EFTA Document EFTA01734227

Gulfstrearn° Ail DYNAMICS C.CINIIMNY Bldg C.-FAX 561-681-9392 • West Palm Beach. Ronda 33406 PRELIMINARY INVOICE Part/Model #: CHB AC Serial No./fail No.: 151 I N9093E Mail Remittance To: Gulfstream Aerospace Corporation P.O. Box 730349 Dallas, Texas 75373-0349 Overnight Remittance To: Gulfstream Aerospace Corporation (Box # 730149) do JP Morgan Chase Bank. NA ATTN: Dallas National Wholesale Lockbox TX1.0029 14800 Frye Road Ft. Worth. TX 76155 Wire Remittance To: Gulfstream Aerospace Corporation JP Morgan Chase Bank. NA Chicago. IL 60670 Account No. 10-15825 Fcdwirc Routing No. (ABA) 021 000021 ACH Credit Routing No. (ABA1071 000 013 IIIII.1111.11.1111.111111I 11.111 Bill To: HYPERION AIR, INC. 3800 SOUTHERN BLVD SUITE 204 WEST PALM BEACH, Florida 33406 United States Title: HYPERION AIR, INC. Invoice Number: Invoice Date: Customer ID: P.O. Number: Repair Station: In Date: Out Date: Payment Type: Payment Terms: 7112000954 3/15/2012 CH200 FAA CRS 11002624N 02/06/2012 03/23/2012 Net 30-Open terms INVOICE SUMMARY FOR WORK ORDER NUMBER: SC10420 Time & 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 $0.00 $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 otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoiee.rpt Page I of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012031 EFTA01734227 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112000954 Item: 1 Airframe Gulfstream CHB Scheduled N909JE Team Manager: Sean Brown Customer Coordinator: Ray Kra her Part/Model GlIft AC Serial NoiTail No.: 151 / N909JE TSWTS0: CSN/CSO: 5663 Aircraft Time: 10804.3 Discrepancy: 1.1 Return to Service FAR 91.409 (013) Inspection Resolution: ACTT: 10,8043 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 91.409 003) 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-PB1 1500-C Perimeter Road West Palm Beach, FL 33406 FAA CRS PB8R624N Step: 1.1.1 Step: 1.1.2 Waiting A/C Times and Cycles approval (L) Waiting A/C Warranty 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 Step: 1.2.2 Completed Inbound/Preliminary Inspection Waiting Outbound Inspection approval IL) Discrepancy: 13 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 arc in US Dollars (USD). GAC_Work0nlerPreliminaryInvoice.rpt Page 2 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012032 EFTA01734228 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 toolrooni. Pans USD: No Charge N/ C Pans: Ref. No. Part number: Description Quantity 1.511 740031 Wing wedge templete Left Discrepancy: 1.6 Cover & Protect Resolution: Cover & Protected as required. Labor USD: No Charge N/ C Discrepancy: 1.7 Service Chemical Toilet/Clean Galley Resolution: N/A Discrepancy: 1.8 Arrival/Departure 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_WorkOrderPreliminaryInvoiee.rpt Page 3 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012033 EFTA01734229 Bill To: HYPERION AIR, INC. WO SC10420 Invoice Number 7112000954 Discrepancy: 1.10 Resolution: N/A Remove Valuables & Secure. 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 arc in US Dollars (USD). GAC_Work0rderPreliminaryInvoiee.rpt Page 4 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012034 EFTA01734230 Bill To: HYPERION AIR, INC. WO 0: SC10420 Invoice Number: 7112000954 Discrepancy: 1.15 Resolution: N/A IlazMat - 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 he 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 Parts 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 arc in US Dollars (USD). GAC_Work0rderPreliminaryinvoiee.rpt Page 5 of 98 Printed: 3/23/2012 4:28:32P? Rd:! EFTA_R1_00012035 EFTA01734231 Bill To: HYPERION AIR, INC. WO 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 8. 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 arc in US Dollars (USD). GAC_Work0nterPreliminaryInvoice.rpt Page 6 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012036 EFTA01734232 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 AM! 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. * It after QC review, weight change is greater than 2 pounds or .05% of MAC, the weight and balance report will require I-I:computation. 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 API;; 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 N: AC Serial No./Tail No.: TSWTS0: 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_Work0nlerPreliminaryInvoiee.rpt Page 7 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012037 EFTA01734233 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 Resolution: An entryway light inop. Item: 8 Mechanical Team Manager: Sean Brown Customer Coordinator: Ray Kraber Pan/Model ft: AC Serial No.fTail No.: TSN/TS0: CSN/CS0: Aircraft Time: Discrepancy: 8.1 Extra time for removing BUL-1 & BUI.-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. IAW CHB AMM 27-00-00 and 20-00-00. Billing Method Hours Rate Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $300.32 Total USD: $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 arc in US Dollars (USD). GAC_Work0rderPreliminaryInvoiee.rpt Page 8 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012038 EFTA01734234 Bill To: HYPERION AIR, INC. Pans: WO #: SC10420 Invoice Number 7112000954 Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.2 #1 NASI203-3 BOLT 100 $0.26 $26.00 8.2 #2 NASI203-5 BOLT SO $0.26 $13.00 8.2 #3 GASSS0E3S9 SCREW 10 $4.12 $41.20 8.2 #4 GAS550E3S10 SCREW 4 $1.81 $7.24 8.2 #5 NAS583-1I BOLT 4 $24.66 $98.64 8.2 #6 NAS583-13 BOLT 2 $15.68 $31.36 8.2 #7 NAS583-14 BOLT 2 $23.77 $47.54 8.2 #8 NAS583-I 6 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 M525083-2BB13 and replaced with new bonding wire P/N MS25083-2BB13 lAW GI1B ANEW 20-00-00. Billing Method Flouts Rate Total Labor USD: Flat Rate $230.00 Parts USD: Time and Material $10.30 Total USD: $240.30 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.3 #1 M525083-2BBI3 JUMPER-ELEC BONDING,13 IN 1 $10.30 S10.30 Discrepancy: 8.4 While complying with CMP#'s 575030/575025 , Wing to fuselage interior Left/Right 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: 1159821241-73 Qty: 1 P/N: 1159521241-81 Qty: 1 P/N: 1159B21241-35 Qty: 1 Resolution: Removed and discarded corroded screws and installed new screws.P/N: MS24694550 : Qty: 330 P/N: 1159B21241-71 Qty: I P/N: 1159821241-78 Qty: 1 P/N: 1159B21241-33 Qty: I P/N: 1159B21241-73 Qty: P/N: 1159B21241-81 Qty: I P/N: 1159B21241-35 Qty: 1 All work done i/a/w G-11 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 arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoice.rpt Page 9 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012039 EFTA01734235 Bill To: HYPERION AIR, INC. WO I: SC10420 Invoice Number: 7112000954 Labor USD: Parts USD: Total USD: Pans: Ref. No. 8.401 Billing Method Flat Rate Time and Material Pan number: MS24694-S50 Hours Description SCREW-MACHINE.FLAT CSK HEAD Rate Total $460.00 $78.00 $538.00 Quantity Sell price USD 300 $0.26 Extended USD $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 0 rings under mount screw heads. All work performed JAW CHB AMM 28-02-00. Labor USD: Labor USD: Parts USD: Total USD: Pans: Ref. No. 8.501 8.5 03 8504 Step: 8.5.1 Step: 8.5.2 Step: 8.5.3 Billing Method Time and Material Time and Material Time and Material Pan number: 1159SCP006-1 HT183-3-2 GAS13AF6 Completed Completed Completed Hours Rate ST 15.88 @ $115.00 OT 0.13 @ $173.00 Description PUMP SCREW 0 -RING Total $1,826.20 $22.49 $2,557.27 $4,405.96 Quantity Sell price USD 1 $1.925.35 3 $197.76 3 $12.88 Extended USD Remove float valve mid point on right wing P/N159SC-P-006 S/N 1010. Work IAW CHB MM 28-02-00 Positioned new float valve in place, P/N 1159SCP006.1, S/N 4771, and tightened mounting screws. Moat valve will have to be removed in order to install 3 o-rings that are to he placed under mounting screws. Refer to Gulfstream lilt 1PC 28.10.00 figure 6, sheet I, item 3.O-rings are on order. Install 3 o rings under float valve mounting screw heads IAN' CHB AMM 28-01-01. $1,925.35 $593.28 $38.64 Discrepancy: 8.6 Nine rivnuts need replaced on Rill wing wedge panel. Required drilling of screws due to rivnuts spinning. Resolution: Removed and replaced nine rivnuts on the R/H 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: Parts USD: Total USD: Pans: Ref. No. 8.6 01 Billing Method Time and Material Time and Material Time and Material Pan number: ST OT I lours Rate 13.44 @ $115.00 435 @ $173.00 Total $1,545.60 $752.55 $273.47 $2,571.62 Description Quantity Sell price USD Extended USD GAN51283-166 BLIND NUT 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 arc in US Dollars (USD). GAC_WorkOrderPrcliminaryInvoiec.rpt Page 10 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012040 EFTA01734236 Bill To: HYPERION AIR, INC. Parts: WO #: SC10420 Invoice Number: 7112000954 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 Completed 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 Removed access cover 22,SR-2 on outboard side of sponson Removed all spinning and bad rivnuts on the Rill wing wedge panel IAW 6-IIB AMM 51-40-00. Discrepancy: 8.7 Left wing flap tracts A,B,C, and D have corrosion on roller hearing 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. 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 LAW 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, LAW. GAME'S 4000. Labor USD: Pans USD: Total USD: Pans: Ref. No. 8.7 #1 Step: 8.7.1 Step: 8.7.2 Step: 8.73 Step: 8.7A Billing Method Hours Rate Total Flat Rate $6,900.00 Time and Material Part number: PRIMO-B-I/2 Completed Completed Completed Completed $153.12 $7,053.12 Description Quantity Sell price USD SEALANT, PRC,CARTRIDGE 4 $38.28 Extended USD Removed corrosion from flap track beating surfaces on tracks A.B.0 and D IAW GI1B 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 JAW Gulftream drawing SEU5811901. 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. LAN'. (;AMPS 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 GIIB CPCM 20-5041.Nleasured tracks A,B,C and D for thickness as required IAW Gulftream drawing SF,05811901, with no defects noted. Performed brush cadmium plating repair to all exposed surfaces of flap tracks A,B,C and D IAW Gulftream drawing SE05811901.Nlasked ott flaps tracks A B C and D. washed with solvent and primed with 2012 primer, and applied topcoat LAW CAC CAMPS 4000. Billing Method Gouts 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. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoiee.rpt Page I I of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012041 EFTA01734237 Bill To: HYPERION AIR, INC. WO A: SC10420 Invoice Number 7112000954 Step: 8.8.1 Step: 8.8.2 Step: 8.83 Step: 8.8.4 Step: 8.8.5 Completed Completed Completed Completed Removed corrosion from flap track bearing surfaces on tracks A,B,C and D IAW GDR 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.0 and D Gulftream drawing SEOS811901. 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. GAMPS 4000.1 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 primed with 2012 primer ready to spray paint. Discrepancy: 8,9 Jill wing wedge has 18 drilled off screw heads because rivnuts were spining. Resolution: Removed and replaced eighteen rivnuts on the IAI wing wedge panel. Installed new rivnuts P/N GANS12B3.166 wet with sealant. Had to gain acess to fuel tank area to remove drilled out rivnuts All work done TAW G-1111 SRM 51-41-00. Labor USD: Parts USD: Total USD: Parts: Billing Method Flat Rate Time and Material $117.00 Hours Rate Total $2,300.00 $2,417.00 Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.911 GABSI IGA3-7 HI-BOLT 1 $2.06 $2.06 8.9/2 PR1422-B-2 SEALANT, PRC, CARTRIDGE 1 $38.47 $38.47 8.9 /3 GAN512B3-166 BLIND NUT 25 $1.52 $38.00 8.9 14 PR1422-B-2 SEALANT, PRC, CARTRIDGE 1 $38.47 $38.47 Step: 8.9.1 Completed Removed all spinning and bad limits on IA1 wing wedge IAW G-IIB AMM 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 Labor USD: Flat Rate Total USD: flours Rate Total $460.00 $460.00 Discrepancy: 8.11 Rill elevator, top, inbd, hinge cover attach screw hole, heli-coil is bad. Resolution: Replaced bad RBI elevator, top. inbd, hinge cover attach screw hole, heli-coil with a new one IAW GAMPS 2212. 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_WorkOnlerPrcliminaryInvoice.rpt Page 12 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012042 EFTA01734238 Bill To: HYPE:RION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Total USD: $460.00 Discrepancy: 8.12 IJH elevator No.3 hinge, attach boll bore is corroded. Resolution: Removed corrosion as required and remeasured 1/11 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 rota' Labor USD: Flat Rate $460.00 Total USD: $460.00 Discrepancy: 8.13 It/II 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 lop coat as required JAW GIV 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. IAW. SRM.51.13.20. Discrepancy: 8.14 R/H wing upper sponson plate is corroded. Resolution: Mechanically removed corrosion from edges of the RAJ upper sponson plate, Strip heavy paint for a better look IAW. GAC. SFA5802903. Removed all old sealant from around sponson plate. Treated and primed all bare metal. Resealed sponson plate. All work done JAW Standard Repair/Corrosion of Sponson Plates DWG No. SF45802903 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 @ 5115.00 $2,029.75 Labor USD: Time and Material OT 4.33 @ 5173.00 $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_WorkOnlerPreliminaryInvoicc.rpt Page 13 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012043 EFTA01734239 Bill To: HYPF:RION AIR, INC. Services: Ref. No. Description WO 8: SC10420 Invoice Number 7112000954 8.14 111 Step: 8.14.1 Step: 8.14.2 Step: 8.14.3 Quantity Sell Price USD Extended USD SERVICE 1.00 $400.00 $400.00 Completed Completed Completed Mechanically removed corrosion from edges of the Rai upper sponson plate. Strip heavy paint for a better look JAW. GAC. SE45802903. Removed all old sealant front around sponson plate. Treated and primed all bare metal. Resealed sponson plate. All work done LAW Standard Repair/Corrosion of Sponson Plates DWG No. 5E45802903 REV.I) Performed cadmium plating repair on IUD upper sponson plate. All work done IAW Standard Repair/Corrosion of Sponson Plates DWG No. SE45802903 REV.D Discrepancy: 8.15 WEI wing flap has 2 spots of corrosion. (Marked) Resolution: Removed light surface corrosion from WH flap upper surface [outboard flap track &mid track]. Cleaned treated bare metal, primer and top coat as required. All work performed IAW. CAMPS 4000. Billing Method Labor USD: Flat Rate Total USD: Hours Rate Thal $1,150.00 $1,150.00 Step: 8.15.1 Completed Removed and blend out light surface corrosion from the R/H Flap, upper surface around 44 track, Treated bare metal. and spot primer as required. IAW. SRM.S1-13.20. 