 CMP GIIB 271017 Aileron Actuator (Right) - Inspection Resolution: COMPLIED WITH CMP GIIB 271017 Aileron Actuator (Right) - Inspection IAW GIIB AMM 27-02-00. Ref to squawk 8.32 for discrepencies. Labor USD: No Charge N/ C Step: 1237.1 Completed Compleate steps A through B-(3) IAW GIIB AMM 27-02-00 Discrepancy: 12.38 CMP GHB 271021 Elevator Actuator - Inspection Resolution: COMPLIED WITH CMP GIIB 271021 Elevator Actuator - Inspection IAW GIIB MM 27.01.00. No defects noted at this time. Labor USD: No Charge N/ C Discrepancy: 12.39 CMP GlIB 271311 Rudder Actuator and Forward Attach Fitting - Inspection Resolution: COMPLIED WITH CMP GIIB 271311 Rudder Actuator and Forward Attach Fitting - Inspection as required. No discrepancies found at this time. All work performed I.A.W. (MB M.M. 27-03.00 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 63 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080555 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 12.40 CMP GLIB 271314 Rudder Trim Tab Actuator - Inspection Resolution: COMPLIED WITH CMP GIIB 271314 Rudder Trim Tab Actuator - Inspection as required. No discrepancies found at this time. All work performed I.A.W. GIIB 117.117. 27.04.00. Labor USD: No Charge N/ C Discrepancy: 12.41 CMP GIIB 271511 Aileron Trim Tab Actuator - Inspection Resolution: COMPLIED WITH CMP GIIB 271511 Aileron Trim Tab Actuator - Inspection No defects found IAW GIIB AMM 27-04-00. Labor USD: No Charge N/ C Discrepancy: 12.42 CMP GIIB 274011 Flap Actuator Yoke (Left Outboard) - Inspection Resolution: COMPLIED WITH CMP GIIB 274011 Flap Actuator Yoke (Left Outboard) - Inspection. Work IAW GIIB MM 27-40-00 Labor USD No Charge N/ C Discrepancy: 12.43 CMP GIIB 274012 Flap Actuator Yoke (Left Inboard) - Inspection Resolution: COMPLIED WITH CMP GIIB 274012 Flap Actuator Yoke (Left Inboard) - Inspection. Work IAW GIIB MM 27.40.00. Labor USD: No Charge N/ C Discrepancy: 12.44 CMP GIIB 274311 Flap Actuator Yoke (Right Outboard) - Inspection Resolution: COMPLIED WITH CMP GIIB 274311 Flap Actuator Yoke (Right Outboard) - Inspection IAW GIIB AMM 27-06-00. See item 8.16 for discrepency 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_WorkOrderPreliminaryInvoicespt Page 64 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080556 Bill To: HYPERION AIR, INC. Labor USD: No Charge WON: SC10420 Invoice Number: 7112000954 N/ C Step: 12.44.1 Completed Complied with CMP (MB 274311 Flap Actuator Yoke (Right Outboard) - Inspection. Step A. through B.(2). All maintenance performed IAW GOB MM 27-06.00. Discrepancy: 12.45 CMP GlIB 274312 Flap Actuator Yoke (Right Inboard) - Inspection Resolution: COMPLIED WITH CMP GIIB 274312 Flap Actuator Yoke (Right Inboard) - Inspection IAW (MB AMM 27-06.00.No defects noted. Labor USD: No Charge N/ C Step: 12.45.1 Completed Complied with CMP (MB 274312 Flap Actuator Yoke (Right Inboard) - Inspection. Step A through B.(4). All maintenance performed IAW GOB MM 27-064)0. Discrepancy: 12.46 CMP GIIB 274813 Ground Spoiler Actuator (Left) - Inspection (Aircraft Having 6 Panel Speed Brakes) Resolution: COMPLIED WITH CMP GIIB 274813 Ground Spoiler Actuator (Left) - Inspection (Aircraft Having 6 Panel Speed Brakes) No defects found IAW GIIB AMM 27.01.00. Labor USD: No Charge N/ C Discrepancy: 12.47 CMP GIIB 274818 Ground Spoiler Actuator (Right) - Inspection (Aircraft Having 6 Panel Speed Brakes) Resolution: COMPLIED WITH CMP GIIB 274818 Ground Spoiler Actuator (Right) - Inspection (Aircraft Having 6 Panel Speed Brakes) No defects found IAW GlIB AMM 27-02-00 Labor USD: No Charge N/ C Discrepancy: 12.48 CMP GlIB 275312 Flight Spoiler Actuator (Left) - Inspection Resolution: COMPLIED WITH CMP GIIB 275312 Flight Spoiler Actuator (Left) - Inspection IAW GIIB MM 27.02.00. See squawk item 8.87 for discrepancy corrective action. Labor USD: No Charge N/ C Discrepancy: 12.49 CMP GIIB 275317 Flight Spoiler Actuator (Right) - Inspection Resolution: COMPLIED WITH CMP GIIB 275317 Flight Spoiler Actuator (Right) - Inspection IAW GIIB MM 27-02-00. See squawk items 8.85 / 8.86 for discrepancy corrective actions. 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 65 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080557 Bill To: HYPERION AIR, INC. WO ft: SC10420 Invoice Number: 7112000954 Labor USD: No Charge N/ C Discrepancy: 12.50 CMP GlIB 280510 Fuel Control System - Functional Test Resolution: COMPLIED WITH CMP GIIB 280510 Fuel Control System - Functional Test IAW 28.05-00. No defects noted. Discrepancy: 12.51 CMP 61IB 321210 Left Anti-Skid Valve Filter - Inspection Resolution: COMPLIED WITH CMP GlIB 321210 Left Anti-Skid Valve Filter - Inspection IAW G2-B AMM 32-04-02 with no defects noted. Labor USD: Billing Method Hours Rate Total No Charge N/ C Pans USD: Time and Material $0.91 Total USD: $0.91 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 12.51 #1 NASI612-4A SEAL, 0.250 INCH OD TUBING 1 $0.43 $0.43 12.51 #2 NASI612-6A O-RING 1 $0.48 $0.48 Discrepancy: 12.52 CMP GlIB 321215 Right Anti-Skid Valve Filter - Inspection Resolution: COMPLIED WITH CMP GIIB 321215 Right Anti-Skid Valve Filter - Inspection IAW 62-B AMM 32-04-02 with no defects noted. Labor USD: Billing Method Hours Rate Total No Charge N/ C Pans USD: Time and Material $0.91 Total USD: $0.91 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 12.52 #1 NASI612-4A SEAL, 0.250 INCH OD TUBING I $0.43 $0.43 12.52 #2 NASI612-6A O-RING I $0.48 $0.48 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 66 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080558 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Discrepancy: 12.53 CMP GLIB 330200 Emergency Exit Light Battery - Scrap Resolution: COMPLIED WITH CMP GlIB 330200 Emergency Exit Light Battery - Scrap IAW GlIB AMM 33-02-00. Discrepancy: 12.54 CMP GlIB 331510 Emergency Exit Light Battery - Replacement Resolution: COMPLIED WITH CMP GlIB 331510 Emergency Exit Light Battery - Replacement IAW GIIB AMM 33-02-00. See item 6.1 for discrepancy noted. Labor USD: No Charge N/ C Discrepancy: 12.55 CMP GlIB 341524 Attitude Indicator Battery No. 1 - Service (PS 823) Resolution: COMPLIED WITH CMP GlIB 341524 Attitude Indicator Battery No. 1 - Service (PS 823) IAW GlIB AMM 34-04-00. No defects noted. AVIALL WO43520715. Removed battery P/N 501.1075.02 S/N 2060. Installed TESTED unit P/N 501-1075-02 S/N 2060. Updated CMP's 341530 and 341524. Billing Method Hours Rate Total Labor USD: No Charge Services USD: Time and Material Total USD: Services: N/ C $1,432.86 $1,432.86 Ref. No. Description Quantity Sell Price USD Extended USD 12.55 #1 SERVICE 1.00 $1,432.86 $1,432.86 Part Ref: 501-1075-02 POWER SUPPLY Step: 12.55.1 Completed Removed Attitude Indicator battery P/N 501-1075-02 S/N 2060 for service. All work accomplished IA \\ GlIB AMM M-04-00. Discrepancy: 12.56 CMP GlIB 351615 Oxygen Cylinder (No. 2) - Hydrostatic Test Resolution: COMPLIED WITH CMP GlIB 351615 Oxygen Cylinder (No. 2) - Hydrostatic Test oxygen cyclinder. Hydro complied with by Ameron Global CRS RU2R148L on 2/10/12. Next Hydro due 2/2015. See item 12.154 for P/N and S/N information. Billing Method Hours Rate Total Labor USD: No Charge N/ C Services USD: Time and Material $250.01) Total USD: $250.00 Services: Ref. No. Description Quantity Sell Price USD Extended USD 12.56 #1 Vendor Supplied Labor 1.00 $250.00 $250.00 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 67 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080559 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Services: Ref. No. Description Quantity Sell Price USD Extended USD Part Ref: 176521-64 CYLINDER 64 CUBIC Ff. Discrepancy: 12.57 CMP GLIB 351620 Oxygen Cylinder (No. 3) - Hydrostatic Test Resolution: COMPLIED WITH CMP GIIB 351620 Oxygen Cylinder (No. 3) - Hydrostatic Test oxygen cyclinder. Hydro complied with by Ameron Global CRS RU2R148L on 2/10/12. Next Hydro due 2/2015. See item 12.158 for P/N and S/N information. Billing Method Hours Rate Total Labor USD: No Charge N/ C Services USD: Time and Material $250.00 Total USD: $250.00 Services: Ref. No. Description Quantity Sell Price USD Extended USD 12.57 #1 Vendor Supplied Labor 1.00 $250.00 $250.00 Part Ref: 17652149 BOTTLE, OXYGEN Discrepancy: 12.58 CMP GIIB 351623 Portable Oxygen Bottle (No. 1) - Service / Hydrostatic Test Resolution: COMPLIED WITH CMP GIIB 351623 Portable Oxygen Bottle (No. 1) - Service / Hydrostatic Test all work done by Ameron Global Product Support , tracking referance # 255045. Next due date 02/2017. Billing Method flours Rate Total Services USD: Time and Material $250.00 Total USD: $250.00 Services: Ref. No. Description Quantity Sell Price