Gulfstrearn°Ail DYNAMICS C.CINIIMNY

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 11S9CS