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 - I I59CM 20621-3) by reference of the Gulfstream IIB MAI chapter 27-06-00 entitled. Flap Actuator Yoke - Inspection. During this install, no defects were noted at this time. Billing Method Hours Labor USD: Pans USD: Time and Material $988.80 Total USD: $1,448.80 Rate Thal Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.16 42 1159O120621.3 YOKE ASSY, FLT CONT - FLAP 1 $494.40 $494.40 DRIVE 8.16 N3 11S9CM20621-3 YOKE ASSY, FLT CONT - FLAP $494.40 $494.40 DRIVE Step: 8.16.1 Completed Removed damaged flap "C" track yoke assembly 1 PN I159CM20621.3) and Flat Rate $460.00 discarded. Installed a new replacement yoke assembly ( PN • 1159CM 20621.3) by reference of the Gulfstream 1111 WM chapter 27.06.011 entitled. Flap Actuator Yoke - Inspection. During this install, no defects were noted at this time. Discrepancy: 8.17 R/II flap. outbd IJE 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 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_WorkOnlerPreliminaryInvoicerpt Page 14 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012044 EFTA01734240 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Labor USD: Total USD: Flat Rate $460.00 $460.00 Discrepancy: 8.18 Rill flap, outbd yoke upper hushing phenolic is debonded from the hushing. Bushing needs to be replaced. Resolution: Removed and replaced the Bap "C" track Support Assembly PN - 1159CSA120836.1) by reference of the Gulfstream IIB NUM 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: Pans: Billing Method Flat Rate Time and Material I lours Rate Total $3,450.00 $840.93 $4,290.93 Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.18 #4 I IS9CSM20836-I SUPPORT ASSY,TRACK C-ACT 1 S628.30 $628.30 YOKE 8.18 #6 ADLF8-4005 BUSHING 2 $62.28 $124.56 8.18 #7 I159C20615-5 WASHER 1 $46.87 $46.87 8.18 I159C20615-I I WASHER I $41.20 $41.20 Step: 8.18.1 Step: 8.18.2 Completed Completed Drilled out existing solids and buck rivets for 20 inches to gain access. Peeled hack skin and inspected bolt heads and found both bolt heads mushroomed over from install. Removed fwd boll and bagged as required. All work done LAM GIIB M.M.27.06.00. Removed damaged flap "C" yoke support assembly (PN -1159CSM20836-11 from flap assembly and installed a new replacement "C" yoke support assembly (PN - I IS9CSM20836.1) by reference of the Gulfstream 116 NUM chapter 27-06-00 entitled. wing flap yoke finings removal / installation. Discrepancy: 8.19 UH elevator trim tab has cracked skin in the area of the inner and outter hinges on the top side of the tab. Resolution: Trimmed Lill elevator outbd trim tab hinge skin area as required IAW Gulfstream drawing SE05516001. Labor USD: Total USD: Billing Method Flat Rate Flours Rate Total $460.00 $460.00 Discrepancy: 8.20 1111 aileron trim tab is missing its data plate. Resolution: Completed Traveler RS-QCT-0069 Rev.05. No defects noted on trim tabinstalled new data plate IAM 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 otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoice.rpt Page 15 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012045 EFTA01734241 Bill To: HYPERION AIR, INC. WO I: SC10420 Invoice Number: 7112000954 Billing Method Flours Rate Total Labor USD: Time and Material ST 0.25 (1) $115.00 $28.75 Labor USD: Time and Material OT 0.27 @ $173.00 $46.71 Parts USD: Time and Material $5.97 Services USD: Time and Material $1,135.00 Total USD: $1,216.43 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.2001 1159F30041-11 NAMEPLATE 1 $5.97 $5.97 Services: Ref. No. Description Quantity Sell Price USD Extended USD 8.2011 SERVICE 1.00 $1,135.00 $1,135.00 Discrepancy: 8.21 The left side, outbd wing attachlitting located at FS 345.875 has exposed bare metal and needs to he 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 3460.00 Total USD: $460.00 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 flours 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: NIS25083-111114. Resolution: Removed broken bonding wire P/N: MS25083-1884 from LH fuselage to wing leading edge anti•icc duct and installed new bonding wire P/N: M525083-IBB4 JAW 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 arc in US Dollars (USD). GAC_Work0nlerPrcliminaryInvoice.rpt Page 16 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012046 EFTA01734242 Bill To: HYPERION AIR, INC. WO SC10420 Invoice Number: 7112000954 Billing Method Flours Rate Total Labor USD: Flat Rate $172.50 Parts USD: Time and Material $56.70 Total USD: $229.20 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.2382 PS870-B-I/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 81.725.00 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 none gear. All work performed 'AIN' CHB MM 51-10-00. Completed Performed brash cadmium plating of belly strap aft of nose gear door JAW CPCMM 20-50-05 6.D. Discrepancy: 8.25 Itfli aileron boast bell crank bottom wing plate has groove carved into it from bell crank hushing. 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 Flours Rate Total Labor USD: Flat Rate $287.50 Total USD: $287.50 Discrepancy: 8.26 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 lAW GI1B AMM 27-00-00 and 20-00-00. No further action required. Billing Method Hours Kale 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_WorkOrderPreliminaryInvoiee.rpt Page 17 of 98 Printed: 3/23/2012 4:28:321'? Rd: EFTA_R1_00012047 EFTA01734243 Bill To: HYPERION AIR. INC. WO 8: SC10420 Invoice Number 7112000954 Discrepancy: 8.27 R/11 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 1159CM20217-2 NSN. Refer to item 12.36 for removal and installation of the R/H aileron boost bellcrank assy. Billing Method Hours Labor USD: No Charge Services USD: Time and Material Total USD: Services: Ref. No. Description 8.27 #2 Vendor Supplied Labor Part Ref: I159CM20216-2 aileron boost IwIlerank 8.27 #3 REPAIR Part Ref: 1159CM20217.2 BELLCRANK ASSEMBLY Rate Total N/ C $3,004.49 $3.004.49 Quantity Sell Price USD 1.00 $1,753.56 1.00 $1,250.93 Extended USD $1.753.56 $1,250.93 Discrepancy: 8.28 Upper and lower bearing on 1A1 aileron boost bellcrank is chiped. Resolution: Reinspected 1./11 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 CHI' GLIB 803013 Engine Starter Assembly (Left) - Removal / Installation Resolution: COMPLIED WITH CMP 611B 803013 Engine Starter Assembly (Left) - Removal / Installation. Removed Left Engine Starter Any 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 JAW G-2B AMM 80-01-00 with no defects noted. Billing Method !lours Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.30 COP GLIB 803012 Engine Starter Splines (Left) - Lubrication / Inspection For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 18 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012048 EFTA01734244 Bill To: HYPERION AIR, INC. WO 4: SC10420 Invoice Number 7112000954 Resolution: COMPLIED WITH CMP GLIB 803012 Engine Starter Splines (Left) - Lubrication / Inspection with satisfactory results IAW 62-B AMM 80-01.00. Billing Method Hours Rate Total Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.31 Nylon plugs (anti torsion bumper) on IJH aileron actuator worn and need replacing. ( 4 ea ) Resolution: Removed 4 worn plugs and installed 4 new plugs P/N 87048 on aileron actuator IAW CHB AMM 27-00-00. Billing Method I louts Raw Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $90.64 Total USD: $320.64 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.3141 87048 PLUG 4 $22.66 $90.64 Discrepancy: 832 It/H aileron actuator anti torsion bumpers(4) need replaced. P/N 87048 Ref CMP 1237 Resolution: Removed 4 worn plugs and installed 4 new plugs P/N 87048 in the Rill aileron actuator IAW GM) AMM 27-00-00. Billing Method Hours Rate Total Labor USD: Flat Rate $230.00 Parts USD: Time and Material $90.64 Total USD: $320.64 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 832 41 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 IJH outboard flight spoiler bellcrank assy. with repaired bellcrank P/N 1159CM20209-5. Refer to item 12.153 for Removal and installation of bellcrank assy. 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_WorkOrderPreliminaryInvoice.rpt Page 19 of 98 Printed: 3/23/2012 4:28:32F'? Rd:3 EFTA_R1_00012049 EFTA01734245 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number 7112000954 Services USD: Total USD: Services: Time and Material $1,322.88 $1,322.88 Ref. No. Description Quantity Sell Price USD Extended USD 8.3311 Vendor Supplied Labor 1.00 $1,322.88 $1322.88 Pan Ref: I159CM20209-5 CRANK ASSEMBLY Discrepancy: 8.34 Right outbd flight spoiler bellcrank assy to be sent to Savannah for insp. Resolution: Replaced the RAI outboard flight spoiler bellcrank P/N 1159CM20209.6 and installed "repaired" bellcrank P/N 1159CM207.09-6. Refer to item 12.149 for Removal and installation of hellcrank. Services USD: No Charge N/ C Discrepancy: 8.35 Right inhd flight spoiler hellcrank assy to be sent to Savannah for insp. Resolution: Replaced the R/I1 inboard flight spoiler bellcrank with a "repaired" hellcrank P/N 1159CM2020S-2. Refer to item 12.152 for Removal and installation of bellcrank. Billing Method Services USD: Time and Material Total USD: Services: Ref. No. 8.35 #2 Vendor Supplied Labor 1.00 $1,995.50 $1,995.50 Pan Ref: 1159CM20208-2 CRANK ASSEMBLY Hours Rate Total $1,995.50 $1,995.50 Description Quantity Sell Price USD Extended USD Discrepancy: 8.36 UH 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 Ull elevator hinge #2, hinge to airframe through hole (2-3) Hole measurement is within limits. Work performed IAW CHB 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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 20 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012050 EFTA01734246 Bill To: HYPERION AIR, INC. WO #: 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 1AW Drawing SE055000901 rev.T. No further action required. Billing Method I lours Rate Total Labor USD: Flat Rate $460.00 Parts USD: Time and Material $170.28 Total USD: $630.28 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.37 #1 1159CSM20118-19 PAD ASSY,ELEV HINGE-ELT CONT 1 $170.28 $170.28 Discrepancy: 8.38 FUH elevator trim tab hinge #1 bearing is frozen. Resolution: Removed corroded 12/11 elevator trim tab hinge #1 hearing P/N MS14101-4 and replaced with new bearing P/N MSI4101-4 IAW GAC drawing GAB14E. Checks good. Billing Method I lours Rate Total Labor USD: Flat Rate $460.00 Parts USD: Time and Material $18.85 Total USD: $478.85 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 838#1 MS14101.4 BEARING,PIAIN$ELF LUB & 1 $18.85 $18.85 ALIGN Discrepancy: 8.39 Rfil elevator trim tab hinge #2 bearing is frozen. Resolution: Removed It/11 elevator trim tab hinge #2 hearing 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 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.39 #1 MSI4101.4 BEARING,PLAIN,SELF LUB & 1 $18.85 518.85 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_WorkOnlerPrcliminaryInvoiee.rpt Page 21 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012051 EFTA01734247 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Discrepancy: 8.40 K/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 Rill 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 MS21151-8C S/N NSN and new nut P/N AN316-6R S/N NSN. Refer to Gulfstream Drawing 1159020455 Rev. D for work performed. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $76.48 Total USD: $536.48 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.4091 MS21151-8C ROD END WITH KEY-WAY 1 $76.22 $76.22 8.4092 AN316-6R NUT 1 $0.26 $0.26 Discrepancy: 8.41 WEI elevator trim tab #3 hinge bearing is corroded. Resolution: Removed corroded K/H elevator trim tab hinge #3 bearing P/N MSI4101-4 and replaced with new bearing P/N MS14101-4 JAW GAC drawing GAB14E. Checks good. Billing Method Hour: 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 8.41 #1 M514101.4 BEARING,PLAIN,SELF LUB & I 518.85 $18.85 ALIGN Discrepancy: 8.42 R/H elevator trim tab hinge #1 bushings are corroded. Resolution: Removed corroded K/H 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 Hours Rate Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $122.52 Total USD: $582.52 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8A2 #1 1 159CSM20155-I BUSHING 2 $43.26 $86.52 8.42#2 GABIOF4-4 BUSHING I $3O0 $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 arc in US Dollars (USD). GAC_Work0nlerPreliminaryInvoice.rpt Page 22 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012052 EFTA01734248 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Step: 8.42.1 Completed Removed corroded Wli elevator trim tab hinge NI lower hat bushings P/N's 1159CSS120155-1 ( 2 each) and replaced with new lower hat bushings P/N's 1159LS:1120155-I ( 2 each ) lAW 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 Parts USD: Time and Material $4.557.00 Total USD: $4,787.00 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.43 #1 1159SCC213-17 SHAFT. WING FLAP & STABILIZER 1 $4.557.00 $4,557.00 Discrepancy: 8.44 VII wing, second from outbd flap drive rod is scored. Resolution: Removed IJH wing second from outbd flap drive shaft .P/N 1159SCC213.13, S/N unreadable. Installed new flap shaft W'S 1159SCC2I3-13. S/N 2034 lAW GlIB AMM 27-06.00. See item 8.123 for rigging of flaps. Billine Method Hours Rate Total Labor USD: Flat Rate $230.00 Parts USD: Time and Material $4,556.67 Total USD: $4,786.67 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.44 81 1159SCC213-13 SHAFT I $4.556.67 $4,556.67 Discrepancy: 8.45 IJH elevator trim tab hinge #1 bearing is corroded. Resolution: Removed corroded IJH elevator trim tab hinge #1 bearing P/N NIS14101-4 and replaced with new bearing P/N NIS14101-4 IAW GAC drawing GABI4E. Checks good. Billing Method Hours Kate To al 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 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoice.rpt Page 23 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012053 EFTA01734249 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number 7112000954 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.45 11 MSI4101.4 BEARING,PLAIN,SELF LUB & I $18.85 $18.85 ALIGN Discrepancy: 8.46 Ulf elevator trim tab hinge #2 bearing is corroded / frozen. P/N MS21232-4. Resolution: Removed corroded UH elevator trim tab hinge #2 bearing P/N MS1410I-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 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.46#1 MS14101.4 BEARING.PLAINSELF LUB & I 518.85 S18.85 ALIGN Discrepancy: 8.47 Uti elevator trim tab hinge #3 bushings are corroded. P/N I159CSM20155.1 and P/N 1159CSM20155-5. Resolution: Removed corroded Jill 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-S IAW GAC Drawing # SE05000901-T. Checks good. Billing Method I lours Rate Total Labor USD: Flat Rate $460.00 Paris USD: Time and Material $98.26 Total USD: $558.26 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.4711 1159CSNI20155.1 BUSHING 1 $43.26 $43.26 8.4782 1159CSM20155-5 BUSHING 1 $55.00 $55.00 Discrepancy: 8.48 IJH 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-I and replaced with new hat bushings P/N's 1159CSM20155.1 JAW Urals ing # SE05000901-T. Checks good. Billing Method Hours Kate Tot', Labor USD: Flat Rate $460.00 Parts USD: 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 arc in US Dollars (USD). GAC_Work0nlerPreliminaryInvoice.rpt Page 24 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012054 EFTA01734250 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Total USD: $546.52 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.48 ill 1159CSM20155-1 BUSHING 2 $43.26 $86.52 Discrepancy: 8.49 14/11 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 SE0500090I-5. Work performed IAW GIIB MM 27-04-00. Billing Method Hours Rate Total Labor USD: Time and Material OT 0.27 @ $173.00 $46.71 Pans USD: Time anti Material $388.64 Total USD: $435.35 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8A9 III SE05000901.911P1.5 REPAIR BUSHING 1 $388.64 $388.64 Discrepancy: 8.50 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 GHB 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 R/II elevator trim tab hinge #3 bushings are corroded. Resolution: Removed corroded Rill 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: Pans USD: Billing Method Hours 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 arc in US Dollars (USD). GAC_Work0nlerPreliminaryInvoice.rpt Page 25 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012055 EFTA01734251 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Total USD: $558.26 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.51 #1 11S9CSM20155-1 BUSHING 1 $43.26 $43.26 8.51 #2 I1S9CSM20155-5 BUSHING t $55.00 $55.00 Discrepancy: 8.52 UN elevator trim tab hinge #3 hole 3-1 bushing is No-Go. Bushing being replaced under squawk 8.47. Resolution: Removed Lai elevator trim tab hinge #3 lower hat bushing 3-1 P/N 1159CS8120155-1 and replaced with new hat bushing P/N 1159CSM20155-1 LAW 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 lAW GAMPS 4000. Billing Method Hours Raic Total Labor USD: Flat Rate $460.00 Total USD: 5460.00 Discrepancy: 8.54 CMP CHB 321810 BLEED L WHEEL BRAKES. See 12.51 & 12.52 Resolution: COMPLIED WITH CMP GLIB 321810 BLEED L WHEEL BRAKES. No defects noted. Work done IAW CMP 321810 & GLIB M/M 32-04-01. Complied with GLIB CMP 321815 Brake (Right) - Bleeding Procedure. No defects noted. Work done JAW CMP 321815 & CHB M/M 32-04-01. Labor USD: No Charge N/ C For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_Work0rderPreliminaryInvoice.rpt Page 26 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012056 EFTA01734252 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Discrepancy: 8.5$ CMP GI1B 321315 Antiskid Control System - Functional Test. See 12.51 & 12.52 Resolution: COMPLIED WITH CMP CHB 321315 Antiskid Control System - Functional Test. No defects noted. Work done IAN' CMP 321315 & CHB M/M 32-04-02. Billing Method Hours Rate Total Labor USD: Rat Rate $172.50 Total USD: $172.50 Discrepancy: 8.56 CMP CHB 321305 Wheel Brake (CHB) - Functional Test. See 12.51 & 12.52 Resolution: COMPLIED WMI CMP CHB 321305 Wheel Brake (611B) - Functional Test. No defects noted. Work done IA W CMP 321305 & GIIB 32-04-01. Billing Method flour: Rate Total labor USD: Flat Rate $287.50 Total USD: $287.50 Discrepancy: 8.57 IAI wing upper sponson plate is corroded. Resolution: Removed sealent from around IJH wing sponson plate. All work performed JAW CHB 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 'ANY GAC drawing 5E45802903 limitations as stated in GAC engineering disposition CS278586.Performed cadmium plating repair on 1111 upper sponson plate. All work done JAW Standard Repair/Corrosion of Sponson Plates DWG No. SE45802903 REV.D Billing Method Hours 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: Rd. No. Description Quitiiiiiy Sell Price USD Fut:titled t 'SD 8.57 #1 SERVICE I.1w $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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoiee.rpt Page 27 of 98 Printed: 3/23/2012 4:28:32P? Id :3 EFTA_R1_00012057 EFTA01734253 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Step: 8.57.1 Step: 8.57.2 Completed Removed sealent from around UH wing sponson plate. All work performed IAW CHB MM 51.10-00. Completed Treated and primed all bare metal. Resealed sponson plate. Performed cadmium plating repair on UH upper sponson plate. All work done IAW Standard Repair/Corrosion of Sponson Plates DWG No. 5E45802903 REV.0 Discrepancy: 8.58 Several spots inboard of L/1I wing leading edge need sealant. Resolution: Replaced missing sealant LAW CHB 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 CN1P#575005 , Found Hydraulic line chaffing against structure at I/II wing trailing edge outboard of flap well. Resolution: Repostioned Hydraulic line and wrapped with protective wrap. All work done IAW CHB 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 CMP# 575005, Found a hydraulic leak has caused the under aircraft ( Keel 1 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 tube 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_Work0rderPrcliminaryInvoiee.rpt Page 28 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012058 EFTA01734254 Bill To: HYPERION AIR. INC. WO II: SC 10420 Invoice Number 7112000954 Resolution: Cleaned and Installed all fuel panels removed for x-ray IAW DUB AMM 57-00-00. Performed pressure check with no defects noted. Billing Method Hours Rate Total Labor USD: Flat Rate $1,150.00 Total USD: $1,150.00 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. SE35809903 rev. "C" entitled, Sleeve installation - winglet attachment, Cres. Map of vertical (wing side) repairs are as follows. Fwd. Inbd. 