USD Extended USD 12.58 #1 Vendor Supplied Labor 1.00 $250.00 $250.00 Part Ref: 900-002-035.01 portable O2 bottle Discrepancy: 12.59 CMP GIIB 380101 ELEMENT,FRESH WATER SYS FILTER Resolution: COMPLIED WITH CMP GIIB 380101 ELEMENT,FRESH WATER SYS FILTER. Removed filter P/N AL-II.OG NSN and installed new filter AL-11-06 NSN. Work IAW GIIB 38-00-00 Billing Method Hours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $59.51 Total USD: $59.51 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 68 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080560 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 1239 ftl AL-11-0G FILTER 1 $59.51 $59.51 Discrepancy: 12.60 CMP GLIB 531535 Shear Clips Aft Fuselage - Inspection Resolution: COMPLIED WITH CMP GIIB 531535 Shear Clips Aft Fuselage - Inspection. No defects noted at this time. Performed IAW GIIB MM 53-00-00. Labor USD: No Charge N/ C Discrepancy: 12.61 CMP GIIB 531545 Static Ports (RVSM) - Inspection Resolution: COMPLIED WITH CMP GIIB 531545 Static Ports (RVSM) - Inspection JAW GIIB MUM 53.00.00. No defects noted. Labor USD: No Charge N/ C Discrepancy: 12.62 CMP GlIB 534015 Main Power Junction Box Interior - Inspection Resolution: COMPLIED WITH CMP GIIB 534015 Main Power Junction Box Interior - Inspection. All work was done IAW Culfstream GIIB AMM 53.40-15. No defects noted. Discrepancy: 12.63 CMP GlIB 539010 Main Landing Gear Installation (Left) - Inspection Resolution: COMPLIED WITH CMP GIIB 539010 Main Landing Gear Installation (Left) - Inspection, IAW GLIB NUM Chapter 53.00.00. No defects noted at this time. Labor USD: No Charge N/ C Discrepancy: 12.64 CMP GIIB 539020 Main Landing Gear Installation (Right) - Inspection Resolution: COMPLIED WITH CMP GM 539020 Main Landing Gear Installation (Right) - Inspection IAW GIIB MM 53-00-00. No defects noted at this time. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelitninarylnvoicespt Page 69 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080561 Bill To: HYPERION AIR, INC. Labor USD: No Charge WON: SC10420 Invoice Number: 7112000954 N/ C Discrepancy: 12.65 CMP GLIB 553035 Rudder Leading Edge and Ballast Weight Corrosion - Inspection Resolution: COMPLIED WITH CMP GIIB 553035 Rudder Leading Edge and Ballast Weight Corrosion - Inspection JAW GII-B AMM 55-00-00. No defects noted. Labor USD: Pans USD: Total USD: Billing Method Flours Rine Total No Charge Flat Rate N/ C $2,500.00 $2,500.00 Pans: Ref. No. Part number: Description Quantity 12.65 #1 NASI919M05.04 RIVET 200 12.65 #2 NASI919M05.05 RIVET 300 12.65 #3 NASI919M05.06 RIVET 200 12.65 #4 NASI9191O04-03 RIVET 100 12.65 #5 NASI919M05.03 RIVET 38 12.65 #6 NAS1919M05.03 RIVET 62 12.65 #7 PRI.140-B-U2 SEALANT, PRC,CARTRIDGE I Step: 12.65.1 Completed Complied with rudder ballast weight inspection section (B) 1-5, IAW G-II B AMM 55-00-00. Found no corrosion on ballast weights or cracks on the structure for the ballast weights. Discrepancy: 12.66 CMP (NIB 575002 Winglet Attach Hardware (Right) - Inspection Resolution: COMPLIED WITH CMP GM 575002 Winglet Attach Hardware (Right) - Inspection. IAW (NIB AMM 57.00.00. Ref squawk 8.62 for discrepencies. Billing Method Flours Rate Total Labor USD: No Charge N/ C Pans USD: Time and Material $127.00 Total USD: $127.00 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 12.66 #I 6856K GREASE, MASTINOX 1 $127.00 $127.00 Discrepancy: 12.67 CMP CHB 575003 Winglet Attach Hardware (Left) - Inspection Resolution: COMPLIED WITH CMP GIIB 575003 Winglet Attach Hardware (Left) - Inspection IAW G-II AMM 57-00-00. Found 10 bores with corrosion in them see squawk 8.73 for repair information. 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 70 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080562 Bill To: HYPERION AIR, INC. WO It: 5C10420 Invoice Number: 7112000954 Step: 12.67.1 Completed Complied with section (B) step[-3. Found 10 winglet bores with some corrosion see squawk 8.73 . Discrepancy: 12.68 CMP GLIB 575005 Wing Exterior (Left) - Inspection (GIIB) Resolution: COMPLIED WITH CMP GIIB 575005 Wing Exterior (Left) - Inspection (CHB) JAW GlIB MM 57-00-00. Discrepancies were entered under item 8. Labor USD: No Charge N/ C Discrepancy: 12.69 CMP GIIB 575010 Wing Exterior (Right) - Inspection (GlIB) Resolution: COMPLIED WITH CMP GIIB 575010 Wing Exterior (Right) - Inspection (GIIB) 'ANN' GLIB MM 57-00-00. Refer to Squawks 8.14 for discrepancy noted . Labor USD: No Charge NI C Step: 12.69.1 Step: 12.69.2 Completed Complyed with CUPS, 575010 sections 1.5 JAW GIIB MM 57-00-00. Sections 6-10 still remain to be completed. Completed Complyed with CMPit 575010 R/H wing exterior inspection IAW (HIB MM 57-00-00. Go to Squawks 8.14 for discrepancy corrective action. Discrepancy: 12.70 CMP GIIB 575025 Wing to Fuselage Interior (Left) - Inspection (GIIB) Resolution: COMPLIED WITH CMP GIIB 575025 Wing to Fuselage Interior (Left) - Inspection (GIIB) IAW GIIB MM 57-00-00. Go to Squawk 8.2 for discrepancy corrective action. Labor USD: No Charge N/ C Step: 12.70.1 Completed Completed CMP# 575025 wing to fuselage interior ( Left ) inspection Sections A I &2 , and section B subsection 1 a through i JAW GIIB MM 57-00-00. Go to Squawk 8.2 for discrepancy corrective action. Discrepancy: 12.71 CMP GLIB 575030 Wing to Fuselage Interior (Right) - Inspection (GIIB) Resolution: COMPLIED WITH CMP GIIB 575030 Wing to Fuselage Interior (Right) - Inspection (611B) JAW GIIB MM 57-00-00. Go to Squawk 8.2 for discrepancy corrective action. Labor USD: No Charge N/ C Step: 12.71.1 Step: 12.71.2 Completed Began CMP# 575030 wing to fuselage interior inspection IAN' GIIB MM 57.00.00. Note: Screws of access panels are rusted/corroted. Completed Completed CMP# 575030 wing to fuselage interior ( Right ) inspection Sections A 1&2 , and section B subsection 1 a through i IAW GIIB MM 57-00-00. Go to Squawk 8.2 for discrepancy corrective action. 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 71 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080563 Bill To: HYPERION AIR, INC. WO ft: SC10420 Invoice Number: 7112000954 Discrepancy: 12.72 CMP GLIB 575049 Wing Plank Fastener / Radius Block Removal (Left) - Corrosion Inspection (GIIB) Resolution: COMPLIED WITH CMP GIIB 575049 Wing Plank Fastener / Radius Block Removal (Left) - Corrosion Inspection (GHB) IAW GIIB 57-00.00. Work performed by Structual testing systems Cert. # ES1R124K.refer to squawk 8.122 for discrepency noted. Labor USD: Parts USD: Step: 12.72.1 Step: 12.72.2 Step: 12.72.3 Step: 12.72.4 No Charge No Charge Completed Completed Completed Completed N/ C N/C Removed Fuel panels 21-FT LWR-1, 2I-FT LWR-2, 21-FT LWR-3, 21-FT LWR-4, 22-FT LWR-I,22FT LWR-2. 22-FT LWR-3, 22-FT LWR-4, 22-17 UPR-12, 22-FT UPR-I3, 22-FT UPR-15, 22 FT UPR-17. Done I.A.W. GIIB 57.00.00. Began removing Hi-loc fasteners IAW GIIB AMM 57.00.00. Finished removing Iii-Loc fasteners and complied with CMP GlIB 575049 Wing Plank Fastener / Radius Block Removal (Left) - Corrosion Inspection (GIIB) Step 2(a). Completed Inspection By Structual Testing Systents (Cert. # ESIR124K). Refer To Squawk 8.122 For Discrepency Noted. Completed Re-installation Of Hi-Loc Fasteners And Complied With (CMP (MB 575049) Wing Plank Fastener / Radius Block Removal (Left) - Corrosion Inspection. All hlaintenence Performed In Reference To GIIB AMM 57-00-00. Discrepancy: 12.73 CMP GlIB 575054 Wing Plank Fastener / Radius Block Removal (Right) - Corrosion Inspection (GlIB) Resolution: COMPLIED WITH CMP GIIB 575054 Wing Plank Fastener / Radius Block Removal (Right) - Corrosion Inspection (611B) JAW GIIB 57-00-00. Work performed by Structual testing systems Cert. # ES1R124K. No defects noted.. Labor USD: Parts USD: Total USD: Parts: Billing Method No Charge Time and Material Hours Rate Total N/C $533.69 $533.69 Ref. No. Part number: Description Quantity Sell price USD Extended USD 12.73 #1 HL70-8 COLLAR 220 $0.90 $198.00 12.73 #2 GABS 10B4-13 BOLT 3 $2.83 $8.49 12.73 #3 GAB510B4-7 BOLT 10 S1.90 $19.00 12.73 #4 GABS 10B4-8 BOLT 10 $22.57 $225.70 12.73 #5 GAB510B4-9 BOLT 10 $2.07 $20.70 12.73 #6 GAB510B4-6 BOLT 10 $6.18 $61.80 Step: 12.73.1 Step: 12.73.2 Step: 12.73.3 Step: 12.73.4 Completed Completed Completed Completed Removed Fuel panels 21-FT LWR-1, 21-FT LWR-2, 21-FT LWR-3, 21-FT LWR-4, 22-FT LWR-1, 22FT LWR-2. 