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 - SE35809903.1S & 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 - 5E35809903- 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 Parts 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 5E35809903-19 SLEEVE 1 $123.60 $123.60 8.62 #3 SE35809903-35 SLEEVE 1 $226.00 $226.00 8.6214 5E35809903-39 SLEEVE 1 $72.10 $72.10 8.62 #5 SF.3580990345 SLEEVE 8 570.00 $560.00 8.62#6 SE35809903-35 SLEEVE 8 $226.00 $1,808.00 8.62 #7 SE35809903-19 SLEEVE 1 $123.60 $123.60 8.62 #8 5E35809903-39 SLEEVE 1 $72.10 $72.10 8.62#9 NASII6S-43L BOLT 8 $131.43 $1.051.44 8.62 #10 SE35809903-17 SLEEVE 12 $30.21 $362.52 8.62 #11 SE35809903-37 SLEEVE 12 $129.42 $1,553.04 8.62 #12 NAS1165.421. BOLT 5 $39.00 $195.00 8.62 #14 NAS116511/4 3B BOLT 8 $5.46 $43.68 8.62 #15 NAS1165E40B BOLT 3 $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 arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoicerpt Page 29 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012059 EFTA01734255 Bill To: HYPE:RION AIR, INC. Parts: WO #: SC10420 Invoice Number 7112000954 Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.62#16 GASSSIB3C9 SCREW 100 $1.21 $121.00 8.62 #18 PS870.0.2 SEALANT 1 $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 Hours Rate Total Labor USD: Flat Rate $460.00 Total USD: $460.00 Discrepancy: 8.64 While complying with CMP#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 CUB 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 CMP#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-I , S/N N/A JAW GHB AM M 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_WorkOrderPreliminaryInvoiee.rpt Page 30 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012060 EFTA01734256 Bill To. HYPERION IR. IM'. WO #: SC10420 Invoice Number 7112000954 Resolution: Installed cabin threshold potted insert P/N TYE2001-04-08. AB work performed IAW GUS 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 IJH flap, outbd yoke upper bushing phenolic is debonded front 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 - 1159CSN120836-1) by reference of the Gulfstream IlB MINI 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 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.67 #4 I ISKSM20836-I SUPPORT ASSY,TRACK C-ACT I $628.30 $628.30 YOKE 8.67 #5 NAS1921800-02 BLIND RIVET 300 $1.22 $366.00 8.67 #6 NAS1921804-03 RIVET 200 $1.37 $274.00 8.67 #8 NASI921N104-02 RIVET 300 $3.68 $1,104.00 8.67 #9 NASI921M04-03 RIVET 200 $2.85 $570.00 8.67 #10 NAS6605-58 BOLT, HEX HEAD, CLOSE 'fOL, 2 $11.93 $23.86 UNDRILLED 8.67 #11 1159CS20005.35 WASHER 2 $89.32 $178.64 8.67 #12 N18210421.5 NUT. SELF-LOCKING RING BASE 2 $1.24 $2.48 Discrepancy: 8.68 LAI elevator hinge fitting A-7 bushing ID is No-Go. New hushing (P/N 1159CSM20094-25) is included in "install kit". Resolution: Removed old bushing and installed new bushing P/N 1159CSM20094 as required IAW 27-00-00. Parts included in 72 Month kit. Billing Method Flours 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. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoice.rpt Page 31 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012061 EFTA01734257 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number 7112000954 Discrepancy: 8.69 Rill aileron #1 hinge fitting inbd hole 1.3 is corroded. (Clean, Treat. and remeasure). Resolution: Removed corrosion, treated and renteasured the R/H aileron #1 hinge fitting inhd hole 1-3. Hole is within limits. Work performed lAW GLIB NINI 27-02-00 and SRM 51.13.10. Billing Method I 1 0 1 1 1 , . Rate Total Labor USD: Flat Rate $690.00 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 lAW 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 UH aileron #1 hinge fitting center attach hole 1.2 is corroded. (Clean, Treat, and remeasure). Resolution: Removed corrosion, treated and remeasured the 1./II aileron #1 hinge fitting hole 1-2. Hole measurment is within limits. Work performed lAW 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 IJII aileron #3 wing attach fitting bolt hole, upper and lower bushings are corroded. P/N GABI005-12. 2ea Resolution: Removed corroded 1./H aileron #3 wing attach fitting upper and lower hat bushings P/N's GABIOCS-12 and replaced with new hat bushings P/N's GARIOCS-121AW GAC Drawing # SF.05000901-T. Checks good. 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 arc in US Dollars (USD). GAC_Work0nlerPreliminaryInvoice.rpt Page 32 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012062 EFTA01734258 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Labor USD: Flat Rate $690.00 Pans USD: Time and Material $39.34 Total USD: $729.34 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.72 #1 GABI005-12 BUSHING 2 $19.67 $39.34 Discrepancy: 8.73 Found small amounts of corrosion in 10 bores of the IJH 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. SE35809903 rev. "C" entitled, Sleeve installation - winglet attachment, Cres. Map of vertical (wing side) repairs are as follows. Fwd. lnhd. & Aft inbd. 1st oversize new set (.9057 - 9077) PN - SE35809903-15. 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 & SE35809903-37. Labor USD: Parts 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 he sent to Savannah for insp. Resolution: Replaced the IJII inboard flight spoiler bellcrank with a "repaired" bellcrank P/N 1159S530144•11. Refer to item 12.150 for Removal and installation of hellcrank. Billing Method flours 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 el Vendor Supplied Labor 1.00 $1,800.86 $1,800.86 Part Ref: I159SB30144-O 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_Work0nlerPreliminaryInvoicerpt Page 33 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012063 EFTA01734259 Bill To: HYPERION AIR. INC. WO #: SC10420 Invoice Number 7112000954 Resolution: Removed "O" rings on all 3 oxygen cylinder air lines and installed new o-rings P/N MS22012-6 IAW G-IIB AMM 35.00-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 6.81 @ $115.00 $783.15 Pans USD: Time and Material $48.04 Total USD: $831.19 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.7511 MS22012-6 PACKING RING 4 $8.70 $34.80 8.7513 MS28775406 PACKING-PORT FITTING,3/16 LINE 4 $0.26 $1.04 8.7514 MS28778-5 O-RING, TUBE FITTING 4 $3.05 $12.20 PREFORMED Discrepancy: 8.76 Rudder hinge #1 bearing is rough and corroded. Resolution: Removed old hearing P/N MS28913.5C and replaced with a new bearing P/N MS28913.5C on rudder hinge #1 LAW GAC engineering drawing # SEO5000901 -T. Checks good. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Parts USD: Time and Material $113.82 Total USD: $573.82 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.7611 MS28913-5C BEARING 1 $113.82 $113.82 Step: 8.76.1 Completed Removed bearing retainer and bearing on rudder hinge el lAW GAC engineering drawing # SEO500090I -T. Discrepancy: 8.77 Rudder hinge #2 bearing is rough and corroded. Resolution: Removed old bearing P/N MS28913-5C and replaced with new bearing P/N MS28913-5C on rudder hinge #2 IAW GAC drawing # SE05000901-T. Checks good. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $133.07 Total USD: $593.07 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.7711 MS28913-SC BEARING 1 $113.82 $113.82 8.77 #2 MS20615-5M16 RIVET. MONEL UNIVERSAL HEAD 25 $0.77 $19.25 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryinvoice.rpt Page 34 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012064 EFTA01734260 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Step: 8.77.1 Completed Removed hearing retainer and bearing from rudder hinge #2. Step: 8.77.2 Completed Removed hearing retainers and hearing from rudder hinge #3. (written in Error refer to squawk 8.78.O Discrepancy: 8.78 Rudder hinge #3 bearing is rough and corroded. Resolution: Removed old bearing P/N MS28913.5C and replaced with a new hearing P/N 81528913-5C on rudder hinge #3 TAW CAC drawing SEO500090-T. Checks good. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Parts USD: Time and Material $113.82 Total USD: $573.82 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.78 #1 MS28913-5C BEARING 1 $113.82 8113.82 Step: 8.78.1 Completed Removed hearing retainers and hearing from rudder hinge #3 IAW CAC drawing a SEO500090-T. Discrepancy: 8.79 Rudder hinge #1 attach bolt, airframe side, hole Ls oversized. Resolution: After re-evaluation and further inspection of Rudder # 1 airframe hinge attach point found hinge point fitting to be within limits JAW GIIB MM 27-02-00 requirements. No further action required. Billing Method flours Rate Total Labor USD: Flat Rate $690.00 Total USD: 5690.00 Discrepancy: 8.80 Rudder hinge #2 attach bolt, airframe side, hole is oversized. Resolution: After re-evaluation and further inspection of Rudder it 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 Kate Tom) Labor USD: Flat Rate $690.00 Total USD: $690.00 Discrepancy: 8.81 Rudder hinge #2 rudder fitting upper hole 2.2 is No-Co. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 35 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012065 EFTA01734261 Bill To: HYPE:RION AIR, INC. WO #: SC10420 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 CAC drawing # SE05000901-T. Checks good. Billing Method Hours Rate Total Labor USD: Flat Rate $690.00 Pans USD: Time and Material $12.88 Total USD: $702.88 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.81.1 1159SB30210-43 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 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.82#I SEO5000901.913D1.26 BUSHING 1 $666.87 $666.87 8.82#2 NAS6604D138X 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 GABI0E7-6 and installed new bushings PN. GABI0E7-6 as required IAW GAC drawing # SE05000901-T. Checks good. Billing Method Hours Rate Total Labor USD: Flat Rate $690.00 Parts USD: Time and Material $59.74 Total USD: $749.74 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD MAI GAB I0E7-6 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_WorkOnlerPreliminaryInvoice.rpt Page 36 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012066 EFTA01734262 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. "IY" entitled, Material Removal Limits - Vertical Stabilizer Torque Tube. The torque tube hushing (sleeve) was replaced with new. Reference 72 mo. inspection for replacement of bushing. Billing Method I lours Rate Total Labor USD: Flat Rate $690.00 Parts USD: Time and Material $1,227.33 Total USD: $1,917.33 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.84#1 1159CSM20091.3 SLEEVE 1 $128.96 $128.96 8.84 #2 1159BM20959-O PIN I $143.92 $143.92 8.84 #3 NAS6604H4 BOLT HEX HD-CL 101„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 H1,218-10-17 HILOK 3 $44.45 $13335 8.84 #10 11L218-8-12 IMAM 3 $26.60 $79.80 Discrepancy: 8.85 Rh Flight spoiler actuator fwd hearing pin is burred/defective. Resolution: Complied with by replacing the had RH flight spoiler actuator and installing a Modified RH flight spoiler actuator P/N 1159SCH250-30, REF Item S/N 1731. Work performed IAW CHB MM 27-02-00. 12.151 Billing Method Flours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material 516.506.90 Total USD: $16,506.90 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.85 #2 1159SCH250-30 ACTUATOR, HYDRAULIC FLIGHT 1 $16,500.00 $16,500.00 SPOILER (R/H) 8.85 #3 NAS1612-6A 0 -RING 8 $0.48 $3.84 8.85 #4 NASI612-8A SEAL 6 $0.51 $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_WorkOrderPreliminaryInvoice.rpt Page 37 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012067 EFTA01734263 Bill To: HYPERION AIR, INC. Labor USD: No Charge WO a: SC10420 Invoice Number 7112000954 C Discrepancy: 8.87 Lh Flight spoiler actuator fwd bearing pin is burred/defective. Resolution: Complied with by replacing the had LH flight spoiler actuator and installing a Modified LH flight spoiler actuator l'/N 1159SC11250-29, S/N 2002. Work performed lAW GLIB MM 27-02-00. REF Item 12.148 Labor USD: No Charge N/ C Discrepancy: 8.88 Left "C " Flap track lower inhd and outbd failed measure check after corrosion removal (Ref. to item 8.7) Resolution: Reworked and refinished left "C" flap track JAW Gulftream drawing 5E05811901. Flap track is acceptable for continued normal operation per eng. despo CS278586. No further action required on this item. Billing Method Flours 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 hare wires. Resolution: Inspected the Ft/II outboard flap actuator cannon plug wires and found no broken wire strands. Installed heat shrink sleeve over the wire on Rif outboard flap actuator cannon plug. All work was done JAW Gulfstream (MB AN1N1 20-10-01. Billing Methixl Hours Rate Total Labor USD: Time and Material ST 1.00 @ $115.00 $115.00 Total USD: $115.00 Discrepancy: 8.90 While inspecting the rudder trim actuator found it to be sticking in the full left and full right positions. Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_Work0nlerPreliminaryInvoiee.rpt Page 38 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012068 EFTA01734264 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 71120011954 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 Parts 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.) All work performed IA%V GIIB MM 22-00-00. Discrepancy: 8.92 Found the Left AFT elevator trim cable (I 159C20080-27) 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 10x magnifier and found no damage to any strands at the bend area. No other defects noted. All work performed IA%V GlItt 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 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.9281 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 JAW Culftream 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_Work0nlerPreliminaryInvoice.rpt Page 39 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012069 EFTA01734265 Bill To: HYPE:RION 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 GABIOG6-0500 on inner and outer left aileron hinge. Parts supplied with 72 mnt kit. All work done IAW CHB AMM 27-10-00. Billing Method Ilours Rate Taal Labor USD: Flat Rate $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 1AW CHB AMM 20-00-00 and 27-00-00. Billing Method Hours Rate Total Labor USD: Time and Material OT 0.27 @ $173.00 $46.71 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 NIS27039-1-09 al work in accordance st ith t ;DR amm chapter 27-01-00 Billing Method Hours Rate Total Labor USD: Time and Material ST 2.50 t? $115.00 $287.50 Parts USD: Time and Material $4.16 Total USD: $291.66 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.96 #1 MS27039-I-09 SCREW, MACHINE PAN HEAD 16 $0.26 STRUCTURAL $4.16 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 P/n N1S27039-1-09 al work in accordance with GlIB amm chapter 27-01-00 Billing Method Ilours 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 arc in US Dollars (USD). GAC_Work0rderPreliminaryInvoicespi Page 40 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012070 EFTA01734266 Bill To: HYPF:RION AIR, INC. WO #: SC10420 Invoice Number 7112000954 Labor USD: Time and Material ST 2.00 fit $115.00 $230.00 Parts USD: Time and Material $4.16 Total USD: $234.16 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.97 #1 M527039-1-09 SCREW, MACHINE PAN HEAD 16 $0.26 $4.16 STRUCTURAL Discrepancy: 8.98 Left elevator hinge fitting bearing A-I0 is grooved and needs to be replaced. Resolution: Removed grooved Left elevator hinge fitting bearing A-I0 P/N MS28913.10C and installed new Left elevator hinge fitting bearing A-10 P/N MS28913-10C IAW 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 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.98#1 N1S289B-10C BEARING 1 $504.91 $504.91 Discrepancy: 8.99 Right elevator hinge fitting bearing A-10 is grooved and needs to he replaced. Resolution: Removed grooved Right elevator hinge fitting bearing A-10 P/N MS28913-10C and installed new Right elevator hinge filling bearing A-10 P/N MS28913-I0C IAW GAC drawing # GAB14E. Checks good. Billing