22-FT LWR-3, 22-FT LWR-4, 22-FT UPR-12, 22-FT UPR-I3, 22-FT UPR-I5, 22 FT UPR-17. Done I.A.W. GIIB 57.00.00. Began removing Hi-loc fasteners IAW (NIB AMM 57.00.00. Finished removing Iii-Loc fasteners and complied with CIIIP GIIB 575054 IVing Plank Fastener / Radius Block Removal (Left) - Corrosion Inspection (GIIB) Step 2(a). Completed Inspection By Structual Testing Systents (Cert. # ES1R124K). Refer To Squawk 8.122 For Discrepency Noted. Completed Re-installation Of Hi-Lac Fasteners And Complied With (CMP (MB 575049) Wing Flank Fastener / Radius Block Removal (Left) - Corrosion Inspection. All Maintenence Performed In Reference To GlIB AMM 57-00-00. Discrepancy: 12.74 CMP (MB 575065 Wing Rear Beam (Left) - Inspection (GIIB) 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 72 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080564 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Resolution: COMPLIED WITH CMP GIIB 575065 Wing Rear Beam (Left) - Inspection (GIIB). Work IAW GlIB MM57-00-00 Discrepancy: 12.75 CMP GlIB 575070 Wing Rear Beam (Right) - Inspection (GlIB) Resolution: COMPLIED WITH CMP GIIB 575070 Wing Rear Beam (Right) - Inspection (GHB).Work IAW GIIB MM57-00-00 Discrepancy: 12.76 CMP GHB 575086 Aileron Leading Edge and Ballast Weight Corrosion (Left) - Inspection (GIIB Resolution: COMPLIED WITH CMP GIIB 575086 Aileron Leading Edge and Ballast Weight Corrosion (Left) - Inspection (GIIB IAW GIIB MM 57.00.00. See Squawk items 8.63/8.64 and 8.65 for discrepancy corrective actions. Labor USD: No Charge N/ C Step: 12.76.1 Step: 12.76.2 Completed Began CMP#575086 Aileron leading edge and ballast weight corrosion ( LEFT ) inspection Sections A #'s 1-2, and section B tts 1.6 IAN? (MB MM 57-00-00. See Squawk items 8.63/8.64 and 8.65 for discrepancy corrective actions. Completed Complied with C1%11'8575086 Aileron leading edge and ballast weight corrosion ( LEFT ) inspection IAW (;11B MM 57.00.00. See Squawk items 8.63/8.64 and 8.65 for discrepancy corrective actions. Discrepancy: 12.77 CMP GIIB 575091 Aileron Leading Edge and Ballast Weight Corrosion (Right) - Inspection (GlIB) Resolution: COMPLIED WITH CMP GUS 575091 Aileron Leading Edge and Ballast Weight Corrosion (Right) - Inspection (GlIB) IAW GIIB MM 57.00.00. See squawk item 8.63 for discrepancy corrective actions. Labor USD: No Charge N/ C Discrepancy: 12.78 CMP GIIB 575105 Wing Wedge (Left) - Inspection (GlIB) Resolution: COMPLIED WITH CMP GIIB 575105 Wing Wedge (Left) - Inspection (GIIB) IAW GlIB 57.00.00. Work performed by Structual testing systems Cert. # ESIR124K.See item 8.126 for discepency noted.. Labor USD: No Charge N/ C Step: 12.78.1 Completed Complied with section (B) 1, removed Lai wing wedge IAW G-IIB AMM 57-00-00. Discrepancy: 12.79 CMP GIIB 575110 Wing Wedge (Right) - Inspection (GIIB) 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_WorkOrderFreliminaryInvoicespt Page 73 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080565 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Resolution: COMPLIED WITH CMP GIIB 575110 Wing Wedge (Right) - Inspection (GlIB) IAW GIIB 57-00-00. Work performed by Structual testing systems Cert. M ES1R124K.See item 8.126 for discrepency noted. Labor USD: No Charge N/ C Step: 12.79.1 Completed Completed steps A,B and C removing right wing wedge panel as required IAW GlIB AND' 57.00.00. REF Squawk 8.6 for discrepency noted. Discrepancy: 12.80 CMP GlIB 575115 Wing Sponson Rib (Left) - Inspection (GIIB) Resolution: COMPLIED WITH CMP GlIB 575115 Wing Sponson Rib (Left) - Inspection (GIIB). Work IAW GIIB MM 57-51-00 Labor USD: No Charge N/ C Discrepancy: 12.81 CMP GIIB 575120 Wing Sponson Rib (Right) - Inspection (GlIB) Resolution: COMPLIED WITH CMP GIIB 575120 Wing Sponson Rib (Right) - Inspection (GIIB)All work done per G-IIB amm ch 05.01-00. No defects noted. Labor USD: No Charge N/ C Discrepancy: 12.82 CMP G1111 731510 TEST ENG TEMP CONT SYS Resolution: COMPLIED WITH CMP GIIB 731510 TEST ENG TEMP CONT SYS with no faults noted. All work done IAW RR Spay 511-8 EMM 5-10. Labor USD: No Charge N/ C Discrepancy: 12.83 CMP GIIB 732010 Engine Temperature Control System - Functional Test Resolution: COMPLIED WITH CMP GIIB 732010 Engine Temperature Control System - Functional Test with no faults noted. All work done IAW RR Spay 511.8 EMM 5.10. Labor USD: No Charge N/ C Discrepancy: 12.84 CMP (NIB 733015 ENG LP GOY RESET CK 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 74 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080566 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Resolution: Performed CMP code 733015 as per GIIB Rolls Royce EMM 5.10. No defects were noted. Discrepancy: 12.85 CMP GlIB 733515 ENG LP GOV RESET CK Resolution: COMPLIED WITH CMP GIIB 733515 ENG LP GOV RESET CK as per Rolls Royce EMM 5-10. No defects were noted. Discrepancy: 12.86 CMP GIIB 771510 ENG TGT CIRCUIT RES CHECK Resolution: COMPLIED WITH CMP GIIB 771510 ENG TGT CIRCUIT RES CHECK. No defects noted. Work performed IAW GAC GIIB MM 77-04-00. Labor USD: No Charge N/ C Discrepancy: 12.87 CMP GIIB 771515 ENG TGT CIRCUIT RES CHECK Resolution: COMPLIED WITH CMP GIIB 771515 ENG TGT CIRCUIT RES CHECK. No defects noted. Work performed IA W GAC GIIB MM 77-04-00. Labor USD: No Charge N/ C Discrepancy: 12.88 CMP GlIB 801520 Engine Starter (Left) - Oil Change Resolution: COMPLIED WITH CMP GIIB 801520 Engine Starter (Left) - Oil Change with no defects noted IAW 62-B AMM 80-01-00. Labor USD: Billing Method Hours Rate Total No Charge N/ C Parts USD: Time and Material $115.28 Total USD: $115.28 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 12.88 #1 S9809-6 GASKET "C" 1 $3.71 $3.71 12.88 #2 S9809-3 GASKET S8995-3 2 $8.84 $17.68 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 75 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080567 Bill To: HYPERION AIR, INC. WO ft: SC10420 Invoice Number: 7112000954 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 12.88 #5 BE20057 SEAL 2 S39.94 $79.88 12.88 #4 KB21614 SEAL 1 $14.01 $14.01 Discrepancy: 12.89 CMP GHB 801535 Engine Starter (Right) - Oil Change Resolution: COMPLIED WITH CMP GIIB 801535 Engine Starter (Right) - Oil Change TAW G2-B MUM 80-01-00 with no defects noted. Billing Method I lour. Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $115.28 Total USD: $115.28 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 12.89 #1 S9809-6 GASKET "C" 1 $3.71 $3.71 12.89 #2 S9809-3 GASKET 58995-3 2 $8.84 $17.68 12.89 #5 BE20057 SEAL 2 $39.94 $79.88 12.89 #4 KB21614 SEAL I $14.01 $14.01 Step: 12.89.1 Completed COMPLIED WITH CMP (MB 801535 Engine Starter (Right) Oil Change steps A. to B(7). Awaiting for filler plug gasket. Discrepancy: 12.90 CMP GHB 997407 AD74-08-09 R2 MOD LAVATORIES Resolution: COMPLIED WITH CMP GIIB 997407 AD74-08-09 R2, MOD LAVATORIES, IAW AD 74-08-09 R2. No defects noted. Next due 11804.3 Airframe hours. Discrepancy: 12.91 RELATED CMP CODES Resolution: Complied with related codes. Discrepancy: 12.92 CMP GIIB 243510 Alternator, Left Engine Resolution: COMPLIED WITH CMP GIIB 243510 L Engine Alternator - Removal / Installation P/N 28B135-126A, S/N 119, IAW GIIB MM 24-02-04. No defects noted at this time. 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 76 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080568 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Step: 12.92.1 Step: 12.92.2 Completed Removed Left engine alternator ( P/N: 28BI35-126A ; S/N: 119 ) LAW GIIB MM 24-02-04. No defects noted at this time. Completed Installed Left engine alternator ( P/N: 28B135-126A ; S/N: 119 ) IAW GLIB MM 24-02-04. No defects noted at this time. Discrepancy: 12.93 CMP GIIB 244010 Alternator, Right Engine Resolution: COMPLIED WITH CMP GIIB 244010 R Engine Alternator - Removal / Installation P/N 28B135.126A, S/N 369, IAW GIIB MM 24-02-04. No defects noted at this time. Labor USD: No Charge N/ C Discrepancy: 12.94 CMP GIIB 252031 VEST, LIFE NO 1 Resolution: COMPLIED WITH CMP GIIB 252031 VEST, LIFE NO 1. Removed life vest #1 P/N PO1074-101 S/N 263978 and installed #1 life vest P/N P01074-101 S/N263978, IAW GIIB MM chapter 25.00.00. Next inspection due 9/2013. Step: 12.94.1 Completed Complied with section (A) removal and inspection of #1 life vest IAW G-IIB AMM 25-20-31. Next inspection due date is SEPT. 2013. Discrepancy: 12.95 CMP GM 252032 VEST, LIFE NO 2 Resolution: COMPLIED WITH CMP GIIB 252031 VEST, LIFE NO 2. Removed life vest #2 P/N PO1074-101 S/N 264254 and installed overhauled life vest P/N S-21850-6300 S/N 82901-1141, IAW GIIB MM chapter 25.00.00. Next inspection due 2/2015. Discrepancy: 12.96 CMP GIIB 252033 VEST, LIFE NO 3 Resolution: COMPLIED WITH CMP GIIB 252033 VEST, LIFE NO 3. Removed life vest #3 P/N P01074-101 S/N 263936 and installed overhauled life vest P/N 51850-6300 S/N 21987-1660, IAW GIIB MM chapter 25.00-00. Next inspection due 2/2015. Discrepancy: 12.97 CMP GIIB 252034 VEST, LIFE NO 4 Resolution: COMPLIED WITH CMP GIIB 252034 VEST, LIFE NO 4. Removed life vest #4 P/N PO1074-101 S/N 263871 and installed overhauled life vest P/N S-51850-6300 S/N 20071-1660, IAW GIIB MM chapter 25.00.00. Next inspection due 2/2015. 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 77 of. 98 Printed: 3/23/2012 4:28:32M Rd X EFTA01080569 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 12.98 CMP GlIB 252035 VEST, LIFE NO 5 Resolution: COMPLIED WITH CMP GIIB 252035 VEST, LIFE NO 5. Removed life vest #5 P/N PO1074-101 S/N 264143 and installed overhauled life vest P/N S-51850-6300 S/N 21948-1660, IAW GIIB MM chapter 25.00.00. Next inspection due 2/2015. Discrepancy: 12.99 CMP GlIB 252036 VEST, LIFE NO 6 Resolution: COMPLIED WITH CMP GIIB 252036 VEST, LIFE NO 6. Removed life vest #6 P/N PO1074-101 S/N 264059 and installed #6 life vest P/N P01074-101 S/N 264059, IAW GIIB MM chapter 25.00.00. Next ispection due 9/2013. Step: 12.99.1 Completed Complied with section (A) removal and inspection of #6 life eNt 1:11 6-11B AMM 25-20-31. Next inspection due date is SEPT. 2013. Discrepancy: 12.100 CMP (MB 252037 VEST, LIFE NO 7 Resolution: COMPLIED WITH CMP GIIB 252037 VEST, LIFE NO 7. Removed life vest #7 P/N PO723E105P S/N 57151 and installed overhauled life vest P/N P01074-101 S/N 264256., IAW GIIB MM chapter 25-00-00. Next inspection due 2/2017. Discrepancy: 12.101 CMP GIIB 252038 VEST, LIFE NO 8 Resolution: COMPLIED WITH CMP GIIB 252038 VEST, LIFE NO 8. Removed life vest #8 P/N PO1074-101 S/N 263943 and installed #8 life vest P/N P01074-101 S/N 263943, IAW GIIB MM chapter 25.00.00. Next inspection due 9/2013. Step: 12.101.1 Completed Complied with section (A) removal and inspection of #8 life vest P/N P01074-101 S/N 263943 IAW 641B AMM 25-20-31. Next inspection due date is SEPT. 2013. Discrepancy: 12.102 CMP GIIB 252039 VEST, LIFE NO 9 Resolution: COMPLIED WITH CMP GIIB 252039 VEST, LIFE NO 9. Removed life vest #9 P/N PO1074-101 S/N 264108 and installed #9 life vest P/N P01074-101 S/N 264108, IAW GIIB MM chapter 25.00.00. Next inspection due 9/2013. 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 78 of 98 Printed: 3/23/2012 4:28:32PP Rd X EFTA01080570 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Step: 12.102.1 Completed Complied with section (A) removal and inspection of #9 life vest P/N P01074-101 S/N 264108 IAW G-IIB AMM 25-20-31. Next inspection due date is SEPT. 2013. Discrepancy: 12.103 CMP GIIB 252040 VEST, LIFE NO 10 Resolution: COMPLIED WITH CMP GIIB 252040 VEST, LIFE NO 10. Removed life vest #10 P/N P01074-101 S/N 264206 and installed overhauled life vest P/N P01074-101 S/N 264206, IAW GIIB MM chapter 25-00.00.. Next inspection due 2/2017. Step: 12.103.1 Completed Complied with section (A) removal and inspection of #10 life vest P/N P01074-101 S/N 264206 IAW G-IIB AMM 25-20-31. Next inspection due date is SEPT. 2013. Discrepancy: 12.104 CMP GIIB 252041 VEST, LIFE NO 11 Resolution: COMPLIED WITH CMP GIIB 252041 VEST, LIFE NO 11. Removed life vest #11 PIN P01074-101 S/N 264204 and installed #11 life vest PIN P01074-101 S/N 264204, IAW GIIB MM chapter 25-00-00. Next inspection due 9/2013. Step: 12.104.1 Completed Complied with section (A) removal and inspection of #11 life vest P/N P01074-101 S/N 264204 IAW (;-IIB AMM 25-20-31. Next inspection due date is SEPT. 2013. Discrepancy: 12.105 CMP GIIB 252042 VEST, LIFE NO 12 Resolution: COMPLIED WITH CMP GIIB 252042 VEST, LIFE NO 12. Removed life vest #12 P/N P01074-101 S/N 263941 and installed #12 life vest PIN P01074-101 S/N 263941, IAW GIB MM chapter 25-00-00. Next inspection due 9/2013. Step: 12.105.1 Completed Complied with section (A) removal and inspection of #12 life vest P/N P01074-101 SIN 263941 IAW G-IIB AMM 25-20-31. Next inspection due date is SEPT. 2013. Discrepancy: 12.106 CMP GIIB 252043 VEST, LIFE NO 13 Resolution: COMPLIED WITH CMP GIIB 252043 VEST, LIFE NO 13. Removed life vest #13 P/N 3505-101 S/N Q0503655 and installed overhauled life vest PIN P01074-101 S/N 689973, IAW GIIB MM chapter 25.00.00. Next inspection due 2/2017. Discrepancy: 12.107 CMP GIIB 252044 VEST, LIFE NO 14 Resolution: COMPLIED WITH CMP GIIB 252044 VEST, LIFE NO 14. Removed life vest #14 P/N P01074-101 SIN 264247 and installed overhauled life vest PIN P01074-101 S/N 264247, IAW GIIB MM chapter 25.00.00. Next inspection due 2/2017. Step: 12.107.1 Completed Complied with section (A) removal and inspection of #14 life vest P/N P01074-101 S/N 264247 IAW (;-IIB AMM 25-20-31. Next inspection due date is SEPT. 2013. 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 79 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080571 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Discrepancy: 12.108 CMP GLIB 252056 LIFE VEST, JUMPSEAT Resolution: COMPLIED WITH CMP GIIB 252056 LIFE VEST, JUMPSEAT. Removed jump seat life vest P/N 3505-101 S/N Q0704477 and installed overhauled vest P/N 3505-101 S/N Q0704477, IAW GIIB MM chapter 25.00.00. Next inspection due 2/2014. Step: 12.108.1 Completed Complied with section (A) removal and inspection of Jumpseat life vest P/N 3505-101 S/N Q0704477 IAW G-IIB AMM 25.20.31. Next inspection due date is Discrepancy: 12.109 CMP GIIB 252057 LIFE VEST, PILOT Resolution: COMPLIED WITH CMP GIIB 252057 LIFE VEST, PILOT. Removed pilot's life vest P/N S51850-6300 S/N 21965-1660 and installed overhauled life vest P/N 551850-6300 S/N 21965.1660, JAW GIIB MM chapter 25-00.00. Next inspection due 2/2015. Step: 12.109.1 Completed Complied with section (A) removal and inspection of pilot's life vest P/N 551850-6300 S/N 21965-1660 lAW 6-11B AMM 25-20-31. Next inspection due date is Discrepancy: 12.110 CMP GIIB 252058 LIFE VEST, CO-PILOT Resolution: COMPLIED WITH CMP GIIB 252058 LIFE VEST, CO-PILOT. Removed Co-pilots life vest P/N P0723W105P S/N 74634 and installed Co-pilots life vest P/N P0723E105P S/N 74634, IAW GIIB MM chapter 25.00.00. Next inspection due 9/2013. Step: 12.110.1 Completed Complied with section (A) removal and inspection 4C0-Pilot's life vest P/N P0723W105P S/N74634 lAW G-11B AMM 25-20-31. Next inspection due date is Discrepancy: 12.111 CMP GIIB 266626 HALON FIRE EXT, COCKPIT Resolution: COMPLIED WITH CMP GIIB 266626 HALON FIRE EXT, COCKPIT. Removed Fire Extinguisher P/N 6120.0000, S/N W575565 and installed Fire Extinguisher P/N 6120-0000, S/N W575565. All work done per G-IIB amm ch 26-03-(10. No defects noted. Labor USD: No Charge N/ C Discrepancy: 12.112 CMP GIIB 266627 HALON FIRE EXT, FWD CABIN Resolution: COMPLIED WITH CMP GIIB 266627 HALON FIRE EXT, FWD CABIN. Removed Fire Extinguisher P/N C352, S/N X-983309 and installed Fire Extinguisher P/N C352, S/N X-983309. All work done per G-IIB amm ch 26.03-00. No defects noted 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_WoikOrderPreliminarylnvoicespt Page 80 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080572 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 12.113 CMP (MB 266629 BAGG COMP HALON FIRE BTL Resolution: COMPLIED WITH CMP GIIB 266629 BAGG COMP HALON FIRE BTL. Removed Fire extinguisher P/N 898052, S/N 575549 and installed Fire extinguisher P/N 898052, S/N 575549. All work done per G-IIB amm ch 26.03.00. No defects noted. Labor USD: No Charge N/ C Discrepancy: 12.114 CMP GlIB 270115 Lateral Control System (Power) - Operational Test Resolution: COMPLIED WITH CMP GIIB 270115 Lateral Control System (Power) - Operational Test 1.1W GIIB ANIM 27.02.00. No defects noted. Discrepancy: 12.115 CMP GlIB 272010 Aileron (Left) Resolution: COMPLIED WITH CMP GIIB 272010 Aileron (Left). Removed LAI Aileron P/N 1159CS20006-5, S/N 151. Installed the LH aileron P/N 1159C520006-5, S/N 151 IAW GIIB MM 27-02-00. Billing Method Hours Rate Total Labor USD: No Charge N/ C Pans USD: Time and Material $6.19 Total USD: $6.19 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 12.115 #1 NAS6605D50 BOLT HEX HD-CLOSE TOL,DR I $6.19 $6.19 SHANK Step: 12.115.1 Step: 12.115.2 Completed Complied with CMP GlIB 272010 IJH Aileron Removal & Installation Step C to D. Removed Lai Aileron Pn#1159C520006.5 Sn#I51 All work done IAIV GlIB MM 27-2-00. Completed Installed the LH aileron PIN 1159CS20006-5, S/N 151 IAW GlIB MM 27-02-00. Discrepancy: 12.116 CMP GIIB 272015 Aileron (Right) Resolution: COMPLIED WITH CMP GIIB 272015 Aileron (Right). Removed the RH aileron P/N 1159C520006-6, S/N 151. Installed the same RH aileron P/N 1159CS20006-6, S/N 151 IAW GIIB MM 27.02.00. Ref contingency sheet. 