Method flours Rate Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $504.91 Total USD: $734.91 Pans: Ref. No. Pan 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 Bouts 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 arc in US Dollars (USD). GAC_Work0nterPreliminaryInvoice.rpt Page 41 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012071 EFTA01734267 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Labor USD: Pans USD: Total USD: Pans: Ref. No. Flat Rate Time and Material Part number: $230.00 $4.42 $234.42 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 MS27039-1-09 al work in accordance with CHB amm chapter 27.01.00 Billing Method Hours Rate Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $4.16 Total USD: $234.16 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.10181 MS27039-1-09 SCREW, MACHINE PAN HEAD 16 $0.26 $4.16 STRUCTURAL 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 I lours Rate Total Labor USD: Flat Rate $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 CHB amm chapter 27-01-00 Billing Method Hours Rate Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $4.42 For detail description of the work complied with see the Work Order Detail repeat Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_Work0rderPreliminaryInvoicc.rpt Page 42 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012072 EFTA01734268 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Total USD: $234.42 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.103 al MS27039-1.09 SCREW, MACHINE PAN HEAD STRUCTURAL 17 $0.26 $4.42 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 # SE05000901-T and Gila 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 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.104 NI I I 59CSM20095-5 BUSHING 1 $185.40 $185.40 8.104 12 I I 59CSM20095-5 BUSHING 1 $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 pin 1159CSM20094-25. All work was done IAIN G-IIB m/m 27-01-00. (Installation to accomplished under item # 12.122 CMP 272315. Ref contingency sheet. Billing Method Hours Rate Total Labor USD: Flat Rate $690.00 Parts USD: Time and Material $54.59 Total USD: $744.59 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.105#1 I I 59CSN12,0094-25 SLEEVE 1 $54.59 $54.59 Discrepancy: 8.106 LH IB Flight Spoiler Bell Crank Rod End has siezed bearing. Resolution: Removed the 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 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_Work0nIerPreliminaryInvoice.rpt Page 43 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012073 EFTA01734269 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Labor USD: Pans USD: Total USD: Pans: Ref. No. 8.106 #1 Flat Rate $115.00 Time and Material $529.40 Part number: $644.40 Description Quantity Sell price USD Extended ( 'SI) 1159O0262-3 PUSH ROD 1 $529.40 $529.40 Discrepancy: 8.107 1.11 OB Flight Spoiler Bell Crank Rod End has set/y(1 hearing. Resolution: Replaced the L/H outboard flight spoiler bellcrank pushrui with "New" rod P/N 1159C20262-3. Refer to item 12.149 for Removal and installation of push rod. Labor USD: Pails USD: Total USD: Parts: Ref. No. 8.107 #1 Billing Method Hours Rate Total Flat Rate $115.00 Time and Material $529.40 Part number: $644A0 Description Quantity Sell price USD Extended USD I159C20262-3 PUSH ROD 1 $529.40 $529.40 Discrepancy: 8.108 RH IB Flight Spoiler Bell Crank Rod End has siezed bearing. Resolution: Replaced the W11 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 Hours Rate Total Labor USD: Flat Rate $115.00 Parts 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 1159O0262-3 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/11 elevator trim tab hinge #2 lower hal 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 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_WorkOrderPreliminaryInvoiee.rpt Page 44 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012074 EFTA01734270 Bill To: HYPERION AIR. INC. Pans USD: Time and Material WO 0: SC10420 Invoice Number 7112000954 Total USD: $546.52 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.109 II 059C5M20155-1 BUSHING 2 $43.26 $86.52 Discrepancy: 8.110 L/H I/B flight spoiler is missing bushing 4-3. P/N 1159SB30210.49. 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 1159SB30210-49 provided in the 72month install kit. Work performed IAW (MB MM 27.02.00. Ref contingency sheet. Pans USD: No Charge N/ C Discrepancy: 8.111 Rill O/B flight spoiler O/B bearing is halfway out of spoiler attach point. Resolution: Reinstalled WH O/B flight spoiler O/It hearing hack into place and secured as required 1AW GLIB AMM 20.00.00. Checks good. Billing Method Hours Rate Total Labor USD: Time and Material ST 0.85 @ $115.00 Total USD: $97.75 $97.75 Discrepancy: 8.112 Right middle Bap drive has grooves in it and requires changing. Resolution: Duplicate item See item 8.117 for details. Discrepancy: 8.113 Left 0/B flight spoilers have rust on steel plate on top surfaces. Resolution: REMOVED , light corrosin and rust on top surface0/B flight spoiler , treated and primed top coat as required IAW GP/ gawps 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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 45 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012075 EFTA01734271 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112000954 Labor USD: Time and Material ST 7.35 @ $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 R/11 elevator , outbd top skin has spot of corrosion, removed light corrosion and sanded as required.Area ready for primer. All work lAW Camps 4000. Discrepancy: 8.114 Right 0/B flight spoilers have rust on steel plate on top surfaces. Resolution: REMOVED light corrosion on spoiler top surface, treated and primed as required JAW GIV CAMPS 4000 Billing Method Hours Rate Taal 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 IJH ground spoiler has chiping paint and corrosion in numerious locations. Resolution: Sanded Lill 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 IAW GAC. GAMPS 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 I AI ground spoiler lAW CHB 51-10-00. Discrepancy: 8.116 L/H flight spoiler actuator rear hearing 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 JAW CHB MM 27-02-00. REF Item 12.148 Billing Method Hours Rate 'Raid Labor USD: No Charge Parts USD: Time and Material Total USD: N/ C $19,912.00 $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_WorkOrderPreliminaryInvoiee.rpt Page 46 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012076 EFTA01734272 Bill To: HYPE:RION AIR, INC. WO1: SC10420 Invoice Number 7112000954 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.11611 1159SCI1250-29 ACTUATOR, HYDRAULIC FLIGHT 1 519,912.00 $19,912.00 SPOILER (MD Discrepancy: 8.117 R/1I wing, second from outbd flap drive rod is scored. Resolution: Removed RJH wing outbd flap drive shaft P/N 11595CC213-15 , SIN unreadable. Installed new flap shaft P/N 11595CC213-15 .5/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 Parts USD: Time and Material $4,984.00 Total USD: $5,214.00 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.11711 1159SCC213-15 SHAFT I $4984.00 $4.984.00 Discrepancy: 8.118 Rfill O/B flight spoiler O/13 hat bushings bushing 6-2 on wing attach fitting failed no go gauge (Ref 12.23) . Resolution: Removed had bushings. Prepped and installed new bushings P/N 115951330210-29 UtiV Gulfstream Drawing 5E05000901 rev.T. IhIling Method Flours Rate Total Labor USD: Flat Rate $460.00 Parts USD: Time and Nlaterial $64.48 Total USD: $524.48 Pans: Rd. No. Part number: Description Quantity Sell price USD Extended USD 8.11811 1159SB30210-29 BUSHING 2 $32.24 $64.48 Discrepancy: 8.119 Ftfil ground spoiler has paint missing and light corrosion in numerious locations Resolution: Sanded and primed R/II ground spoiler that had paint missing, removed light corrosion ,treated and primed and painted as required IAW GAC Gamps 4000. Billing Method Flours Rate rola Labor USD: Time and Material ST 4.75 @ S115.011 $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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoiee.rpt Page 47 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012077 EFTA01734273 Bill To: HYPERION AIR, INC. WO #: SC10420 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 install.P/N MS22012-6 new "0" ring was installed lAW 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. Pan number: Description Quantity Sell price USD Extended 'SD 8.12011 M522012-6 PACKING RING 6 $8.70 $52.20 Discrepancy: 8.121 UH 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 hearing P/N MS28913-6C in L/H aileron inboard hinge as required IAW GAC drawing # GABI4E. Billing Method I lOUN Rate Total Labor USD: Flat Rate $230.00 Parts USD: Time and Material $321.32 Total USD: $551.32 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.121#2 111S20427M5-11 MONEL RIVET 20 $1.93 $38.60 8.121 #3 MS20427M5-18 RIVET, MONEL 100 DEGREE 25 $2.15 $53.75 COUNTERSUNK 8.12184 MS28913-6C BEARING 1 $228.97 $228.97 Discrepancy: 8.122 During NDT Inspections Multiple Spots Of Corrosion Were Found In VII Center Chanel Skegg and F1VD R/II Breastplate Inboard Hi-Lok Fastners. Resolution: Removed Iii-Lok Fastners From L/H Center Chanel Skegg and FWD RJH Breastplate Inboard. Cleaned And Removed Surface Corrosion. Installed HI-Lok Fastners Wet With PRC 1422 B2. All Maintenence Performed In Reference To GHB AMM 57-00-00. Billing Method ROWS Rate Total Labor USD: Time and Material ST 12.76 @ $115.00 $1.467.40 Palls 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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 48 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012078 EFTA01734274 Bill To: HYPE:RION AIR, INC. Pans: WO #: SC10420 Invoice Number 7112000954 Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.122 #1 HL19PB8-12 HILOK 1 $8.24 $8.24 8.122 #2 GA8510B4-10 BOLT 3 $3.16 $9.48 Discrepancy: 8.123 Flaps require rigging, due to actuator removal. Resolution: Complied with flap rigging. Work done I/A/W CHB MM chapter 27.06.00. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.00 @ $115.110 $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 avaiahle and flaps require final rigging. Completed Complied with flap rigging. Work done I/MW GIIB MM chapter 27-06-00. Discrepancy: 8.124 NDT of all hardware over 318" 2 each P/Ns. NAS6610D56 1159CM20223-1 1159CM20264-1 Resolution: Complied with NDTof 2 each PN. NAS6610O56, 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 night spoiler attach hardware missing. Resolution: Installed new hardware P/Ns 1159CM20265-1, AN4C11, NAS1149C0463R and M517826-4. All work done lAW Gulfstream AMM 27-00-00. Parts USD: Parts: No Charge N/C Ref. No. Part number: Description Quantity 8.125 #1 I IS9CM20265.I DOWEL 1 8.125 #2 AN4C11 BOLT MACHINE-CRES,DRILLED 1 SHK 8.125 #3 NASI 149(0463k WASHER-FLAT CRES I 8.125 #4 MS17826.4 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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 49 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012079 EFTA01734275 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112000954 Resolution: Removed surface corrosion on both left and right side surface of wing wedge areas IAW G-11B SRM 51-13-10. Treated and primed areas IAW SRM 51.07.10. Checks good. Billing Method Hours 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 1AW GlIB 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 1159CSH2O500.1 S/N 147, with 10,8043 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. MI work performed IAW GIIB AMM 27.04.00. Ref squawk 12.124 for CMP 272510. Parts USD: No Charge N/ C Pans: Ref. No. Part number: Description Quantity 8.12881 1159CSH20500.1 TAB ASSY, TRIM, ELEVATOR 8.12882 2-16SC-1 DISCHARGER. STATIC WICK Step: 8.128.1 Completed Inspected LH Elevator trim tab hinge fittings on trim tab P/N 1159C51120500-1 S/N TS7 IAW CHB AMM 27-04-00. Found bushings 3-1 and 3-2 to be out of tolerance. Removed bad bushings P/N 1159CSM20155.1 and P/N1159CSM20155.5 and installed new hat bushings P/N 1159CSN120155-1 and P/N 1159CSM20155-5 removed from damaged I.H elevator trim tab P/N 1159CSH2O500-1 S/N 147 hinge fittings 3-1 and 3.2. All work was performed 1AW GAC drawing it SE05000901-T. Discrepancy: 8.129 Perform Ops check of all flight controls as required. Resolution: Billing Method Mut. kale Total Labor USD: Time and Material ST 3.50 Oe $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_WorkOnlerPrcliminarylnvoiccspt Page 50 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012080 EFTA01734276 Bill To: HYPF:RION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 8.130 The RH elevator trim tab actuator's outboard bellows is torn Resolution: Removed torn 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 8.13001 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-M528038-1 S/N-12329, from Fwd RH nose area . Installed NEW OAT sensor P/N-MS28038-1 S/N-00138. Performed ops check JAW GHB AMM 34.02.00. No defects noted. Updated CMP 342515. Billing Method I louts Rate Total Labor USD: Time and Material ST 9.00 @ $115.00 $1,035.00 Parts USD: Time and Material $1,115.60 Total USD: $2,438.10 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.13103 I02-00035-I OAT TEMP BULB 1 $1,115.60 $1,115.60 Step: 8.131.1 Completed 'Verified discrepancy removed OAT sensor connector, reading remains the same. Telling us the sensor is in a open-defective state. Removed OAT sensor from Fwd RIIS nose area P/N-MS28038-I S/N-12329 and checked on bench I.A.W. G IIB M.M. 34.02-00 Performed OAT system - Inspection Check / Bulb resistance vs Temperature Chart . and temp bulb fails. Placed OAT Temp bulb P/N-NIS280384 S/N-I2329 on order and reinstalled OAT Temp Bulb hack in act, and strermered part in act,, awaiting parts delivery ETA early Am. All work performed I.A.%%. 61111 M.M. 34.02.00. Discrepancy: 8.132 APU door motor intermittent. Resolution: Removed APU door actuator P/N GYLC9482-1 S/N 33 and installed overhauled APU door actuator P/N CYLC9482-2 S/N 592 1AW GIIR AMM 49-00-00. Ops check good. See steps for details. Labor USD: No Charge N/ C Pans USD: No Charge N/ C Pans: Ref. No. Part number: Description Quantity 8.13201 GYLC9482-2 ACTUATOR For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoiee.rpt Page 51 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012081 EFTA01734277 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Step: 8.132.1 Step: 8.132.2 Step: 8.1323 Completed Inspected AFT door motor, wiring and linkage NO DEFECTS NOTED. Operated APU door several times with no faults noted. Could not duplicate. Ops check good. AIII work done lAW 6111$ 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 GlIB A NIN1 49-00-00. Actuator stops need safetied. Completed Safetied actuator stops on APU door actuator. Performed Ops check on APU door actuator JAW G11B AMM 49-00-00. Ops check good. Discrepancy: 8.133 IJH elevator trim tab actuator outboard boot is torn in several places. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 0.50 @ $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 GlIB MM 27-04-00. Discrepancy: 8.134 Left main gear side brace actuator up line saturated and leaking. Resolution: Billing Method Hours 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 81 11591120200.83 HOSE ASSEMBLY 1 $398.77 $398.77 Item: 9 Paint Team Manager: Sean Brown Customer Coordinator: Ray Kraber ParUModel 9: AC Serial No./Tail No.: TSWTSO: 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_WorkOrderPrcliminaryInvoice.rpt Page 52 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012082 EFTA01734278 Bill To: HYPERION AIR, INC. Total USD: Pans: Ref. No. Part number: Description WO SC10420 Invoice Number: 7112000954 $2300.00 Quantity 9.101 P1251 HN IMRON 5000 PHONTON GREY EFFECT 9.102 193$ ACTIVATOR Step: 9.1.1 Waiting SAND AREAS treated and primed as required Ramps 4000 Insp 1 Item: 10 Outstanding Parts, Materials, and / or Services Team Manager: Sean Brown Customer Coordinator: Ray Kraber Part/Modell,: AC Serial No./Tail No.: TSWTSO: CSNICSO: Aircraft Time: Discrepancy: 10.1 72 month kit - order in advance. Resolution: Complied with Discrepancy: 10.2 Outstanding services waiting. Resolution: Services USD: Total USD: Services: Billing Method Time and Material Ref. No. Description Hours Kate Total $5.792.58 $5,792.58 Quantity Sell Price USD Extended USD 10.2 tt4 Vendor Supplied Labor 1.00 $2,226.72 $2,226.72 Part Ref: I 159CM202094 CRANK ASSEMBLY 10.2 al SERVICE 1.00 $3.215.86 $3,215.86 10.2 #2 SERVICE 1.00 $0.00 $0.00 10.2 tt3 SERVICE 1.00 $350.00 $350.00 Discrepancy: 103 Resolution: Service for man extra manpower. Services USD: No Charge Services: Ref. No. Description 103 SERVICE Quantity 1.00 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 arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoice.rpt Page 53 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_0 0012 083 EFTA01734279 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112000954 Discrepancy: 10.4 Resolution: Parts pulled not turned green,(check with WiTkelld crew I Billing Method Huun Rate Total Parts USD: Time and Material $609.39 Total USD: Pans: $609.39 Ref. No. Pan number: Description Quantity Sell price USD Extended USD 10.415 1-16SC-1 DISCHARGER, STATIC WICK $75.80 $75.80 10.413 I159CM20228-17 BUSHING 1 $263.21 $263.21 10.4112 1159CM20228-17 BUSHING $263.21 $263.21 10.4 el MS29513-214 PACKING PREFORMED-0 RING 1 $0.41 $0.41 10.4 #4 MS27039-1-09 SCREW, MACHINE PAN HEAD 16 $0.26 $4.16 STRUCTURAL 10.4 e7 NIS25083-1BB4 JUMPER, EI.EC BONDING - 4 INCH $2.60 $2.60 Discrepancy: 10.5 Customer approved overtime. Resolution: 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 Part/Model 0: AC Serial NoJTail No.: TSWTSO: CSN/CS& 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 $85460.00 Resolution: Complied with Customer Supplied CMP Due List. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOnterPreliminaryInvoice.rpt Page 54 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012084 EFTA01734280 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Billing Method Flours Rate Total Labor USD: Parts USD: Total USD: Pans: Ref. No. Flat Rate Time and Material Part number: Description $85,660.00 $14.503.49 Extended USD 51 00,163.49 Quantity Sell price USD 12.1 #1 G3 72MONTH KIT 2 361,385,387,188,390 & SUB / 0386.0499 I $9,893.53 $9,893.53 12.1 #3 1159CSM20091-3 SLEEVE 1 $96.72 $96.72 12.1#4 PRI422-B-2 SEAI.ANT, PRC, CARTRIDGE 4 $38.47 $153.88 12.1 #5 FM191138-8 BOLT 30 $5.15 $154.50 12.1 #6 HL70-8 COLLAR 50 $0.90 $45.00 12.1 #7 NAS1303-29D BOLT 2 $4.35 $8.70 12.1 #9 GABI0G5-00500 BUSHING 3 $74.74 $224.22 12.1 #10 I 159CSN120094-17 SLEEVE 2 $282.13 $564.26 12.1 #11 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 MS2I0421.5 NUT, SELF-LOCKING RING BASE 1 $1.24 $1.24 12.1 #I5 NAS6604D31 BOLT HEX IID-CL TOL.DRILLED 4 $1.87 $7.48 SIIK 12.1 #I6 I 159CS3120118-19 PAD ASSY.ELEV HINGE-FLT CONT 1 $170.28 $170.28 12.1 #17 MS21151.8C ROD END WITH KEY-WAY 1 $76.22 $76.22 12.1 #I8 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 AN$25-10R26 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 PR1422-B-2 SEALANT, PRC, CARTRIDGE 2 $38.47 $76.94 12.1 #25 PR1440-B-1/2 SEALANT, PRC,CARTRIDGE 2 $38.28 $76.56 12.1 #26 NASI303-2711 BOLT 2 $12.47 $24.94 12.1 #27 A V30-00372 CORROSION PREVENTIVE, 13.5 1 $69.53 $69.53 OUNCE AEROSOL (12/CS) 12.1 #28 LUBRI-BOND-220 LUBRICANT, 12 OUNCE AEROSOL 1 $47.87 $47.87 SPRAY 12.1 #29 PR1422-B.2 SEALANT, PRC, CARTRIDGE 4 $38.47 $153.88 12.1 #30 PS870-B-2 SEALANT 2 $56.69 $113.38 12.1 #31 PR 1440-B-2 SEALANT. PRC, CARTRIDGE 2 $46.48 $92.96 12.1 #32 PR 14224.2 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 PR 1440-B-1/2 SEALANT, PRC,CARTRIDGE 1 $38.28 $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 $11.53 523.06 SHANK For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoice.rpt Page 55 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012085 EFTA01734281 Bill To: HYPERION AIR, INC. WO It: 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 $26.82 $26.82 12.1 #41 PR1422-11.1/2 SEALANT,PRC.CARTRIDGE 2 $40.62 $81.24 Discrepancy: 12.2 CMP CHB 246020 C Inverter - Frequency / Voltage Check Resolution: COMPLIED WITH CMP GIIB 246020 C Inverter - Frequency / Voltage Check with no discrepancies noted at this time. All work performed IAW G-HB maintenance manual 2A-03-00. Labor USD: No Charge N/ C Discrepancy: 12.3 CMP GlIB 247020 L Alternator Spline - Lubrication Resolution: COMPLIED WITH CMP GIIB 247020 L Alternator Spline - Lubrication IAW GBH MM 24-02-04. No defects noted at this time. Billing Method Hours Rate Total Parts USD: Time and Material $32.38 Total USD: $32.38 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 12341 NAS1593-214 0 -RING 2 $0.74 $1.48 12342 KB21307 SEAL 2 $15.45 $30.90 Discrepancy: 12.4 CMP CUB 247025 R Alternator Spline - Lubrication Resolution: COMPLIED WITH CMP GHB 247025 R Alternator Spline - Lubrication IAW GIIB MM 24-02-04. No defects noted al this time. Labor USD: No Charge N/ C Discrepancy: 12.5 CMP GlIB 252020 Life Vest(s) - Inspect / Re-Certify Resolution: COMPLIED WITH CMP CHB 252020 Life Vest(s) - Inspect / Re-Certify IAW 611B AMNI 25.00-00. See squawks 12.94 thru 12.110 for life vests status. Billing Method Hours Ratc 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 arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoice.rpt Page 56 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012086 EFTA01734282 Bill To: HYPERION AIR, INC. Labor USD: No Charge Services USD: Time and Material W01: SC10420 Invoice Number: 7112000954 N/ C $487.69 Total USD: $487.69 Services: Ref. No. Description Quantity Sell Price USD Extended USD 12.5 /1 Vendor Supplied Labor 1.00 1487.69 $487.69 Discrepancy: 12.6 CMP GIIB 257530 Lavatory Compartment (Above Floor) - Inspection (AD 74-08-09) Resolution: COMPLIED WITH CMP GlIB 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 COP GlIB 261760 Portable Halon Fire Extinguisher (Cockpit No. 1 I - 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 GlIB 261761 Portable Halon Fire Extinguisher (Forward Cabin) - Inspection Resolution: COMPLIED WITH CMP GlIB 261761 Portable Halon Fire Extinguisher (Forward Cabin) - Inspection. All work done per G-IIB amm ch 26-03-00. No defects noted Laborl.SI) No Charge N/ C Discrepancy: 12.9 CMP GlIB 261763 Portable Halon Fire Extinguisher (Baggage Compartment) - Inspection Resolution: COMPLIED WITH CMP (NIB 261763 Portable Halon Fire Extinguisher (Baggage Compartment) - Inspection. All work done per G-118 anun 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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 57 of 98 Printed: 3/23/2012 4:28:32P? Rd:! EFTA_R1_00012087 EFTA01734283 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112090954 Discrepancy: 12.10 CMP GIIB 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 GlIB 270210 Aileron / Hinge Fitting (Left) - Inspection Resolution: COMPLIED WITH CMP GHB 270210 Aileron / Hinge Fitting (Left) - Inspection as required JAW GHB AMM 27-02-00.Refer to squawks ,8.71,8.72 8.94. for discrepencies noted. NDT performed by Structual testing systems Cert It ES1R124K. No defects noted.. Labor USD: No Charge N/ C Step: 12.11.1 Step: 12.11.2 Completed Removed all three hinges from IAI aileron and cleaned. • Noce all hinges are in the perspective positions and clearly marked as to the inboard/out hoard 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 IA1V G-II B AMM 27-02-00. Ready for NDT. Discrepancy: 12.12 CMP GIIB 270215 Aileron / Hinge Fitting (Right) - Inspection Resolution: COMPLIED WITH CN1P 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. it ES1R124K. No defects noted.. Labor USD: No Charge N/ C Step: 12.12.1 Step: 12.12.2 Completed Removed all three hinges from R/11 aileron and cleaned. • Note• all hinges are in the perspective positions and clearly marked as to the inboard facing side.. Completed Complied with step 13) of part B, the removal of the bearing retainers and bearings from the three hinges on the right aileron IAW G-II B AMM 27-02.00. Ready for NUT. Discrepancy: 12.13 CMP GLIB 270220 Aileron Trim Tab Hinge Fitting - Inspection Resolution: COMPLIED WITH CMP GIIB 270220 Aileron Trim Tab Hinge Fitting - Inspection IAW CHB 27-04-00. No defects noted. Refer to squawk 8.20 for discrepency noted while compling with this CMP. Discrepancy: 12.14 CMP GI1B 270225 Elevator Hinge Fitting (Left) - Inspection Resolution: COMPLIED WITH CMP CHB 270225 Elevator Hinge Fitting (Left) - Inspection IAW GlIB 27-01-00. Refer to squawk 8.98 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 arc in US Dollars (USD). GAC_Work0rderPreliminaryInvoice.rpt Page 58 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012088 EFTA01734284 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number 7112000954 Labor USD: No Charge N/ C Step: 12.14.1 Completed Complied with CMP GIB 270225 Elevator Hinge Fitting (Lett) - Inspection stepB(3) thru B(6) IAN' GLIB AMM 27.01.00. Discrepancy: 12.15 CMP GLIB 270230 Elevator Hinge Fitting (Right) - Inspection Resolution: COMPLIED WITH CMP GIIB 270230 Elevator Hinge Fitting (Right) - Inspection IAW GIIB 27-01-00. No defects noted. Labor USD: No Charge N/ C Step: 12.15.1 Completed Complied with CMP CHB 270230 Elevator Hinge Fitting (RT - Inspection steplit3) thru 11(6) IAN' GIIB 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-11B maint manual 27-04-00. Discrepancy: 12.18 CMP GIIB 270245 Rudder/ Hinge - Inspection Resolution: COMPLIED WITH CMP GIIB 270245 Rudder / Hinge - Inspection IAW GIIB AMM 27-20-00. No defects noted. Labor USD: No Charge N/ C Parts USD: No Charge N/ C Step: 12.18.1 Step: 12.18.2 Completed Gained access to hinge points, removed rudder hinge fittings from rudder. Performed dimensional checks of rudder and hinge fittings. Performed IAW GIIB 27-03-00. Completed Installed lower rudder hinge fitting P/N I159CSIS120025-5 as required and safetied IAW CHB AMM 27-03-00. Discrepancy: 12.19 CMP CHB 270247 Rudder Torque Tube - Inspection Resolution: COMPLIED WITH CMP GIIB 270247 Rudder Torque Tube - Inspection. All Maintenence Performed In Reference To GHB 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 arc in US Dollars (USD). GAC_Work0nlerPrcliminaryInvoice.rpt Page 59 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012089 EFTA01734285 Bill To: HYPERION AIR. INC. WO It: SC10420 Invoice Number 7112000954 Labor USD: No Charge N/ C Step: 12.19.1 Completed Complied with CMP GlIB 270247 Rudder Torque Tube - Inspection. step A. through B. UM. All maintenance performed IAW GIIB MM 27.03.00. Discrepancy: 12.20 CMP GLIB 270250 Inboard Flight Spoiler Hinge (Left) - Inspection Resolution: COMPLIED WITH CMP GHB 270250 Inboard Hight Spoiler Hinge (Left) - Inspection. Used go no go gauges IAW (MB AMM 27-02-00. Ref squawk 8.110 for discrepencies. Labor USD: No Charge N/ C Discrepancy: 12.21 CMP CHB 270255 Outboard Flight Spoiler Hinge (Left) - Inspection Resolution: COMPLIED WITH CMP GHB 271)255 Outboard Flight Spoiler Hinge (Left) - Inspection. Used go no go gauges. No defects found IAW GIIB AMM 27-02-00. Discrepancy: 12.22 CMP GlIB 270260 Inboard Flight Spoiler Hinge (Right) - Inspection Resolution: COMPLIED WITH CMP GHB 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 i Right I - Inspection. l'se go no go gauges. IAW GIIB AMM 27.02.00. Ref squawk 8.111 for discrepencies. Discrepancy: 12.24 CMP GHB 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 JAW 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 arc in US Dollars (USD). GAC_Work0rderPreliminaryInvoice.rpi Page 60 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012090 EFTA01734286 Bill To: HYPERION AIR, INC. WO 4: SC10420 Invoice Number: 7112000954 Discrepancy: 12.25 CMP GIIB 270276 Right Ground Spoiler Hinge - Inspection (Aircraft Ilaving 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 GHB 270610 Rudder Pedal Controls - Lubrication Resolution: COMPLIED WITH CMP GIIB 270610 Rudder Pedal Controls - Lubrication I \ G I Ilt \hi 27.113.00. No defects noted at this time. Labor USD: No Charge Discrepancy: 12.27 CMP CHB 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 CHB 270619 Flap Actuator Bushing (Left Outboard) - Lubrication. Work JAW GHB mm 27-06-00 Labor USD: No Charge N/ C Discrepancy: 12.29 CMP GHB 270622 Flap Actuator Bushing (Right Inboard) - Lubrication Resolution: COMPLIED WITH CMP GIIB 270622 Flap Actuator Bushing (Right Inboard) - Lubrication IAW GHB 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 arc in US Dollars (USD). GAC_Work0rderPreliminaryinvoiee.rpt Page 61 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012091 EFTA01734287 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112000954 Step: 12.29.1 Step: 12.29.2 Completed Complied with CMP GDR 270622 Flap Actuator Bushing (Right Inboard) - Lubrication, step A.through B.(2). All maintenance performed IAW GHB MM 27-06410. Completed Complied with CMP GIIB 270622 Flap Actuator Bushing (Right Inboard) - IAW GlIB MM 27.06.00. No defects noted at this time. Discrepancy: 12.30 CMP GIIB 270623 nap Actuator Bushing (Right Outboard) - Lubrication Resolution: COMPLIED WITH CMP GlIB 270623 Flap Actuator Bushing (Right Outboard) - Lubrication IAN' 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 JAW GOB MM 27-06-00. Completed Complied with CMP GIIR 270623 Flap Actuator Bushing (Right Outboard) - TAW GOB MM 27.06.00. No defects noted at this time. Discrepancy: 12.31 CMP Glib 270635 Control Surface Hinge Joints - Lubrication Resolution: COMPLIED WITH CMP GIIB 270635 Control Surface Hinge Joints - Lubrication. All Maintenence Performed In Reference To GIIB AMM 27-00-00. Discrepancy: 12.32 CMP GlIB 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 Glib 270725 Elevator Trim Tab Actuator (Right) - Lubrication Resolution: COMPLIED WITH CMP (NIB 270725 Elevator Trim Tab Actuator (Right) - Lubrication. Work done JAW CMP 270725 & GLIB 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 arc in US Dollars (USD). GAC_Work0nlerPreliminaryInvoice.rpt Page 62 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012092 EFTA01734288 Bill To: HYPE:RION AIR, INC. WO It: SC10420 Invoice Number. 7112000954 labor USD: No Charge N/ C Step: 12.34.1 Completed Complied with section (B) 1-4 in procedure; the measurements are .625 on upper ID of shall hole, lower hushing II) is.62$ and OD is .748 and lower hole size ID is .625 all dimensions are within Imits LAW GIIB AMNI. Discrepancy: 1235 CMP GIIB 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 GIIB 271014 Aileron Boost Bell Crank (Right) - Inspection Resolution: Complied with CMP GLIB 271014 Aileron Boost Bell Crank (Right) - Inspection as required IAW GIIB MM 27-02-00. Refer to squawk 8.27 for di.screpency noted. Labor USD: No Charge N/ C Step: 12.36.1 Step: 12.36.2 Completed Compleate steps A-B(4) JAW GIIB AMM 27-02-00. Completed Compleate steps A through B(4) IAW GIIB AMM 27-02-00 Discrepancy: 12.37 CMP GLIB 271017 Aileron Actuator (Right) Inspection Resolution: COMPLIED WITH CMP GIIB 271017 Aileron Actuator (Right) - Inspection IAW GIIB MOM 27-02-00. Ref to squawk 832 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 GIIB 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 GIIB 271311 Rudder Actuator and Forward Attach Fitting - Inspection Resolution: COMPLIED WITH CMP CHB 271311 Rudder Actuator and Forward Attach Fitting - Inspection as required. No discrepancies found at this time. All work performed I.A.W. (NIB M.M. 27-03-00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial valtu.s listed in this document arc in US Dollars (USD). GAC_WorkOrderPrcliminaryInvoice.rpt Page 63 of 98 Printed: 3/23/2012 4:28:32P? Rd:) EFTA_R1_00012093 EFTA01734289 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. GlIB M.M. 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 JAW CHB 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 GlIB 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 GlIB 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 611B ANINI 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_WorkOrderPreliminaryinvoiee.rpf Page 64 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012094 EFTA01734290 Bill To: HYPERION AIR, INC. Labor USD: No Charge WO It: SC10420 Invoice Number 7112000954 N/ C Step: 12.44.1 Completed Complied with CMP GIIII 274311 Flap Actuator Yoke i Right Otillmardi - Itipection. Step A. through B.(2). All maintenance performed to SS ( ;Mt \ I 27-06-00. Discrepancy: 12.45 CMP GIIB 274312 Flap Actuator Yoke (Right Inboard) - Inspection Resolution: COMPLIED WITH CMP CHB 274312 Flap Actuator Yoke (Right Inboard) - Inspection JAW CHB AMM 27.06.00.No defects noted. Labor USD: No Charge N/ C Step: 12.45.1 Completed Complied with CMP 61111 274312 Flap Actuator Yoke (Right Inboard) - Inspection. Step A through B.