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_WorkOrderPreliminaryInvoicespt Page 81 of 98 Printed: 3/23/2012 4:28:32P) Ftst X EFTA01080573 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Step: 12.116.1 Step: 12.116.2 Step: 12.116.3 Completed Removed upper and lower right wing aileron removal access panels IAW GIIB MM 05.04.01. No defects noted at this time. Completed Complied with CMP 272015 steps C. [I] thru [9]. Removed RH aileron P/N H59O;20006-6 S/N 151. All work done IAW GLIB MM 27-02-00 Completed Installed the RH aileron P/N 1159CS20006-6, S/N 151 lAW GLIB MM 27-02-00. Ref contingency sheet. Discrepancy: 12.117 CMP GLIB 272020 Aileron Trim Tab Resolution: Complied With CMP GIIB 272020 Aileron Trim Tab - Removal / Installation. All Maintenence Performed In Reference To GIIB AMM 27-04-00. No Defects Noted At This Time. Step: 12.117.1 Completed Removed aileron trim tab. Discrepancy: 12.118 CMP GIIB 270410 ELEV FREE PLAY INSP Resolution: COMPLIED WITH CMP GIIB 270410 ELEV FREE PLAY INSP. Found to be within limits and no other defects noted. All work done IAW GIIB MM 27-01-00. Labor USD: No Charge N/ C Discrepancy: 12.119 CMP GIIB 270510 Elevator Control System - Operational Test Resolution: COMPLIED WITH CMP GIIB 270510 Elevator Control System - Operational Test. All Maintenence Performed In Reference To GIIB AMM 27.01.00. Discrepancy: 12.120 CMP GIIB 272310 Elevator (Left) Resolution: COMPLIED WITH CMP GIIB 272310 Elevator (Left) lAW GIIB AMM 27.01.00. No defected noted. Labor USD: No Charge Services USD: No Charge Services: Ref. No. Descri tion Quantity 12.120 #1 Vendor Supplied Labor 1.00 N/ C 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 82 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080574 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Step: 12.120.1 Completed COMPLIED WITH Elevator (Right) removal preparation IAW CMP GIIB 272310 steps A. to B.(g). No defects noted. Step: 12.120.2 Completed COMPLIED WITH Elevator (LEFT) removal preparation by removing several access panels IAW CMP (MB 272310 No defects noted. Step: 12.120.3 Completed Complied with CMP GLIB 272310 Elevator (Left), step C. (1) through (18). All maintenance performed IAW (MB MM 27-01.00. Step: 12.120.4 Completed Complied with CMP (NIB 272310 Elevator (Left), step D. (1) through (k) and D (m) to (0). All maintenance performed IAW GIIB MM 27-01-00. Step: 12.120.5 Completed weekend nights Discrepancy: 12.121 CMP GlIB 271810 ACTUATOR, L ELEVATOR TRIM TAB Resolution: COMPLIED WITH CMP GIIB 271810 ACTUATOR, L ELEVATOR TRIM TAB Removed trim tab actuator P/N 159SCC100-21 S/N 56. Installed trim tab acutor P/N 159SCC100-21 S/N 56 IAW GIIB AMM 27-04.00. Ops checked good. Discrepancy: 12.122 CMP GlIB 272315 Elevator (Right) Resolution: COMPLIED WITH CMP GIIB 272315 Elevator (Right) IAW GlIB AMM 27-01-00. Ops checked good. Labor USD: No Charge Pans USD: No Charge Services USD: No Charge Services: Ref. No. Description Quantity 12.122 #1 Vendor Supplied Labor 1.00 N/C N/C N/C Step: 12.122.1 Completed COMPLIED WITH Elevator (Right) removal preparation IAW CMP GlIB 272315 steps A. to B.(g). No defects noted. Step: 12.122.2 Completed Complied with CMP GlIB 272315 Elevator (Right), step C. (1) through (IS). All maintenance performed IAW (MB MM 27-01.00. Step: 12.122.3 Completed Complied with CMP GlIB 272315 Elevator (Right), step D. (1) through (k) and D (m) to (o). All maintenance performed IAW (NIB MM 27-01-00. Step: 12.122.4 Completed Complied with steps D.(3),(4),(5) and (6) of CMP 272315 by reconnecting and safetying the previously removed Right Elevator Trim Tab Actuator. All work was done IAW GlIB AMM Ch.27.Ot-O0. Discrepancy: 12.123 CMP GIIB 271815 ACTUATOR, R ELEVATOR TRIM TAB Resolution: COMPLIED WITH CMP GIIB 271815 ACTUATOR, R ELEVATOR TRIM TAB- Removal / Installation. All Maintenence Performed In Reference To GIIB AMM 27-04-00. Ops checked good. Step: 12.123.1 Completed Complied with Installation step IM5) of CMP 271815 by reconnecting the previously disconnected Elevator Trim Tab Actuator. All work was done IAW GlIB AMM Ch. 27.04.00. Discrepancy: 12.124 CMP GIIB 272510 Elevator Trim Tab (Left) 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 83 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080575 Bill To: HYPERION AIR, INC. WO 4r: SC10420 Invoice Number: 7112000954 Resolution: COMPLIED WITH CMP GIIB 272510 Elevator Trim Tab (Left) Removed trim tab P/N 1159CSH2O500.1 S/N 147, with 10,804.3 TSN, 5,663 CSN. Installed "serviceable" as removed from G-II S/N 055 trim tab P/N 1159CSH20500-1 S/N 57, with 18,947.2 TSN 7,651 CSN. All work performed IAW GIIB AMM 27-04-00. Ref squawk 8.128 Labor USD: No Charge N/ C Step: 12.124.1 Step: 12.124.2 Completed Complied with CMP (MB 272510 Elevator Trim Tab (Left) steps C (1) thru C(4) IAW GIIB AMM 27.04.00. Completed Continued installation of the lilt elevator trim tab. Complied with CMP 272510 C(5) through D(11). Work done UMW GIIB MM chapter 27-04-00. Discrepancy: 12.125 CMP GIIB 272515 Elevator Trim Tab (Right) Resolution: COMPLIED WITH CMP GIIB 272515 Elevator Trim Tab (Right)-Removal / Installation. All Maintenence Performed In Reference To GIIB AMM 27-04-00. Labor USD: No Charge N/ C Step: 12.125.1 Step: 12.125.2 Completed Complied with CMP (;11B 272515 Elevator Trim Tab (RT) steps C (I) thru C(4) 1AW (NIB AMM 27-04-00. Completed Complied with CMP 272515 Elevator trim tab (Right) - removal / installation stepsD (2) through (6) installed right elevator trim tab bolts, all work in accordance with GlIB amm chapter 27-04-00. Discrepancy: 12.126 CMP GIIB 270310 Rudder Control System (SP-50G Aircraft) - Operational Test Resolution: COMPLIED WITH CMP GIIB 270310 Rudder Control System (SP-50G Aircraft) Operational Test. All Maintenence Performed In Reference To GIIB AMM 27-03-00. Discrepancy: 12.127 CMP GIIB 272810 Rudder (Aluminum) - Removal / Installation Resolution: COMPLIED WITH CMP GIIB 272810 Rudder (Aluminum) - Removal / Installation IAW GIIB AMM 27-00-00. See steps for details. 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_WorkOrderPreliminaryInvoicespt Page 84 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080576 Bill To: HYPERION AIR, INC. WO It: 5C10420 Invoice Number: 7112000954 Step: 12.127.1 Completed Complied with CMP 272810 Rudder Removal/ Installation. Step B. [21[1d thru 1d1 and C. Ill Removed requried access panels and bonding straps. Removed hinge bolt softies. Applied prentrant to all hinges. Rudder is ready to remove. All work done IAW GIIB MM 27-03-00 Step: 12.127.2 Completed Complied with CMP (MB 272810 Rudder (Aluminum) - Removal / Installation, step C. (2) through (5). All maintenance performed IAW GlIB MM 27-03-00. Right throw (22), Left throw (23). Step: 12.127.3 Completed Complied with CMP GlIB 272810 Rudder (Aluminum) - Removal / Installation, step D. (I) through (8) and D (11) to (13). All maintenance performed IAW GIIB MM 27-03-00. Step: 12.127.4 Completed Complied with step D (9),(10), (14) thru (16) of CMP 272810 Rudder (Aluminum - removal / installation. Discrepancy: 12.128 CMP GlIB 270121 Speed Brake - Operational Test (A/C Having 6 Panel Speed Brakes) Resolution: COMPLIED WITH CMP GIIB 270121 Speed Brake - Operational Test (A/C Having 6 Panel Speed Brakes)IAW GIIB AMM 27-02-00. No defects noted. Discrepancy: 12.129 CMP GIIB 275515 Flight Spoiler, Inboard (Left) Resolution: COMPLIED WITH CMP GIIB 275515 Flight Spoiler, Inboard (Left). Removed the LH inboard flight spoiler P/N 1159SCH20700-5,S/N AV119MAR02, and Installed the same LH inboard flight spoiler P/N 1159SCH20700-5, S/N AV119MAR02. Work performed IAW GlIB MM 27-02-00. Ref contingency sheet. Labor USD: No Charge N/ C Step: 12.129.1 Step: 12.129.2 Completed Complied with CMP (MB 275515 Inb Flight Spoiler Removal & Installation Step C to D. Removed 1.8i lab Flight Spoiler Pnit 1159SCH20700.5 Snit AV119MAR02 All work done JAW GIIB MM 27--02-00 Completed Cleaned and greased all hardware and attach fitting holes. Installed the LH inboard flight spoiler P/N 1159SCH20700-5, S/N AV119hIAR02 using new hardware and slip bushings from 72 month install kit. Work performed IAW (MB MM 27-02-00. Ref contingency sheet. Discrepancy: 12.130 CMP GIIB 275510 Flight Spoiler, Outboard (Left) Resolution: COMPLIED WITH CMP GIIB 275510 Flight Spoiler, Outboard (Left). Removed the LH outboard flight spoiler P/N 1159GSH20702-7, S/N AV-154 and Installed the same LH outboard flight spoiler P/N 1159GSH20702-7, S/N AV-154 lVork performed IAW GLIB MM 27-02-00. Ref contingency sheet. Labor USD. No Charge N/ C Step: 12.130.1 Step: 12.130.2 Completed Complied with CMP GIIB 275510 Ulf Out Flight Spoiler Removal & Installation Step C to D. Removed Ulf Out Flight Spoiler PO 1159GSH20702-7 Snit AV 154 All work done IAW GIIB MM 27-.02-00 Completed Cleaned and greased all hardware and attach fitting holes. Installed the LH outboard flight spoiler P/N 1159GSH20702-7, S/N AV-154 using new hardware and slip bushings from 72 month install kit. Work performed IAW GlIB MM 27-02-00. Ref contingency sheet. Discrepancy: 12.131 CMP GlIB 275525 Flight Spoiler, Inboard (Right) 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_WorkOrderPrelintinaryinvoice.qx Page 85 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080577 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Resolution: COMPLIED WITH CMP GIIB 275525 Flight Spoiler, Inboard (Right). Removed the RH inboard flight spoiler P/N 1159SCH20700-6, S/N AV-155 and Installed the same RH inboard flight spoiler P/N 1159SCH20700.6, S/N AV-155. Work performed IAW GIIB MM 27-02-00. Ref contingency sheet. Litho] USD. No Charge N/ C Step: 12.131.1 Step: 12.131.2 Completed Complied with CMP 275525 Steps B.11l thru C.lsj. Removed RH Inboard Flight Spoiler P/NI159SCH20700-6 S/N AV-155. All work done 1AW (MB MM 27.02.00. Completed Cleaned and greased all hardware and attach fitting holes. Installed the RH inboard flight spoiler P/N 1159SCH2O700.6, S/N AV-155 using new hardware and slip bushings from 72 month install kit. Work performed IAW GlIB MM 27-02-00. Ref contingency sheet. Discrepancy: 12.132 CMP GIIB 275520 Flight Spoiler, Outboard (Right) Resolution: COMPLIED WITH CMP GIIB 275520 Flight Spoiler, Outboard (Right). Removed the RH outboard flight spoiler P/N 1159SCH20702-8, S/N AV-148, and installed the same RH outboard flight spoiler P/N 1159SCH20702-8, S/N AV-148 IAW GIIB MM 27-02-00. Labor USD: No Charge N/ C Step: 12.132.1 Step: 12.132.2 Completed Complied with CMP 275520 Steps B.[1] thru C.I5J. Removed RH Outboard Flight Spoiler P/N1159SCH20702-8 S/N AV-148. All work done IAN' GIIB MM 27-02-00. Completed Installed the RH outboard flight spoiler P/N 1159SCH20702-8, S/N AV-148 IAIV GlIB MM 27-02-00. Ref contingency sheet. Discrepancy: 12.133 CMP GlIB 270011 6 PNL SPEEDBRAKE RIG CK Resolution: COMPLIED WITH CMP GIIB 270011 6 PNL SPEEDBRAKE RIG CK (GlIB) IAW GlIB AMM 27-02-00. No defects noted. Discrepancy: 12.134 CMP GlIB 275011 SPLR,GRND L (6PNL) S/BRK(GIIB) Resolution: COMPLIED WITH CMP GIIB 275011 SPLR,GRND L (6PNL) S/BRK(GIIB). Removed the LH ground spoiler P/N 1159CSH30000-5, S/N AV-414, and installed the same LH ground spoiler P/N 1159CSH30000-5, S/N AV-414 JAW GIIB MM 27-02-00. Labor USD: No Charge N/ C Step: 12.134.1 Step: 12.134.2 Completed Complied with CMP GIIB 275011 L/H Ground Spoiler Removal & Installation Step C to D. Removed L/H Ground Spoiler Pn91159CSH30000-5 Snt/AV414 All work done IAW (MB MM 27--02-00 Completed Installed the LH ground spoiler P/N 1159C'SH30000-5, S/N AV-414 IAW (NIB MM 27-02-00. Ops checks still required. Ref contingency sheet. Discrepancy: 12.135 CMP (MB 270020 CK GRD SPOILER RIGGING 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 86 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080578 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Resolution: COMPLIED WITH CMP GBH 270020 CK GRD SPOILER RIGGING JAW GLIB AMM 27-02-01. No defects noted. Discrepancy: 12.136 CMP GIIB 275166 L.GRD SPOILER IND SW ADJ Resolution: COMPLIED WITH CMP GIIB 275166 L.GRD SPOILER IND SW ADJ IAW GIIB AMM 27-02-01. No defects noted. Discrepancy: 12.137 CMP GlIB 275016 SPLR,GRND R (6PNL) S/BRK(GlIB) Resolution: COMPLIED WITH CMP GIIB 275016 SPLR,GRND R (6PNL) S/BRK(GlIB). Removed RH ground spoiler P/N 1159CSH30000-5, S/N AV-411, and installed the same RH ground spoiler P/N 1159CSH30000-5, S/N AV-411 IAW GIIB MM 27-02-00. Labor USD: No Charge N/ C Step: 12.137.1 Step: 12.137.2 Completed Complied with CMP 275016 Steps B.[Il thru C.161. Removed RH Ground Spoiler P/N1159SCH30000-5 AV-41I. All work done IAIV GlIB MM 27-02-00. Completed Installed RH ground spoiler P/N 1159CSH30000-5, S/N AV-411 IAW GIIB MM 27-02-00. Ops checks still required, ref item # 135 for ops checks. (Ref contingency sheet.) Discrepancy: 12.138 CMP GIIB 275171 R.GRD SPOILER IND SW ADJ Resolution: COMPLIED WITH CMP GIIB 275171 R.GRD SPOILER IND SW ADJ IAW GIIB AMM 27-02-01. No defects noted. Discrepancy: 12.139 CMP GlIB 274510 Flap (Left) - Removal / Installation Resolution: Complied with CMP 274510 Left Flap Removal and Installation. P/n off 1159C520005.1 S/n 151 L/FI P/N on 1159CS20005.1 S/n on 151 IJH Work done I/A/W GlIB MM chapter 27.06-00. 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 87 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080579 Bill To: HYPERION AIR, INC. Step: 12.139.1 Step: 12.139.2 Completed Completed Step: 12.139.3 Completed Step: 12.139.4 Completed WO #: SC10420 Invoice Number: 7112000954 Complied with CMP 274510 steps A through C(1), IAW GM MAI Chapter 27.06.00. Complied with CMP GlIB 274510 Flap (Left) - Removal / Installation, step C.(2) through C.(7). All maintenance performed IAW GlIB MM 27-06-00. Complied with CUP 274510 steps D (1) thru (7) Installed previously removed flap pin I159CS20005-1 s/n 151 and saftied. Work done IAW G-IIB ni/m 27-06-00. (flap still requires symetry and ops checks). ref contingency sheet. Complied with CMP 274510 items D(8) to the end. Work done I/A/W CHB MM chapter 27.06.00. Discrepancy: 12.140 CMP (MB 274710 Flap (Right) - Removal / Installation Resolution: Complied with CMP 274710 Right Flap Removal and Installation. P/n off 1159CS20005-2 S/n 151 Rai P/N on 1159CS20005.2 S/n on 151 R/H Work done I/A/W GlIB MM chapter 27-06-00. Labor USD: No Charge Step: 12.140.1 Completed Step: 12.140.2 Completed Step: 12.1403 Completed Step: 12.140.4 Completed Ni C Complied with CMP 274710 steps A through C(1), IAW GIIB MAI Chapter 27.06.00. Complied with CMP (NIB 274710 Flap (Right) - Removal / Installation, step C.(2) through C.(7). All maintenance performed IAW GlIB MM 27-06-00. Complied with CMP 274510 steps D (1) thru (7) installed previously removed flap p/n I159CS20005-2 s/n 151 and saftied. Work done IAW G-IIB n✓m 27.06.00. (flap still requires symetry and ops checks). ref contingency sheet. Complied with CMP 274710 items D(8) to the end. Work done I/A/W GlIB MM chapter 27.06.00. Discrepancy: 12.141 CMP GLIB 271010 ACTUATOR, LEFT AILERON Resolution: COMPLIED WITH CMP GIIB 271010 ACTUATOR, LEFT AILERON. Removed the LH aileron actuator P/N 1159H20029-11D3, S/N 468 and installed the LH aileron actuator P/N 1159H20029-11D3, S/N 468 IAW GIIB MM 27-02-00. Labor USD: No Charge N/ C Step: 12.141.1 Step: 12.141.2 Completed Complied with LM aileron actuator removal ,steps(C) 1-8 IAW G-IIB AMM27-02-00, P/N 1159H20029-11D3 S/N 468. Ready to be sent out for overhauL Completed Installed LH aileron actuator P/N 1159H20029-11D3, S/N 468 IAW GINS MM 27-02-00. Ref contingency sheet. Discrepancy: 12.142 CMP GIIB 271015 ACTUATOR, RIGHT AILERON Resolution: COMPLIED WITH CMP GIIB 271015 ACTUATOR, RIGHT AILERON. Removed and installed R/H aileron actuator PN. 1159SCH2522E SN. 224GT as required IAW GIIB MM 27.02.00. Labor USD: No Charge N/ C Step: 12.142.1 Step: 12.142.2 Completed Complied with R/H aileron actuator removal ,steps(C) 6-8 IAW G-IIB ANIM27-02-00, P/N 1159SCH2522E S/N 224GT. Completed Installed R/H aileron actuator PN. 1159SCH2522E SN. 224GT as required IAW (MB CMP 271010 D4 -D 10 and GlIB MM 27-02-00. Requires operational and leak checks. Discrepancy: 12.143 CMP GlIB 271315 ACTUATOR, RUDDER TRIM Resolution: COMPLIED WITH CMP GIIB 271315 ACTUATOR, RUDDER TRIM IAW GIIB AMM 27-04-00. No defected 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_WorkOrderPrelintinaryInvoicespt Page 88 of 98 Printed: 3/23/2012 4:28:32P) Flet X EFTA01080580 Bill To: HYPERION AIR, INC. Labor USD: No Charge Step: 12.143.1 WON: SC10420 Invoice Number: 7112000954 N/ C Completed Complied with CMP 271315 steps C4, D2 and C7, to compliy with rudder trim tab actuator inspection (see Item 12.40). Rudder trim tab actuator cables need to be tensioned. Cables are flagged. All work performed I.A.W. (MB M.M. 27.04.00. Ops checked NO GOOD. Sticks in full left and full right travels. See Squawk 8.90 Discrepancy: 12.144 CMP GlIB 271510 ACTUATOR, AILERON TRIM TAB Resolution: COMPLIED WITH CMP GIIB 271510 ACTUATOR, AILERON TRIM TAB. Removed the aileron trim tab actuator P/N 1159SCC201-3, S/N 279 and installed the same aileron trim tab actuator P/N 1159SCC201-3, S/N 279. Work performed IAW GIIB MM 27-04-00. Discrepancy: 12.145 CMP GIIB 270316 Wing Flap / Stabilizer - Operational Test (GIIB) Resolution: Complied with CMP 270316 Wing Flap Stabilizer Operational Test. Work done I/A/W GIIB MM chapter 27-06-01. Discrepancy: 12.146 CMP GlIB 274811 ACTUATOR,L GRND SPOILER (GIIB) Resolution: Complied with CMP GlIB 274811 ACTUATOR,L GRND SPOILER (GIIB) removal and installation as required IAW GIIB MM 27-02-00.Removed PN. 1159SCH305-11 SN. 0105 and installed same unit PN. 1159SCH305.11 SN. 0105. Ref contingency sheet. Labor USD: No Charge N/ C Step: 12.146.1 Step: 12.146.2 Completed COMPLIED WITH Removal of ACTUATOR, Lilt GRND SPOILER P/N I 159SCH305-11 S/N 0105 IAW CMP GIIB 274816 steps A. to C.