(4). All maintenance performed LAW GIIB MM 27.06.00. Discrepancy: 12.46 CMP CHB 274813 Ground Spoiler Actuator (Left) - Inspection (Aircraft Having 6 Panel Speed Brakes) Resolution: COMPLIED WITH CMP GlIB 274813 Ground Spoiler Actuator (Left) - Inspection (Aircraft Having 6 Panel Speed Brakes) No defects found IAW GlIB AMM 27-01-00. Labor USD: No Charge N/ C Discrepancy: 12.47 CMP GHB 274818 Ground Spoiler Actuator (Right) - Inspection (Aircraft Having 6 Panel Speed Brakes) Resolution: COMPLIED WITH CMP GlIB 274818 Ground Spoiler Actuator (Right) - Inspection (Aircraft Having 6 Panel Speed Brakes) No defects found IAW CHB AMM 27-02-00 Labor USD: No Charge N/ C Discrepancy: 12.48 CMP GHB 275312 Flight Spoiler Actuator (Left) - Inspection Resolution: COMPLIED WITH CMP GlIB 275312 Flight Spoiler Actuator (Left) - Inspection IAW CHB MM 27-02-00. See squawk item 8.87 for discrepancy corrective action. Labor USD: No Charge N/ C Discrepancy: 12.49 CMP GIIR 275317 Flight Spoiler Actuator (Right) - Inspection Resolution: COMPLIED WITH CMP GI1B 275317 Hight Spoiler Actuator (Right) - Inspection IAW GlIB 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_Work0rderPreliminaryInvoice.rpt Page 65 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012095 EFTA01734291 Bill To: HYPERION AIR, INC. WO It: 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 GIIB 321210 Left Anti-Skid Valve Filter Inspection Resolution: COMPLIED WITH CMP GIIB 321210 Left Anti-Skid Valve Filter - Inspection IAW G2-B AMM 32-04-02 with no defects noted. Labor USD: Billing Method Hours Rate Taal No Charge N/ C Parts USD: Time and Material $0.91 Total USD: $0.91 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 125111 NAS1612-4A SEAL, 0.250 INCH OD TUBING 1 $0.43 $0.43 123112 NAS1612-6A 0-RING 1 $0.48 $0.48 Discrepancy: 12.52 CMP CHB 321215 Right Anti-Skid Valve Filter - Inspection Resolution: COMPLIED WITH CMP GIIB 321215 Right Anti-Skid Valve Filter - Inspection LAW 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 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 125201 NASI6I2-4A SEAL, 0.250 INCH OD TUBING 1 $0.43 $0.43 125282 N kS11612-6A 0-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 arc in US Dollars (USD). GAC_Work0nlerPreliminaryInvoiee.rpt Page 66 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012096 EFTA01734292 Bill To: HYPERION AIR, INC. WO 4: SC10420 Invoice Number 7112000954 Discrepancy: 12.53 CMP GLIB 330200 Emergency Exit Light Battery - Scrap Resolution: COMPLIED WITH CMP CHB 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 CHB 331510 Emergency Exit Light Battery • Replacement IAW GLIB AMM 33.02.00. See item 6.1 for discrepancy noted. Labor USD: No Charge NI C Discrepancy: 12.55 CMP CHB 341524 Attitude Indicator Battery No. 1 - Service (PS 823) Resolution: COMPLIED WITII CMP GlIB 341524 Attitude Indicator Battery No. 1 - Service (PS 823) 1AW CHB AMM 34-04-00. No defects noted. AVIALL W043520715. Removed battery P/N 501-1075-02 S/N 2060. Installed TESTED unit P/N 501.1075-02 SIN 2060. Updated CMP's 341530 and 341524. Billing Method flours Rate Total Labor USD: No Charge N/ C Services USD: Time and Material $1,432.86 Total USD: $1,432.86 Services: Ref. No. Description Quantity Sell Price USD Extended USD 125501 SERVICE 1.00 $1,432.86 $1,432.86 Part Ref: 501.107542 POWER SUPPLY Step: 12.55.1 Completed Removed Attitude Indicator battery P/N 501-1075-02 S/N 2060 for service. All work accomplished LAW GLIB MINI 34-04.00. Discrepancy: 12.56 CMP (7.11B 351615 Oxygen Cylinder (No. 2) - Hydrostatic Test Resolution: COMPLIED WITH CMP GIIB 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 $250.00 Total USD: $250.00 Services: Ref. No. Description Quantity Sell Price USD Extended USD 125601 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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoiee.rpt Page 67 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012097 EFTA01734293 Bill To: HYPERION AIR, INC. Services: Ref. No. Description WO It: SC10420 Invoice Number: 7112000954 Part Ref: 176521.6.E CYLINDER 64 CUBIC FT. Quantity Sell Price USD Extended USD 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 Flours 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 12.5711 Vendor Supplied Labor 1.00 $250.00 $250.00 Part Ref: 17652149 BOTTLE, OXYGEN Discrepancy: 12.58 CMP GIIB 351623 Portable Oxygen Bottle (No. I) - Service / Hydrostatic Test Resolution: COMPLIED WITH CMP GlIB 351623 Portable Oxygen Bottle (No. 1) - Service / Hydrostatic Test all work done by Ameron Global Product Support , tracking reference it 255045. Next due date 02/2017. Billing Method Hours Rate Total Services USD: Time and Material $250.00 Total USD: $250.00 Services: Ref. No. Description Quantity Sell Price USD Extended USD 12.5881 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-11-06 NSN and installed new filter AL-11-0G NSN. Work IAW G11B 38-00.00 Billing Method Hours Rate Total Labor USD: No Charge Parts USD: Time and Material N/C $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_WorkOrderPreliminaryinvoice.rpt Page 68 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012098 EFTA01734294 Bill To: HYPERION AIR, INC. WO 0: SC10420 Invoice Number 7112000954 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 12.59 NI AL-II-0G FILTER I 5.59.51 $69.51 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 GLIB MM 53-00-00. Labor USD: No Charge N/ C Discrepancy: 12.61 CMP GLIB 531545 Static Ports (RVSM) Inspection Resolution: COMPLIED WITH CMP GIIB 531545 Static Ports (RVSM) - Inspection IAW GLIB AMM 53.00-00. No defects noted. Labor USD: No Charge N/ C Discrepancy: 12.62 CMP GIIB 534015 Main Power Junction Box Interior - Inspection Resolution: COMPLIED WITH CMP GlIB 534015 Main Power Junction Box Interior - Inspection. All work was done IAW Gulfstream GIIB AMM 53-40-15. No defects noted. Discrepancy: 12.63 CMP GIIB 539010 Main Landing Gear Installation (Left) - Inspection Resolution: COMPLIED WITH CMP GIIB 539010 Main Landing Gear Installation (Left) - Inspection, IAW GIIB NUM Chapter 53-00-00. No defects noted at this time. Labor USD: No Charge bll C Discrepancy: 12.64 CMP GIIB 539020 Main Landing Gear Installation (Right) - Inspection Resolution: COMPLIED WITH CMP GlIB 539020 Main Landing Gear Installation (Right) - Inspection IAW GlIB 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_Work0rdcrPreliminarylnvoice.rpt Page 69 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012099 EFTA01734295 Bill To: HYPERION AIR, INC. Labor USD: No Charge WO 0: SC10420 Invoice Number: 7112000954 N/C Discrepancy: 12.65 CMP GlIB 553035 Rudder Leading Edge and Ballast Weight Corrosion - Inspection Resolution: COMPLIED WITH CMP GlIB 553035 Rudder Leading Edge and Ballast Weight Corrosion - Inspection lAW 611-B AMM 55-00-00. No defects noted. Billing Method Hours Rate Total Labor USD: No Charge N/C Parts USD: Flat Rate $2300.00 Total USD: $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 NASI919M04413 RIVET 100 12.65 #5 NAS19198105.03 RIVET 38 12.65 #6 NASI919M05.03 RIVET 62 12.65 #7 PR1440-B-112 SEALANT. PRC.CARTRIDGE 1 Step: 12.65.1 Completed Complied with rudder ballast weight inspection section (B) 1-5, lAW 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 GlIB 575002 Winglet Attach Hardware (Right) - Inspection Resolution: COMPLIED WITH CMP GLIB 575002 Winglet Attach Hardware (Right) - Inspection. TAW GlIB ANINI 57.00.00. Ref squawk 8.62 for discrepencies. Billing Method Labor USD: No Charge Pans USD: Time and Material Total USD: Pans: Ref. No. Pan number: 12.66 11 6856K Hours Rate Total N/C $127.00 $127.00 Description Quantity Sell price USD Extended USD GREASE. MASTINOX 1 $127.00 $127.00 Discrepancy: 12.67 CMP GlIB 575003 Winglet Attach Hardware (Left) - Inspection Resolution: COMPLIED WITH CMP GlIB 575003 Winglet Attach Hardware (Left) - Inspection IAA' 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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoiee.rpt Page 70 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012100 EFTA01734296 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112000954 Step: 12.67.1 Completed Complied with section (B) step)-3 . Found ID winglet bores with some corrosion see squawk 8.73. Discrepancy: 12.68 CMP GIIB 575005 Wing Exterior (Left) - Inspection (GIIB) Resolution: COMPLIED WITH CM' CHB 575005 Wing Exterior (Left) - Inspection (GHB) IAW GIIB MM 57-00-00. Discrepancies were entered under item 8. Labor USD: No Charge N/ C Discrepancy: 12.69 CMP GHB 575010 Wing Exterior (Right) - Inspection (GIIB) Resolution: COMPLIED WITII CMP GIIB 575010 Wing Exterior (Right) - Inspection (611B) IAW GIIB MM 57-00-00. Refer to Squawks 8.14 for discrepancy noted . Labor USD: No Charge N/ C Step: 12.69.1 Step: 12.691 Completed Complyed with CMPI 575010 sections 1-5 IAN' GIIB MM 57.00.00. Sections 6-10 still remain to be completed. Completed Complyed with cNtrit 575010 R/11 wing exterior inspection IAN' GIIB MM 57410.00. 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 (611B) 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 l&2 , and section B subsection 1 a through i IAW 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 (GHB) Resolution: COMPLIED WITH CMP CHB 575030 Wing to Fuselage Interior (Right) - Inspection (G1111) IAW 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 Cfs1P0 575030 wing to fuselage interior inspection IAW GIIB MM 57-00-00. Note: Screws of access panels are rusted/corroted. Completed Completed CNIFIf 575030 wing to fuselage interior ( Right inspection Sections A I &2 , and section B subsection I a through i IAW GDR 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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoiee.rpt Page 71 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012101 EFTA01734297 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Discrepancy: 12.72 CMP GLIB 575049 Wing Plank Fastener / Radius Block Removal (Left) - Corrosion Inspection (CHB) Resolution: COMPLIED WITH CMP CHB 575049 Wing Plank Fastener / Radius Block Removal (Left) - Corrosion Inspection (GHB) TAW GHB 57.00.00. Work performed by Structual testing systems Cert. # ESIR124K.refer to squawk 8.122 for discrepency noted. Labor USD: No Charge Parts USD: No Charge Step: 12.72.1 Step: 12.72.2 Step: 12.723 Step: 12.72.4 Completed Completed Completed Completed N/C N/C Removed Fuel panels 21-F1' 1.WR-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-15. 22 FT UPR-17. Done I.A.W. GIIB 57-00-00. Began removing Hi-loc fasteners IAW CHB ANITA 57-00-00. Finished removing III-Loc fasteners and complied with CMP CHB 575049 Wing Plank Fastener / Radius Block Removal (Left) - Corrosion Inspection (GI1B) Step 2(a). Completed Inspection By Structual Testing Systems (Cert. # ESIR124K). Refer To Squawk 8.122 For Discrepency Noted. Completed Re-installation Of HI-Loc Fasteners And Complied With (CMP GID3 575049) Wing Plank Fastener / Radius Block Removal (Left) - Corrosion Inspection. All Maintenence Performed In Reference To GHB AMid 57-00-00. Discrepancy: 12.73 CMP CHB 575054 Wing Plank Fastener / Radius Block Removal (Right) - Corrosion Inspection (CHB) Resolution: COMPLIED WITH CMP 611B 575054 Wing Plank Fastener / Radius Block Removal (Right) - Corrosion Inspection (Grm) TAW 611B 57-00-00. Work performed by Structual testing systems Cert. # FS1R124K. 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 $0S0 $198.00 12.73 #2 GAB510B4-13 BOLT $2.83 $8.49 12.73 #3 GAB510I34-7 BOLT 10 $1.90 $19.00 12.73 #4 GAB510B44 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 LVVR-1, 22F1' LWR-2.22•Ff LWR-3, 22-FT LWR-4, 22-FT UPR-12, 22-FT UPR-13. 22-FT UPR-15. 22 FT UPR-17. Done I.A.W. GlIB 57-00-00. Began removing Hi-loc fasteners IAW CHB AMM 57-00-00. Finished removing Iii-Loc fasteners and complied with CMP GHB 575054 Wing Plank Fastener / Radius Block Removal (Left) - Corrosion Inspection (GHB) Step 2(a). ompleted Inspection By Structual Testing Systems (Cert. it F:S1R124K). Refer To Squawk 8.122 For Discrepency Noted. Completed Re-installation Of Hi-la Fasteners And Complied With (CMP CHB 575049) Wing Plank Fastener / Radius Block Removal (Left) - Corrosion Inspection. All Maintenence Performed In Reference To CHB AMM 5740-00. Discrepancy: 12.74 CMP GIIB 575065 Wing Rear Beam (Left) - Inspection (GHB) For detail description of the work complied with see the Work Order Detail report Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 72 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_IR1_00012102 EFTA01734298 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number 7112000954 Resolution: COMPLIED WITH CMP GHB 575065 Wing Rear Beam (Left) - Inspection (GHB). Work IAW GHB MM57-00-00 Discrepancy: 12.75 CMP GIIB 575070 Wing Rear Beam (Right) - Inspection (GIIB) Resolution: COMPLIED WITII CMP GIIB 575070 Wing Rear Beam (Right) - Inspection (GIIB).Work JAW GHB NIM57-00-00 Discrepancy: 12.76 CMP GIIB 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 GlIB 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 Ws 1-2, and section B It's 1-6 IAN' GIIB MM 57-00-00. See Squawk items 8.63/8.64 and 8.65 for discrepancy corrective actions. Completed Complied with CMP#575086 Aileron leading edge and ballast weight corrosion ( LEFT I inspection IAN GIIB 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 (GHB) Resolution: COMPLIED WITH CMP GIIB 575091 Aileron Leading Edge and Ballast Weight Corrosion (Right) - Inspection (GIIB) 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 GlIB 575105 Wing Wedge (Left) - Inspection (GIIB) Resolution: COMPLIED WITH CMP GIIB 575105 Wing Wedge (Left) - Inspection (GlIB) LAW GIIB 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 03) I, removed L/H wing wedge IAW AM\I 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_Work0nlerPreliminaryInvoice.rpt Page 73 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012103 EFTA01734299 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Resolution: COMPLIED WITH CMP G118 575110 Wing Wedge (Right) - Inspection (CHB) IAW CHB 57-00.00. Work performed by Structual testing systems Cert. # ESIR124K—See item 8.126 for discrepency noted. Labor USD: No Charge N/ C Step: 12.79.1 Completed Completed steps Asti and C removing right wing wedge panel as required (Stilt A MI 57.00-00. REF Squawk 8.6 for discrepency noted. Discrepancy: 12.80 CMP GIIB 575115 Wing Sponson Rib (Left) - Inspection (GIllt) Resolution: COMPLIED WITH CMP GIIB 575115 Wing Sponson Rib (Left) Inspection (Gil al. Work IAW CHB MM 57-51.00 Labor USD: No Charge N/ C Discrepancy: 12.81 CMP GIIB 575120 Wing Sponson Rib (Right) - Inspection (CHB) Resolution: COMPLIED WITH CMP GIIB 575120 Wing Sponson Rib (Right) - Inspection (GIIB)AII work done per G-I1B amm ch 05-01.00. No defects noted. Labor USD: No Charge N/ C Discrepancy: 12.82 CMP CHB 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 CHB 732010 Engine Temperature Control System - Functional Test with no faults noted. All work done JAW RR Spay 511-8 EMM 5-10. Labor USD: No Charge N/ C Discrepancy: 12.84 CMP GIIB 733015 ENG LP GOV 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 arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoice.rpt Page 74 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012104 EFTA01734300 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112000954 Resolution: Performed CMP code 733015 as per GllB Rolls Royce EMM 5.10. No defects were noted. Discrepancy: 12.85 CMP GIIB 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 CHB 771510 ENG TGT CIRCUIT RES CHECK. No defects noted. Work performed EAW GAC CHB MM 77-04-00. Labor USD: No Charge N/ C Discrepancy: 12.87 CMP GIIB 771515 ENG TGT CIRCUIT RFS CHECK Resolution: COMPLIED WITH CMP GHB 771515 ENG TGT CIRCUIT RES CHECK. No defects noted. Work performed IA W GAC GLIB MM 77.04.00. Labor USD: No Charge N/ C Discrepancy: 12.88 CMP GIIB 801520 Engine Starter (Left) - Oil Change Resolution: COMPLIED WITH CMP GIIB 801520 Engine Starter (Left) - Oil Change with no defects noted IAW G2-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 12.8802 S9809-3 GASKET 58995.3 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_Work0nlerPreliminaryInvoice.rpt Page 75 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012105 EFTA01734301 Bill To. HYPERION AIR. INC. Parts: WO #: SC10420 Invoice Number 7112000954 Ref. No. Pali initithcr Description Quantity Sell price USD Extended USD 12.88 #5 It F20057 SEAL 2 $39.94 $79.88 12.88 #4 Kit2I6I4 SEAL 1 $14.01 $14.01 Discrepancy: 12.89 CMP GI1B 801535 Engine Starter (Right) - Oil Change Resolution: COMPLIED WITH CMP GHB 801535 Engine Starter (Right) - Oil Change JAW 62-R A NIA, 80.01-00 with no defects noted. Billing Method Hours Rate 'Foul Labor USD: No Charge N/ C Pans USD: Time and Material $115.28 Total USD: $115.28 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 12.89 #1 59809-6 GASKET "C" 1 $3.71 $3.71 12.8982 59809-3 GASKET S8995-3 2 $8.84 $17.68 12.89 #5 BE200.57 SEAL 2 $39.94 $79.88 12.89 tt4 KB21614 SEAL I $14.01 $14.01 Step: 12.89.1 Completed COMPLIED WITH CMP GM) 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 CHB 997407 AD74-08-09 112. MOD LAVATORIES, IAW Al) 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 GlIB 243510 Alternator, Left Engine Resolution: COMPLIED WITH CMP CHB 243510 L Engine Alternator - Removal / Installation P/N 28B135-126A, S/N 119, IAW GHB 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 arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoice.rpt Page 76 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012106 EFTA01734302 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Step: 12.92.1 Step: 12.92.2 Completed Removed Left engine alternator ( P/N: 28B135.126A ; S/N: 119 )IAW GDR MM 24-02.04. No defects noted at this time. Completed Installed Left engine alternator ( P/N: 28B13S-126A ; S/N: 119 )1AW GIIB MM 24.02.04. No defects noted at this time. Discrepancy: 12.93 CMP GIIB 244010 Alternator, Right Engine Resolution: COMPLIED WITH CUP GIIB 244010 R Engine Alternator - Removal / Installation P/N 28B135-126A, S/N 369, IAW GlIB MM 24-02-04. No defects noted at this time. Labor USD: No Charge N/ C Discrepancy: 12.94 CMP GlIB 252031 VEST, LIFE NO 1 Resolution: COMPLIED WITH CMP GIIB 252031 VEST, LIFE NO 1. Removed life vest #1 P/N P01074-101 S/N 263978 and installed #1 life vest P/N PO1074-101 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 al life vest IAN G.I1B AMM 25-20.31. Next inspection due date is SEPT. 2013. Discrepancy: 12.95 CMP GIIB 252032 VEST, LIFE NO 2 Resolution: COMPLIED WITH CMP GIIB 252031 VEST, LIFE NO 2. Removed life vest #2 P/N P01074-101 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 GlIB 