(10). Completed Installed same ground spoiler actuator as removed previously PN. I159SCH305.l I SN. 0105 IAW (MB CMP 274811 and MM 27-02-00. Ground spoiler rigging check shall be accomplished under squawk 12.135 of this Work Order CMP 270020. Servicing and bleed of hydraulic reservoir to be complied with under squawk 12.179 ,CMP 290110. Discrepancy: 12.147 CMP (MB 274816 ACTUATOR,R GRND SPOILER (GIIB) Resolution: Complied with CMP GIIB 274816 ACTUATOR,R GRND SPOILER (GIIB) IAW GIIB MM 27-02-00. Ref contingency sheet. 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_WorkOrderPreliminaryInvoicespt Page 89 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080581 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Step: 12.147.1 Step: 12.147.2 Completed COMPLIED WITH Removal of ACTUATOR,R GRND SPOILER P/N I159SCH305-11 S/N 0130GT IAW CMP GIIB 274816 steps A. to C.(10). Completed Installed R/H ground spoiler actuator PN. 1159SCH305-11 SN. 0130GT IAW (MB CMP 274811 and (MB MM 27-02-00. Ground spoiler rigging check will be C/W under squawk 12.135 and reservoir service under squawk 12.179. Ref contingency sheet. Discrepancy: 12.148 CMP GIIB 275310 ACTUATOR, L FLT SPOILER Resolution: COMPLIED WITH CMP GIIB 275310 ACTUATOR, L FLT SPOILER. Removed LH flight spoiler actuator P/N 1159SCH250-3 S/N 3626T. Installed a Modified LH flight spoiler actuator P/N 1159SCH250-29, S/N 2002. Work performed IAW GIIB MM 27-02-00. Ref contingency sheet. Labor USD: No Charge N/ C Step: 12.148.1 Step: 12.148.2 Completed COMPLIED WITH Removal of ACTUATOR, L FLT SPOILER P/N 1159SCH250-3 S/N 362GT JAW CMP (MB 275310 steps C.(I) to C.(5). Completed Installed a Modified LH flight spoiler actuator P/N 1159SCH250-29, S/N 2002. Work performed IAW GIIB MM 27.02-00. Ref contingency sheet. Discrepancy: 12.149 CMP GIIB 275320 Outboard Flight Spoiler Bellcrank Assembly (Left) - Removal / Installation Resolution: COMPLIED WITH CMP GIIB 275320 Outboard Flight Spoiler Bellcrank Assembly (Left) - Removal / Installation. Removed the LH outboard flight spoiler bellcrank assembly P/N 1159CM20209-5, NSN. Installed a Repaired LH outboard flight spoiler bellcrank assembly P/N 1159CM20209-5, NSN IAW GDR MM 27-02-00. Labor USD: No Charge N/ C Step: 12.149.1 Step: 12.149.2 Completed Complied with CMP GIIB 275320 Outboard Flight Spoiler Bellcrank Assembly (Left) - Removal / Installation- Steps C.- (I) thrg C.- (6) - removed (Left) Outboard Flight Spoiler Bellcrank Assembly P/N:1159CM20209-5 (recorded from CMP) S/N: n/a. work done IAW (MB AMM 27-02-00. Completed Installed a Repaired LH outboard flight spoiler bellcrank assembly P/N 1159CM20209.5, NSN IAW GIIB MM 27-02-00. Discrepancy: 12.150 CMP GIIB 275321 Inboard Flight Spoiler Bellcrank Assembly (Left) - Removal / Installation Resolution: COMPLIED WITH CMP GIIB 275321 Inboard Flight Spoiler Bellcrank Assembly (Left) - Removal / Installation. Removed the LH inboard flight spoiler bellcrank assembly P/N 11595B30144-11, NSN. Installed a Repaired LH inboard flight spoiler bellcrank assembly P/N 11595B30144-11, NSN IAW GIIB MM 27-02-00. Labor USD: No Charge N/ C Step: 12.150.1 Step: 12.150.2 Completed Complied with CMP (MB 275321 Intboard Flight Spoiler Bellcrank Assembly (Left) - Removal / Installation- Steps C.- (I) thrg C.- (7) - Removed (Left) Intboard Flight Spoiler Bellcrank Assembly WN:1159SB30144-II (recorded from CMP) S/N: n/a. work done IAW GIIB AMM 27-02-00. Completed Installed a Repaired LH inboard flight spoiler bellcrank assembly P/N 1159SB30144-11, NSN IAW GIIB MM 27-02-00. Ref contingency sheet. Discrepancy: 12.151 CMP (NIB 275315 ACTUATOR, R FLT SPOILER 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 90 of. 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080582 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Resolution: COMPLIED WITH CMP GIIB 275315 ACTUATOR, R FLT SPOILER. Removed R/H flight spoiler actuator P/N 1159SCH250-4D, S/N 294GT. Installed a Modified RH flight spoiler actuator P/N 1159SCH250-30, S/N 1731. Work performed IAW GIIB MNI 27-02-00. Labor USD: No Charge N/ C Step: 12.151.1 Step: 12.151.2 Completed Removed R/H flight spoiler actuator. Work done I/AAV GIIB MM chapter 27-02-00. Complied with CMP 275315 C(I) through (5). Completed Installed a Modified RH flight spoiler actuator P/N 11595C11250-30, S/N 1731. Work performed IAW GIIB MM 27.02-00. Ref contingency sheet. Discrepancy: 12.152 CMP GlIB 275322 Inboard Flight Spoiler Bellcrank Assembly (Right) - Removal / Installation Resolution: Installed the new R/H inbd flight spoiler bellcrank pushrod P/N 1159C20262-3 to the R/H Inbd flight spoiler bellcrank ref. GIIB CMP 275322 and the (MB AMM 27-02-00. Removed P/N 1159a0262-3 S/N NSN. Installed the repaired R/H inbd flight spoiler bellcrank P/N 1159CNI20208-2 NSN ref. GIIB CMP 275322 and the GlIB AMM 27.02.00. Removed P/N 1159CM20208.2 S/N NSN. Refer to items 12.51, 12.114 and 12.128 for final attachments and checks. Labor USD: No Charge N/ C Step: 12.152.1 Completed Complied with CMP GM 275322 Intboard Flight Spoiler Bellcrank Assembly (Right) - Removal / Installation- Steps C.- (I) thrg C.- (7) - Removed (Right) Intboard Flight Spoiler Bellcrank Assembly P/N:11590020208-2 (recorded from CMP) S/N: n/a. work done IAW (MB AMM 27-02-00. Discrepancy: 12.153 CMP GlIB 275323 Outboard Flight Spoiler Bellcrank Assembly (Right) - Removal / Installation Resolution: Installed the repaired R/H outbd flight spoiler bellcrank P/N 1159CM20209.6 NSN ref. GIIB CMP 275323 and the GlIB AMM 27.02.00. Removed P/N 1159CNI20209-6 S/N NSN. Refer to items 12.132, 12.131, 12.114 and 12.128 for final attachment and checks. Labor USD: No Charge N/ C Step: 12.153.1 Completed Complied with CMP GIIB 275323 Outboard Flight Spoiler Bellcrank Assembly (Right) - Removal / Installation- Steps C.- (I) thrg C.- (6) - removed (Right) Outboard Flight Spoiler Bellcrank Assembly P/N:11590020209-6 (recorded from CMP) S/N: n/a. work done IAW GIIB AMM 27-02-00. Discrepancy: 12.154 CMP GlIB 351511 Oxygen Cylinder (No.2) Resolution: COMPLIED WITH CMP GIIB 351511 Oxygen Cylinder (No. 2) - Removal / Installation. Removed #2 oxygen bottle P/N 176521-64, S/N 881993 and sent out for Hydro inspection. Installed inspected 02 bottle P/N 176521.64, S/N 881993 IAW G IlB AMM 35-00.00. 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 91 of. 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080583 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Step: 12.154.1 Step: 12.154.2 Completed Complied with section (A), (B) removed #2 oxygen bottle from aircraft P/N 176521.64, S/N 881993 and sent to vendor for new hydro IAW G JIB AMM 35-00.00. Completed Complied with section (C) (1) through (D)(6) reinstalled #2 oxygen bottle from aircraft P/N 176521-64, S/N 881993 IAW G JIB AMM 35-00-00. Discrepancy: 12.155 CMP GLIB 351010 Oxygen System (Pilot) - Operational Test Resolution: COMPLIED WITH CMP GIIB 351010 Oxygen System (Pilot) - Operational Test IAW GII-B AMM 35-00-00. No defects noted. Discrepancy: 12.156 CMP GIIB 351015 Oxygen System (Copilot) - Operational Test Resolution: COMPLIED WITH CMP GIIB 351015 Oxygen System (Copilot) - Operational Test IAW GII-B AMM 35-00-00. No defects noted. Discrepancy: 12.157 CMP GIIB 351016 Passenger Oxygen System - Operational Test (Gulfstream Installed System) Resolution: Billing Method Flours Rate Total Pans USD: Time and Material $87.00 Total USD: S87.00 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 12.157 #1 MS22012-6 PACKING RING 10 $8.70 $87.00 Discrepancy: 12.158 CMP GIIB 351512 Oxygen Cylinder (No.3) Resolution: COMPLIED WITH CMP GIIB 351512 Oxygen Cylinder (No. 3) - Removal / Installation. Removed #3 oxygen bottle from aircraft P/N 176521-49, S/N 642653 and sent out for Hydro inspection. Installed inspected O2 bottle P/N 176521-49, S/N 642653 IAW G IIB AMM 35.00.00. Labor USD: No Charge N/ C Step: 12.158.1 Step: 12.158.2 Completed Complied with section (A), (B) removed #3 oxygen bottle nom aircraft P/N 17652149, S/N 642653 and sent to vendor for new hydro JAW G IIB AMM 35-00.00. Completed Complied with section (C) (1) through (D)(6) reinstalled #3 oxygen bottle front aircraft P/N 176521-49, S/N 642653 JAW G IIB AMM 35.00.00. Discrepancy: 12.159 CMP (MB 351205 BOTTLE, NO 1 PORTABLE OXYGEN 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 