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, JAW 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 CHB 252034 VEST, LIFE NO 4. Removed life vest #4 P/N P01074-101 S/N 263871 and installed overhauled life vest P/N 5-51850-6300 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 arc in US Dollars (USD). GAC_Work0rderPreliminaryinvoiee.rpt Page 77 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012107 EFTA01734303 Bill To: HYPERION AIR, INC. WO #: 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 P01074-101 S/N 264143 and installed overhauled life vest P/N S-51850-6300 S/N 21948-1660, IAW GLIB MM chapter 25-00-00. Next inspection due 2/2015. Discrepancy: 12.99 CMP GlIB 252036 VEST, LIFE NO 6 Resolution: COMPLIED WITH CMP CHB 252036 VEST, LIFE NO 6. Removed life vest #6 P/N P01074-101 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 lire vest 1AW G-I1B AMM 25.20.31. Next inspection due date is SEPT. 2013. Discrepancy: 12.100 CMP GIIB 252037 VEST, LIFE NO 7 Resolution: COMPLIED WITH CMP GlIB 252037 VEST, LIFE NO 7. Removed life vest #7 P/N P0723E105P S/N 57151 and installed overhauled life vest P/N P01074-101 S/N 264256., IAW CHB MM chapter 25-00-00. Next inspection due 2/2917. Discrepancy: 12.101 CMP GIIB 252038 VEST. LIFE NO 8 Resolution: COMPLIED WITH CMP GIIB 252038 VEST, LIFE NO 8. Removed lire vest #8 P/N P01074-101 S/N 263943 and installed #8 life vest P/N P01074101 S/N 263943. IAW CHB MM chapter 25-00-00. Next inspection due 9/2013. Step: 12.101.1 Completed Complied with section (A) removal and inspection of 418 life vest P/N P01074-101 S/N 263943 IAW C-11B AN131 25.20.31. Next inspection due date is SEPT. 2013. Discrepancy: 12.102 CMP GlIB 252039 VEST, LIFE NO 9 Resolution: COMPLIED WITH CMP GHB 252039 VEST, LIFE NO 9. Removed life vest #9 P/N P01074-101 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 arc in US Dollars (USD). GAC_WorkOnlerPreliminaryinvoiec.rpt Page 78 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012108 EFTA01734304 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 LAW G-1111 AKIN 25-20-31. Next inspection due date is SEPT. 2013. Discrepancy: 12.103 CMP GHB 252040 VEST, LIFE NO 10 Resolution: COMPLIED WITH CMP GHB 252040 VEST, LIFE NO 10. Removed life vest #10 P/N PO1074-101 S/N 264206 and installed overhauled life vest P/N P01074-101 S/N 264206, IAW (111B MNI 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 PO1074-101 S/N 264206 1AW G-1111 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 P/N PO1074-101 S/N 264204 and installed #11 life vest P/N P01074-101 S/N 264204, JAW CHB MM chapter 25.00-00. Next inspection due 9/2013. Step: 12.104.1 Completed Complied with section (A) removal and inspection of ill l life vest P/N P01074-101 S/N 264204 lAW G-118 AM A1 25.20.31. Next inspection due date is SEPT. 2013. Discrepancy: 12.105 CMP GIIB 252042 VEST, LIFE NO 12 Resolution: COMPLIED WITH CMP GHB 252042 VEST, LIFE NO 12. Removed life vest #12 P/N PO1074-101 S/N 263941 and installed #12 life vest P/N PO1074-101 S/N 263941, IAW GlIB 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 S/N 263941 lAW G-1111 AMM 25.20.31. Next inspection due date is SEPT. 2013. Discrepancy: 12.106 CMP GHB 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 P/N P01074-101 S/N 689973, IAW G118 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 PO1074-101 S/N 264247 and installed overhauled life vest P/N PO1074-101 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 1AW 6-11B AMA! 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 arc in US Dollars (USD). GAC_Work0rdarPrcliminarylnvoicc.rpi Page 79 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012109 EFTA01734305 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112000954 Discrepancy: 12.108 CMP GlIB 252056 LIFE VEST, JUMPSEAT Resolution: COMPLIED WITH CMP CHB 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 GOB 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 3505401 S/N Q0704477 IAW G-115 AN181 25.20.31. Next inspection due date Is Discrepancy: 12.109 CMP GDR 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, IAW 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 S51850.6300 S/N 21965-1660 IAW G-IIB ANIN1 25.20-31. Next inspection due date is Discrepancy: 12.110 CMP GlIB 252058 LIFE VEST, CO-PILOT Resolution: COMPLIED WITH CMP GIIB 252058 LIFE VEST, CO-PILOT. Removed Co-pilots life vest P/N PO723W105P S/N 74634 and installed Co-pilots life vest P/N P0723E105P S/N 74634, IAW CUB MM chapter 25-00-00. Next inspection due 9/2013. Step: 12.110.1 Completed Complied with section (A) removal and inspection of Co-Pilot's life vest P/N P0723W105P S/N74634 LAW G-HB AMM 25-20-31. Next inspection due date is Discrepancy: 12.111 CMP GlIB 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-115 amm ch 26-03-00. No defects noted. Labor USD: No Charge N/C Discrepancy: 12.112 CMP GIIB 266627 HALON FIRE EXT, FWD CABIN Resolution: COMPLIED WITH CMP GlIB 266627 HALON FIRE EXT, FWD CABIN. Removed Fire Extinguisher P/N C352, S/N X-983309 and installed Fire Extinguisher P/N O52, 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 arc in US Dollars (USD). GAC_Work0rderPreliminaryInvoice.rpt Page 80 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012110 EFTA01734306 Bill To: HYPERION AIR, INC. WO 8: SC10420 Invoice Number 7112000954 Discrepancy: 12.113 CMP GlIB 266629 BAGG COMP HALON FIRE BTL Resolution: COMPLIED WITH CMP (MB 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-LIB amm ch 26.03.00. No defects noted. Labor USD: No Charge N/ C Discrepancy: 12.114 CMP 611B 270115 Lateral Control System (Power) - Operational Test Resolution: COMPLIED WITH CMP GlIB 270115 Lateral Control System (Power) - Operational Test IAW GHB AMM 27-02-00. No detects noted. Discrepancy: 12.115 CMP GlIB 272010 Aileron (Left) Resolution: COMPLIED WITH CMP GlIB 272010 Aileron (Left). Removed 1)11 Aileron P/N 1159CS20006-5, S/N 151. Installed the LH aileron P/N 1159C520006-5, S/N 151 IAW GlIB 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 Pans: Ret. No. Part number: Description Quantity Sell price USD Extended USD 12.115 11 NAS6605D50 BOLT HEX HD-CLOSE TOL,DR 1 $6.19 $6.19 SHANK Step: 12.115.1 Step: 12.115.2 Completed Complied with CMP GlIB 272010 IUH Aileron Remus al & Installation Step C to D. Removed 1./11 Aileron Pnitl159CS20006-5 Snt/151 All work done IAW CHB MM 27-2-00. Completed Installed the LII aileron P/N 1159CS20006-5.S/N 151 IAW GlIB MM 27.02.00. Discrepancy: 12.116 CMP 6118 272015 Aileron (Right) Resolution: COMPLIED WITH CMP GlIB 272015 Aileron (Right). Removed the rill aileron P/N 1159CS20006-6, S/N 151. Installed the same RH aileron P/N 1159CS20006-6, S/N 151 IAW CHB 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_WorkOnierPreliminaryInvoice.rpt Page 81 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012111 EFTA01734307 Bill To: HYPERION AIR, INC. WO 8: 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 lAW GHB MM 05-0441. No defects noted at this time. Completed Complied with CMP 272015 steps C. (IJ thru (9J. Removed RH aileron P/N 1159CS20006-6 S/N 151. All work done IAW GIIB MM 27-02-00 Completed Installed the RH aileron P/N 1159CS200064,S/N 151 1AW GIIB MM 2742-00. Ref contingency sheet. Discrepancy: 12.117 CMP GIIB 272020 Aileron Trim Tab Resolution: Complied With CMP GIIB 272020 Aileron Trim Tab - Removal / Installation. All Maintenence Performed In Reference To GHB AMM 27-04-00. No Defects Noted At This Time. Step: 12.117.1 Completed Removed aileron trim tab. Discrepancy: 12.118 CMP CHB 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 GlIB 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 GlIB 270510 Elevator Control System - Operational Test. All Maintenence Performed In Reference To GIIB AMM 27-01.00. Discrepancy: 12.120 CMP GHB 272310 Elevator (Left) Resolution: COMPLIED WITH CMP GlIB 272310 Elevator (Left) IAW GLIB AMM 27-01-00. No defected noted. Labor USD: No Charge N/ C Services USD: No Charge N/ C Services: Ref. No. Description Quantity 12.12001 Vendor Supplied Labor 1.00 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_WorkOrderPrcliminaryInvoice.rpt Page 82 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_R1_00012112 EFTA01734308 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Step: 12.120.1 Step: 12.120.2 Step: 12.1203 Step: 12.120.4 Step: 12.120.5 Completed COMPLIED WITH Elevator (Right) removal preparation IAW CMP GHB 272310 steps A. to B.(g). No defects noted. Completed CONIPL1ED WITH Elevator (LEFT) removal preparation by removing several access panels IAW CMP GM) 272310 No defects noted. Completed Complied with CMP GIIB 272310 Elevator (Left). step C. (1) through (18). All maintenance performed JAW CHB MM 27-01.00. Completed Complied with CNIP GIIB 272310 Elevator HAU. step D. (1) through (k) and D (m) to (o). All maintenance performed IAW GEM MM 27-01-00. Completed weekend nights Discrepancy: 12.121 CMP GHB 271810 ACTUATOR, L ELEVATOR TRIM TAB Resolution: COMPLIED WITH CMP CHB 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 TAW GIIB AIM 27-04-00. Ops checked good. Discrepancy: 12.122 CMP CHB 272315 Elevator (Right) Resolution: COMPLIED WITH CMP GlIB 272315 Elevator (Right) IAW GIIB AMM 27-01-00. Ops checked good. labor USD: No Charge N/ C Pans USD: No Charge N/ C Services USD: No Charge N/C Services: Ref. No. Description Quantity 12.122 81 Vendor Supplied Labor 1.00 Step: 12.122.1 Completed COMPLIED WITH Elevator (Right) removal preparation IAW CMP CHB 272315 steps A. to B.(g). No defects noted. Step: 12.122.2 Completed Complied with CMP GIIB 272315 Elevator (Bight). step C. (1) through (IS). All maintenance performed IAW CHB MM 27-01-00. Step: 12.1223 Completed Complied with CMP CHB 272315 Elevator (Right), step D. (1) through (k) and D (m) to (o). All maintenance performed IAW GIIB 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 ANINI Ch.27.0I.00. Discrepancy: 12.123 CMP CHB 271815 ACTUATOR, R ELEVATOR TRIM TAB Resolution: COMPLIED WITII CMP CHB 271815 ACTUATOR, R ELEVATOR TRIM TAB- Removal / Installation. All Maintenence Performed In Reference To GIB AMM 27-04.00. Oµs checked good. Step: 12.123.1 Completed Complied with Installation step 1)45) of CMP 271815 by reconnecting the previously disconnected Elevator Trim Tab Actuator. All work was done 1A1V (MB AMA! Ch. 27-04-00. Discrepancy: 12.124 CMP GHB 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 arc in US Dollars (USD). GAC_WorkOrderPrcliminarylnvoice.rpt Page 83 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012113 EFTA01734309 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Resolution: COMPLIED WITH CMP GlIB 272510 Elevator Trim Tab (Left) Removed trim tab P/N 1159CSH2O500-I 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 1159CSII20500-1 S/N 57, with 18,947.2 TSN 7,651 CSN. All work performed IAW GLIB 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 GLIB 272510 Elevator Trim Tab (Left) steps C (I) thru C(4) LAW (:11B AMNI 27-04.00. Completed Continued installation of the Lai elevator trim tab. Complied with CMP 272510 C(5) through Dill). Work done UMW GLIB MM chapter 27.04.00. Discrepancy: 12.125 CMP GlIB 272515 Elevator Trim Tab (Right) Resolution: COMPLIED WITH CMP GLIB 272515 Elevator Trim Tab (Right)-Removal / Installation. All Maintenence Performed In Reference To CHB AMM 27-04-00. Labor USD: No Charge N/ C Step: 12.125.1 Step: 12.125.2 Completed Complied with CMP GBH 272515 Elevator Trim Tab (RT) steps C (I) thru C(4) LAW GI1R ANIN1 27-04.00. Completed Complied with CMP 272515 Elevator trim fah (Right) - removal / installation stepsD (2) through (6) Installed right elevator trim tab bolts. all work in accordance with GLIB amm chapter 2744-00. Discrepancy: 12.126 CMP GLIB 270310 Rudder Control System (SP-50G Aircraft) - Operational Test Resolution: COMPLIED WITH CMP GLIB 270310 Rudder Control System (SP-50G Aircraft) - Operational Test. All Maintenence Performed In Reference To CHB AMM 27-03-00. Discrepancy: 12.127 CMP GLIB 272810 Rudder (Aluminum) - Removal / Installation Resolution: COMPLIED WITH CMP GlIB 272810 Rudder (Aluminum) - Removal / Installation LAW CHB 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_Work0nlerPrcliminaryInvoiee.rpt Page 84 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012114 EFTA01734310 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Step: 12.127.1 Completed Complied with CMP 272810 Rudder Removal/ Installation. Step B. (21 (al thru MI and C. III Removed requried access panels and bonding straps. Removed hinge bolt sallies. Applied prentrant to all hinges. Rudder is ready to remove. All work done IAW G1111 MM 27.03.00 Step: 12.127.2 Completed Complied with CMP CHB 272810 Rudder (Aluminum) - Removal / Installation, step C. (2) through (5). All maintenance performed IAN' 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 (II) to (13). All maintenance performed IAW GlIB MM 27-03-00. Step: 12.127.4 Completed Complied with step D (9),(10), (14) thru (16) of CFI' 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 GlIB 270121 Speed Brake - Operational Test (A/C Having 6 Panel Speed Brakes)IAW GlIB AMM 27-02-00. No defects noted. Discrepancy: 12.129 CMP GlIB 275515 Flight Spoiler. Inboard (Left) Resolution: COMPLIED WITH CMP GlIB 275515 Flight Spoiler, Inboard (Left). Removed the LH inboard flight spoiler P/N 1159SCH20700-5, S/N AV119MAR02. and Installed the same HI 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 CIIB 275515 lnh Flight Spoiler Removal & Installation Step C to D. Removed IJI1 bib flight Spoiler Plift H5950120700-5 Sal AVII9MAR02 All work done IAW GlIB MM 27-42-00 Completed Cleaned and greased all hardware and attach fitting holes. Installed the LH inboard flight spoiler P/N 1159SCI120700-5, S/N AVII9MA R02 using new hardware and slip bushings from 72 month install kit. Work performed IAW GlIB MM 27-02-00. Ref contingency sheet. Discrepancy: 12.130 CMP GLIB 275510 Flight Spoiler, Outboard (Left) Resolution: COMPLIED WMI CMP GlIB 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 115965H20702-7, S/N AV-154 Work performed IAW Gin 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 IA4 Out Flight Spoiler Removal & Installation Step C to D. Removed IJH Out Flight Spoiler PM 1159GSH20702-7 Sn8 AV 154 All work done IAW GIIII NINI 27--02-00 Completed Cleaned and greased all hardware and attach fitting holes. Installed the LH outboard flight spoiler P/N 115965020702.7. S/N AV-154 using new hardware and slip bushings from 72 month install kit. Work performed IAW CHB 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_WorkOnlerPrcliminaryInvoicc.rpt Page 85 of 98 Printed: 3/23/2012 4:28:32P? Rd: EFTA_R1_00012115 EFTA01734311 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number 7112000954 Resolution: COMPLIED WITH CMP GlIB 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. Labor USD: No Charge N/ C Step: 12.131.1 Step: 12.131.2 Completed Complied with CMP 275525 Steps B.111 thru C.151. Removed RH Inboard Flight Spoiler P/N1159SCH20700-6 S/N AV-155. All work done IAW (MB MM 27-02-00. Completed Cleaned and greased all hardware and attach fitting holes. Installed the RH inboard flight spoiler P/N 1159SCH20700-6. S/N AV-155 using new hardware and slip bushings from 72 month install kit. Work performed IAW CHB MM 27.02-IN). Ref contingency sheet. Discrepancy: 12.132 CMP GHB 275520 Flight Spoiler, Outboard (Right) Resolution: COMPLIED WITH CMP CHB 275520 Hight 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 lAW 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.111 thru C.151. Removed RH Outboard Flight Spoiler P/N1159SCH20702-8 S/N AV-148. All work done JAW CHB MM 27-02-00. Completed Installed the RH outboard flight spoiler P/N n59SCH20702-13, S/N AV-148 IAW GlIB NI NI 27-02-00. Ref contingency sheet. Discrepancy: 12.133 CMP GIIB 270011 6 PNL SPEEDBRAKE RIG CK (GHB) Resolution: COMPLIED WITH CMP GlIB 270011 6 PNI, SPEEDBRAKE RIG CK (GlIB) IAW GlIB AMM 27-02-00. No defects noted. Discrepancy: 12.134 CMP GIIB 275011 SPLR,GRND L (6PNL) S/BRK(GIIB) Resolution: COMPLIED WITH CMP GlIB 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 I.H ground spoiler P/N 1159CSH30000-5, S/N AV-414 IAW GIIB MM 27-02-00. Labor USD: No Charge N/ C Step: 12.134.1 Step: 12.134.2 Completed Complied with CMP GHB 275011 LAI Ground Spoiler Removal & Installation Step C to D. Removed LAI Ground Spoiler Pnit1159CS1130000-5 SnflAV414 All work done lAW GlIB MM 27-02-00 Completed Installed the LH ground spoiler P/N 1159CS1130000-5.S/N AV-414 IAW GIIB MM 27-02-00. Ops checks still required. Ref contingency sheet. Discrepancy: 12.135 CMP GIIB 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 arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoice.rpt Page 86 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012116 EFTA01734312 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112000954 Resolution: COMPLIED WITH CNIP GUM 270020 CK GIRD SPOILER RIGGING ,IAW GHB AMM 27-02-01. No defects noted. Discrepancy: 12.136 CMP CHB 275166 L.GRD SPOILER IND SW ADJ Resolution: COMPLIED WITH CMP GIIB 275166 L.GRD SPOILER IND SW ADJ JAW GlIB AMM 27-02.01. No defects noted. Discrepancy: 12.137 CMP GIIB 275016 SPLR,GRND R (6PNL) S/BRK(GHB) Resolution: COMPLIED WITH CMP CHB 275016 SPLR,GRND R (6PNL) S/BRK(GIII). 