92 of 98 Printed: 3/23/2012 4:28:32P) Ftst X EFTA01080584 Bill To: HYPERION AIR, INC. WON: SC10420 Invoice Number: 7112000954 Resolution: Complied with section (A), removed portable oxygen bottle from aircraft P/N 900-002-035-01, S/N 33925R and sent to vendor for new hydro IAW G IIB AMM 35-00.00. Received portable oxygen bottle from vendor P/N 900-002-035-01, S/N 33925R see item 12.58 for details; and replaced portable oxygen bottle in aircraft IAW G-II B AMM 35.00.00. Step: 12.159.1 Completed Complied with section (A), removed portable oxygen bottle from aircraft P/N 900-002-035-01, S/N 33925R and sent to vendor for new hydro IAW G IIB AMM 35.00.00. Discrepancy: 12.160 CMP GLIB 242520 Inverter, E Instrument Resolution: COMPLIED WITH CMP GIIB 242520 Inverter, E Instrument. Re-moved Inverter E. P/N PC-17A1 S/N 2794. Re-installed Inverter E. P/N PC-17A1 S/N 2794.All work was done IAW Gulfstream GIIB AMM 24.25.20. No defects noted. Discrepancy: 12.161 CMP GlIB 242710 Inverter, B Standby Resolution: COMPLIED WITH CMP GIIB 242710 Inverter, B Standby. Removed Inverter B. P/N 501.1128.01 S/N 1160. Re-installed Inverter B. P/N 501-1128.01 S/N 1160. All work was done JAW Gulfstream GlIB AMM 24-27-10. No defects noted. Discrepancy: 12.162 CMP GlIB 242720 Rectifier, Inverter B Transformer Resolution: COMPLIED WITH CMP GIIB 242720 Rectifier, Inverter B Transformer. Removed Inverter Rectifier Transformer B. P/N 28VS200Y-17 S/N310. Re-installed Inverter Rectifier Transformer B. P/N 28VS200Y-17 S/N310. All work was done IAW Gulfstream GIIB AMM 24-27-20. No defects noted. Discrepancy: 12.163 CMP GIIB 246015 B Inverter - Frequency / Voltage Check Resolution: COMPLIED WITH CMP GIIB 246015 B Inverter - Frequency / Voltage Check with no discrepancies noted at this time. All work performed JAW G-IIB maintenance manual 24.03.00. 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_WoikOrderPreliminarylnvoice.rpt Page 93 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080585 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 12.164 CMP GLIB 246025 E Inverter - Frequency / Voltage Check Resolution: COMPLIED WITH CMP GIIB 246025 E Inverter - Frequency / Voltage Check with no discrepancies noted at this time. All work performed lAW G-IIB maintenance manual 24.03.00. Labor USD: No Charge N/ C Discrepancy: 12.165 CMP GIIB 280110 AIRCRAFT DEFUELING Resolution: Defueled 6400 lbs. Drained fuel from sumps. All work done IAW 28.00.00. Labor USD: No Charge N/ C Discrepancy: 12.166 CMP GIIB 280210 BLEED FUEL SYSTEM Resolution: COMPLIED WITH CMP GIIB 280210 BLEED FUEL SYSTEM IAW GIIB AMM 28.04.00. No defects noted. Step: 12.166.1 Completed Refueled aircraft with 6400 lbs of fuel. Work done UMW GlIB MM chapter 28-04-00. Discrepancy: 12.167 CMP (MB 284511 No. 1 Left Fuel Quantity Probe - Removal / Installation Resolution: N/A Removal was not required. Discrepancy: 12.168 CMP GlIB 284636 No. 13 Left Fuel Quantity Probe - Removal / Installation Resolution: N/A Removal was not required. Discrepancy: 12.169 CMP GIIB 281111 L FUEL PROBE INSUL/CAP CK(GIIB Resolution: No Action Required At This Time Due To Maintenence Performed, Fuel Probes Were Never Disconected. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WoikOrderPreliminarylnvoicespt Page 94 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080586 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 12.170 CMP GIIB 289080 SCREEN ASSY,LM FUEL P/U (GIIB) Resolution: COMPLIED WITH CMP GIIB 289080 SCREEN ASSY,LM FUEL P/U (GIIB) Removed fuel pickup P/N 1159P20142-1 NSN. Installed same fuel pickup P/N 1159P20142-1 NSN JAW GIIB AMM 28.00-00 Labor USD: No Charge N/ C Step: 12.170.1 Completed Complied with CMP GIIB 289080 SCREEN ASSY,LM FUEL P/U (GDR i Steps Al thru A(3). Discrepancy: 12.171 CMP GlIB 289085 SCREEN ASSY,LA FUEL P/U (GIIB) Resolution: COMPLIED WITH CMP GIIB 289085 SCREEN ASSY,LA FUEL P/U (GIIB) Removed fuel pickup PIN 11591'20142-3 NSN. Installed same fuel pickup P/N 1159P20142-3 NSN IAW GIIB AMM 28-00-00. Labor USD: No Charge N/ C Step: 12.171.1 Completed Complied with CMP GIIB 289085 SCREEN ASSY,LA FUEL P/U (GIIB) Steps A(1) thru A(3). Discrepancy: 12.172 CMP GIIB 575048 Lower Wing Planks BL 0 to BL 19 (Left) - X-ray / NDT Inspection Resolution: COMPLIED WITH CMP GIIB 575048 Lower Wing Planks BL 0 to BL 19 (Left) - X-ray / NDT Inspection IAW GIIB 57-00-00. Work performed by Structual testing Systems Cert. It ESIR124K.See item 8.122 for discrepency noted. Labor USD: No Charge N/ C Step: 12.172.1 Completed Removed Fuel panels 21-FT LWR-1, 21-FT LWR-2, 21-Fr LWR-3, 21-Fr L1VR-4, 22-FT LWR-1, 22FT LWR-2. 22-Fr LWR-3, 22-Fr LWR-4, 22-Fr UPR-12, 22-FT UPR-13, 22-FT UPR-I5, 22 FT UPR-17. Done I.A.W. (MB 57.00-00. Discrepancy: 12.173 CMP GlIB 285011 No. 1 Right Fuel Quantity Probe - Removal / Installation Resolution: N/A Removal was not required. Discrepancy: 12.174 CMP GIIB 285136 No. 13 Right Fuel Quantity Probe - Removal / Installation Resolution: N/A Removal was not required. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryinvoicespt Page 95 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080587 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 12.175 CMP GlIB 281116 R FUEL PROBE INSUUCAP CK(GIIB Resolution: No Action Required At This Time Due To Maintenence Performed, Fuel Probes Were Never Disconnected. Discrepancy: 12.176 CMP GIIB 289090 SCREEN ASSY,RM FUEL P/U (GIIB) Resolution: Complied With CMP GIIB 289090 Screen Assembly, Removal / Installation. No Defects Noted At This Time. All Maintenence Performed In Reference To GlIB AMM 28.00.00. Step: 12.176.1 Completed Complied with CMP GIIB 289090 SCREEN ASSY,RM FUEL P/U ((MB) Steps A(1) thru A(3). Discrepancy: 12.177 CMP GlIB 289095 SCREEN ASSY,RA FUEL P/U (GIIB) Resolution: Complied With CMP GIIB 289095 Screen Assembly. Removal / Installation. No Defects Noted At This Time. All Maintenence Performed In Reference To GlIB AMM 28-00.00. Discrepancy: 12.178 CMP GIIB 575053 Lower Wing Planks BL 0 to BL 19 (Right) - X-ray / NDT Inspection Resolution: COMPLIED WITH CMP GIIB 575053 Lower Wing Planks BL 0 to BL 19 (Right) - X-ray / NDT Inspection IAW GlIB 57-00-00. Work performed by Structual Testing Systems Cert. # ES1R124K.See item 8.122 for discrepency noted.. Billing Method Hours Rate Total Labor USD: No Charge N/ C Services USD: Time and Material $14,545.27 Total USD: $14,545.27 Services: Ref. No. Description Quantity Sell Price USD Extended USD 12.178 #1 SERVICE 1.00 $14,545.27 $14,545.27 Step: 12.178.1 Completed Removed Fuel panels 21-FT LWR-1, 21-Fr LWR-2, 2I-Fr LWR-3, 21-Fr LWR-4, 22-Fr LWR-1, 22FT LWR-2. 22-Fr LWR-3, 22-Fr LWR-4, 22-FT UPR-12, 22-Fr UPR-13, 22-FT UPR-15, 22 FT UPR-17. Done I.A.W. GlIB 57.00.00. Discrepancy: 12.179 CMP GM 290110 SRVC HYD SYS RESERVOIR 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 96 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080588 Bill To: HYPERION AIR, INC. WON: SC10420 Invoice Number: 7112000954 Resolution: Complied with CMP 290110 Hydraulic System Reservoir Filling Procedure. Work done I/A/W GIIB MM chapter 29.01-00. Discrepancy: 12.180 CMP GIIB 803027 Engine Starter Splines (Right) - Lubrication / Inspection Resolution: COMPLIED WITH CMP GIIB 803027 Engine Starter Splines (Right) - Lubrication / Inspection with satisfactory results IAN 62-B AMM 80-01.00. Labor USD: No Charge N/ C Discrepancy: 12.181 CMP GIIB 803028 Engine Starter Assembly (Right) - Removal / Installation Resolution: COMPLIED WITH CMP GIIB 803028 Engine Starter Assembly (Left) - Removal / Installation. Removed Right Engine Starter Assy P/N 383700.1-1 S/N P-364 for spline lubrication and inspection and re-installed StarterP/N 383700.1-1 S/N P-364 IAW G-2B AMM 80-01-00 with no defects noted. Labor USD: No Charge N/ C Step: 12.181.1 Completed COMPLIED WITH CMP GIIB 803028 Engine Starter Assembly (Right) - Removal / Installation Steps A. to C(10). Awaiting for Starter duct corrujoint seal. Discrepancy: 12.182 Nine rivnuts need replaced on R/H wing wedge panel. Required drilling of screws due to rivnut spinning. Resolution: Entered in error. Discrepancy: 12.183 Upper and lower bearings on LAI aileron bellcrank are chiped. Resolution: Written in error. Duplicate squawk ,refer to squawk 8.28 for corrective action. 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 97 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080589 Bill To: HYPERION AIR, INC. WO It: SCI0420 Invoice Number: 7112000954 Communications concerning 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_WorkOrderPreliminaryInvoicespt Page 98 of 98 Printed: 3/23/2012 4:28:32Pli Rd X EFTA01080590