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 11.11Ithru C.I6l. Removed RH Ground Spoiler P/N1159SCH30000-5 S/N AV-411. All work done IAW GIIB MM 27.02-00. Completed Installed RH ground spoiler P/N 1159CSH30000-5, S/N AV-411 IAW GlIB MM 27-02-00. Op% checks still required, ref Item N 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 !ASV GIIB AMM 27-02-01. No defects noted. Discrepancy: 12.139 CMP GIIB 274510 Flap (Left) - Removal / Installation Resolution: Complied with CMP 274510 Left Flap Removal and Installation. P/n off I159C520005.1 S/n 151 UR P/N on 1159CS20005-1 S/n on 151 LftI Work done I/A/W 61111 NINI 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_WorkOnlerPreliminaryinvoice.rpt Page 87 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012117 EFTA01734313 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 If: SC10420 Invoice Number: 7112000954 Complied with CMP 274510 steps A through C(1), 1AW GlIB M/11 Chapter 27-06-00. Complied with CMP GIIB 274510 Flap (Left) - Removal / Installation, step C.(2) through C.(7). All maintenance performed IAW GIIB MM 27-06.00. Complied with CMP 274510 steps I) (I) thrts (7) installed previously removed flap p/n 11590;20005-1 s/n 151 and sallied. Work done IAW G-1111 m/m 27.06.00. (flap still requires symetry and ops checks). ref contingency sheet. Complied with CMP 274510 items 1318) to the end. Work done VAIN' GIIB MM chapter 27-06-00. Discrepancy: 12.140 CMP GHB 274710 Flap (Right) - Removal / Installation Resolution: Complied with CMP 274710 Right Flap Removal and Installation. P/n off 1159CS20005-2 SM 151 R/H P/N on 1159CS20005-2 S/n on 151 R/H Work done U.4/99 GIIB 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 N/C Complied with CMP 274710 steps A through CO), IAW G118 M/N1 Chapter 27-06-00. Complied with CMP GlIB 274710 Flap (Right) - Removal! Installation, step C.(2) through C47). All maintenance performed IA19 Gila MM 27.06.00. Complied with CMP 274510 steps D (I) thru (7) installed previously removed flap p/n 1159CS20005-2 sin 151 and sallied. 1 Work done IAW G-1111 mhn 27-06-00. (flap still requires symetry and ops checks). ref contingency sheet. Complied with CMP 274710 items DO) to the end. Work done UAAV 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 1159/120029-11D3, S/N 468 and installed the LH aileron actuator P/N 11591120029-11D3, 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 1/31 aileron actuator removal .steps(C) I.8 JAW G-IIB AMM27-02-00, P/N 11591120029-1103 S/N 468. Ready to be sent out for overhaul. Completed Installed LH aileron actuator P/N 1159H20029.1103, S/N 468 IAW GIIB 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. 1159SCH2.522E SN. 224GT as required lAW GIIB MM 27-02-00. Labor USD: No Charge N/ C Step: 12.142.1 Step: 12.142/ Completed Complied with WH aileron actuator removal ,steps(C) 6-8 IAW 6-1111 AMI1127-02-00, P/N 1159SCH2522E S/N 224GT. Completed Installed WH aileron actuator PN.1159SCH2522E SN. 224GT as required IAW GIIB CMP 271010 D4 -D 10 and GIIB MM 27-02-00. Requires operational and leak checks. Discrepancy: 12.143 CMP GHB 271315 ACTUATOR, RUDDER TRIM Resolution: COMPLIED WITH CMP GlIB 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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryinvoiee.rpt Page 88 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012118 EFTA01734314 Bill To: HYPERION AIR, INC. Labor USD: No Charge WO It: SC10420 Invoice Number: 7112000954 N/ C Step: 12.143.1 Completed Complied with CMP 271315 steps C4. 92 and C7. to compliy with rudder trim tab actuator inspection (see item 12.401. Rudder trim tab actuator cables need to be tensioned. Cables are flagged. All work performed I.A.W. CUB 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 GIIB 271510 ACTUATOR, AILERON TRIM TAB Resolution: COMPLIED WITH CMP CHB 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 JAW GIIB MM 27-04-00. Discrepancy: 12.145 CMP GlIB 270316 Wing Flap / Stabilizer - Operational Test (CHB) Resolution: Complied with CMP 270316 Wing Flap Stabilizer Operational Test. Work done UMW GIIB MM chapter 27.06.01. Discrepancy: 12.146 CMP GIIB 274811 ACTUATOR,L GRND SPOILER (GIIB) Resolution: Complied with CMP GIIB 274811 ACTUATOR,L GRND SPOILER (CHB) 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. IM GRND SPOILER P/N 1159SCH305.11 S/N 0105 IAD' DIP (MR 274816 steps A. to COO. Completed Installed same ground spoiler actuator as removed previously PN. I159SCH305.I I SN. 0105 IlAW GIIR CMP 274811 and MM 27-02-00. Ground spoiler rigging check shall he accomplished under squawk 12.135 of this Work Order CNIP 270020. Servicing and bleed of hydraulic reservoir to be complied with under squawk 12.179 ,CMP 290110. Discrepancy: 12.147 CMP GlIB 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 arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoiee.rpt Page 89 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012119 EFTA01734315 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 1159SCH305-11 S/N 0130GT IAW CMP GUS 274816 steps A. to C.(10). Completed Installed RAI ground spoiler actuator PN. I159SCH305.11 SN. 0130GT JAW GlIB CMP 274811 and GIIB 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 GlIB 275310 ACTUATOR, I. FLT SPOILER Resolution: COMPLIED WITH CMP GIIB 275310 ACTUATOR, L FLT SPOILER. Removed LH flight spoiler actuator P/N 1159SCH250-3 S/N 362GT. Installed a Modified LH flight spoiler actuator P/N 1159SCH250.29, S/N 2002. Work performed IAW CHB 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 1159SCI1250.3 S/N 362GT IAW CMP CUB 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 27.0240. Ref contingency sheet. Discrepancy: 12.149 CMP GIIB 275320 Outboard Flight Spoiler Bellcrank Assembly (Left) - Removal / Installation Resolution: COMPLIED WITH CMP GlIB 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 I159CM20209.5, NSN IAW GIIB 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:I 159CM20209-5 (recorded from CMP) S/N: n/a. work done IAW (NIB AMM 27-02.00. Completed Installed a Repaired LII outboard flight spoiler bellcrank assembly P/N H590420209-5. NSN JAW GIIB MM 27-02-00. Discrepancy: 12.150 CMP GlIB 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 1159SB30144-11, NSN. Installed a Repaired LH inboard flight spoiler bellcrank assembly P/N 1159SB30144-11, NSN IAW GIIB MM 27-02-00. Labor USD: No Charge N/ C Step: 12.150.1 Step: I 2.150.2 Completed Complied with CMP GIIB 275321 Intboard Flight Spoiler Bellcrank Assembly (Left) - Removal / Installation- Steps C. (I) thrg C.- (7) • Removed (Left) Inthoard Flight Spoiler Bellcrank Assembly P/N: 115951330144-11 (recorded from CMP) S/N: n/a. work done IAW GIIB AMM 27-02-00. Completed Installed a Repaired LH Inboard night speller hellerank assembly P/N 115951830144-11, NSN IAW (MB MM 27-02-00. Ref contingency sheet. Discrepancy: 12.151 CNIP GIIB 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 arc in US Dollars (USD). GAC_WorkOnlerPrcliminaryInvoiee.rpt Page 90 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012120 EFTA01734316 Bill To: HYPERION AIR, INC. WO k: SC10420 Invoice Number: 7112000954 Resolution: COMPLIED WITH CMP GLIB 275315 ACTUATOR, R FLT SPOILER. Removed Rill 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 MM 27-02-00. Labor USD: No Charge N/ C Step: 12.151.1 Step: 12.151.2 Completed Removed Rill flight spoiler actuator. Work done 1/A/W GlIB MM chapter 27-02-00. Complied with CMP 275315 CU) through (5). Completed Installed a Modified RH flight spoiler actuator P/N 1159SCH2.50-30, S/N 1731. Work performed IAW GlIB 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 WEI inbd flight spoiler bellcrank pushrod P/N 1159C20262-3 to the WH lnbd flight spoiler bellcrank ref. GlIB CMP 275322 and the GlIB AIM 27-02-00. Removed P/N 1159C20262-3 S/N NSN. Installed the repaired R/11 inbd flight spoiler bellcrank P/N 1159CM20208-2 NSN ref. CHB CMP 275322 and the GM) 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 GlIB 275322 Intboard Flight Spoiler Bellcrank Assembly (Right) - Removal / Installation- Steps C.- (1) thrg C.- (7) - Removed (Right) Intboard Flight Spoiler Bellcrank Assembly P/N:1159CNI20208.2 (recorded from CMP) S/N: n/a. work done IAW (AIR AMM 2742.00. Discrepancy: 12.153 CMP GlIB 275323 Outboard Flight Spoiler Bellcrank Assembly (Right) - Removal / Installation Resolution: Installed the repaired R/II outbd flight spoiler bellcrank P/N 1159CM20209-6 NSN ref. GlIB CMP 275323 and the (NIB AMM 27-02-00. Removed P/N 1159CM20209-6 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 GlIB 275323 Outboard Flight Spoiler Bellcrank Assembly (Right) • Removal / Installation- Steps C.- (1) thrg C.- (6) • removed (Right) Outboard Flight Spoiler Bellcrank Assembly P/N:1159CN120209-6 (recorded from CMP) S/N: n/a. work done IAW GlIB AMM 27-02-00. Discrepancy: 12.154 CMP GlIB 351511 Oxygen Cylinder (No.2) Resolution: COMPLIED WITH CMP GlIB 351511 Oxygen Cylinder (No. 2) - Removal / Installation. Removed k2 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 IIB 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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 91 of 98 Printed: 3/23/2012 4:28:32P? Rd: EFTA_R1_00012121 EFTA01734317 Bill To: HYPE:R1ON 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 IIB A MN! 35.00.00. Completed Complied with section (CI II I through (DX6) reinstalled #2 oxygen bottle from aircraft P/N 176521.64, S/N 881993 1AW G IIB AMM 35.00.00. Discrepancy: 12.155 CMP GLIB 351010 Oxygen System (Pilot) - Operational Test Resolution: COMPLIED WITH CMP CHB 351010 Oxygen System (Pilot) - Operational Test JAW GII-B AMM 35-00-00. No defects noted. Discrepancy: 12.156 CMP CHB 351015 Oxygen System (Copilot) - Operational Test Resolution: COMPLIED WITH CMP GlIB 351015 Oxygen System (Copilot) • Operational Test JAW GII-B AMM 35-00-00. No defects noted. Discrepancy: 12.157 CMP CHB 351016 Passenger Oxygen System - Operational Test (Gulfstream Installed System) Resolution: Billing Method I loon. Rate Total Parts USD: Time and Material $87.00 Total USD: $87.00 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 12.157 11 M522012-6 PACKING RING 10 $8.70 $87.00 Discrepancy: 12.158 CMP GLIB 351512 Oxygen Cylinder (No.3) Resolution: COMPLIED WITH CMP CHB 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 02 bottle P/N 176521-49, S/N 642653 IAW C JIB 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 from aircraft P/N 176521.49, S/N 642653 and sent to vendor for new hydro IAW G IIB AMM 35.00.00. Completed Complied with section (0 (1) through (DX6) reinstalled #3 oxygen bottle from aircraft P/N 176521.49.5/N 642653 IAW G JIB AMM 35.00.00. Discrepancy: 12.159 CMP GLIB 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_Work0nlerPreliminaryInvoice.rpt Page 92 of 98 Printed: 3/23/2012 4:28:32P? Rd: 3 EFTA_IR1_00012122 EFTA01734318 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Resolution: Complied with section (A), removed portable oxygen bottle from aircraft PIN 900-002.035.01, S/N 33925R and sent to vendor for new hydro IAW C IIB A NIM 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 JAW 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 IIR AMM 35-00-00. Discrepancy: 12.160 CMP GLIB 242520 Inverter, E Instrument Resolution: COMPLIED WITH CMP GLIB 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 GLIB AMM 24-25-20. No defects noted. Discrepancy: 12.161 CMP GLIB 242710 Inverter, B Standby Resolution: COMPLIED WITH CMP CHB 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 IAW 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 CHB AMM 24-27-20. No defects noted. Discrepancy: 12.163 CMP GlIB 246015 B Inverter - Frequency / Voltage Check Resolution: COMPLIED WITH CMP CHB 246015 B Inverter - Frequency / Voltage Check with no discrepancies noted at this time. All work performed IAW 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 arc in US Dollars (USD). GAC_Work0nterPreliminaryInvoice.rpt Page 93 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012123 EFTA01734319 Bill To: HYPERION AIR, INC. WO 8: SC10420 Invoice Number 7112000954 Discrepancy: 12.164 CMP GIIB 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 IAW 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 Ilxs of fuel. Work done I/A/W GBH MM chapter 28-04.00. Discrepancy: 12.167 CMP 61111 284511 No. 1 Left Fuel Quantity Probe - Removal / Installation Resolution: N/A Removal was not required. Discrepancy: 12.168 CMP GIIB 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 arc in US Dollars (USD). GAC_WorkOnlerPreliminaryInvoice.rpt Page 94 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012124 EFTA01734320 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Discrepancy: 12.170 CMP GLIB 289080 SCREEN ASSY,LM FUEL P/U (GIB) Resolution: COMPLIED WITH CMP (NIB 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 IAW GIIB AMM 28-00-00 Labor USD: No Charge N/ C Step: 12.170.1 Completed Complied with CMP GI IR 289080 SCREEN ASSY,LM FUEL P/U (GIIB) Steps AD) thru A(3). Discrepancy: 12.171 CMP GEM 289085 SCREEN ASSY,LA FUEL P/U (GlIB) Resolution: COMPLIED WITH CMP GIIB 289085 SCREEN ASSY,LA FUEL P/U (GHB) Removed fuel pickup P/N 1159P20I42-3 NSN. Installed same fuel pickup P/N 1159P20142-3 NSN IAW GlIB 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(I) thru A(3). Discrepancy: 12.172 CMP GlIB 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 CHB 57-00-00. Work performed by Structual testing Systems Cert. # ES1R124K.See item 8.122 for discrepency noted. Labor USD: No Charge N/ C Step: 12.172.1 Completed Removed Fuel panels 21 -Ff LWR-1, 21-FT LWR-2. 21-FT L1VR-3„ 21-FT LWR-4, 22-FT LWR-I, 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. Discrepancy: 12.173 CMP GIIB 285011 No. 1 Right Fuel Quantity Probe - Removal / Installation Resolution: N/A Removal was not required. Discrepancy: 12.174 CMP CHB 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 arc in US Dollars (USD). GAC_Work0nterPreliminaryInvoiee.rpt Page 95 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012125 EFTA01734321 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112000954 Discrepancy: 12.175 CMP GIIB 281116 R FUEL PROBE INSUL/CAP CK(GIEB Resolution: No Action Required At This Time Due To Maintenence Performed. Fuel Probes Were Never Disconnected. Discrepancy: 12.176 COP GIIB 289090 SCREEN ASSY,RM FUEL P/U (GHB) Resolution: Complied With CMP GIIB 289090 Screen Assembly, Removal / Installation. No Defects Noted At This Time. All Maintenence Performed In Reference To GIIB AMM 28-00-00. Step: 12.176.1 Completed Complied with CMP GIIB 289090 SCREEN ASSY,RM FUEL P/U (011)) Steps A(1) thru A(3). Discrepancy: 12.177 CMP GIIB 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 GIIB AMM 28-00-00. Discrepancy: 12.178 CMP GHB 575053 Lower Wing Planks BL 0 to B1, 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 lAW GIIB 57-00-00. Work performed by Structual Testing Systems Cert. # ES1R124K-See item 8.122 for discrepency noted.. Billing Method flours 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 11 SERVICE 1.00 $14345.27 $14,545.27 Step: 12.178.1 Completed Removed Fuel panels 21-FT LWR-1, 21-FT LWR-2. LWR-3, 21-FT I.WR-4. 224T LWR-1, 22FT LWR-2. 22-FT LWR-3, 22-FT LWR4, 22-V1 UPR-12, 22-FT UPR-13. 22-FT UPR-1.5. 22 F1' UPR-17. Done I.A.W. GIIB 57-00-00. Discrepancy: 12.179 CMP GLIB 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_WorkOrderPreliminaryInvoice.rpt Page 96 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012126 EFTA01734322 Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number 7112000954 Resolution: Complied with CMP 290110 Hydraulic System Reservoir Filling Procedure. Work done VANV CHB MM chapter 29-01.00. Discrepancy: 12.180 CMP GLIB 803027 Engine Starter Splines (Right) - Lubrication / Inspection Resolution: COMPLIED WITH CMP G11B 803027 Engine Starter Splines (Right) - Lubrication / Inspection with satisfactory results IAW G2-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 GI1B 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 1AW 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 $03028 Engine Starter Assembly (Right) - Removal / Installation Steps A. to C(10). Axaiting for Starter duct corrujoint seal. Discrepancy: 12.182 Nine rivnuts need replaced on R/II wing wedge panel. Required drilling of screws due to rivnut spinning. Resolution: Entered in error. Discrepancy: 12.183 Upper and lower bearings on 1./I1 aileron bellcrank are chiped. Resolution: Written in error. Duplicate squawk serer 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 arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicerpt Page 97 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012127 EFTA01734323 Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Communications concerning disputed debts, including a check or other instrument tendered as full satisfaction of a debt, must be forwarded to: GoIfstream Aerospace Ann: 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 arc in US Dollars (USD). GAC_Work0rderPreliminaryinvoice.rpt Page 98 of 98 Printed: 3/23/2012 4:28:32P? Rd:3 EFTA_R1_00012128 EFTA01734324