EFTA01080493.pdf

Gulfstreant DYNASMCC COMPANY PRELIMINARY INVOICE ParUModel #: GIIB AC Serial No./Tail No.: 151 / N909JE Bldg C.-FAX 561-681-9392 - West Paint Beach. Florida 33406 Mail Remittance To: Overnight Remiaance To: Wire Remittance To: Gulfstream Aerospace Corporation Gulfstream Aerospace Corporation (Box # 730349) Gulfstream Aerospace Corporation P.O. Box 730349 Go JP Morgan Chase Bank. NA JP Morgan Chase Bank. NA Dallas. Texas 75373-0349 ATTN: Dallas National Wholesale Lockbox TX1-0029 Chicago. IL 60670 14800 Frye Road Ft. Worth, TX 76155 Invoice Number. 7112000954 Bill To: HYPERION AIR, INC. Invoice Date: 3/15/2012 3800 SOUTHERN BLVD Customer ID: CH200 SUITE 204 P.O. Number. WEST PALM BEACH, Florida 33406 Repair Station: FAA CRS PB8R624N United States In Date: 02/06/2012 Out Date: 03/23/2012 Payment Type: Net 30-Open terms Payment Terms: Title: HYPERION AIR, INC. INVOICE SUMMARY FOR WORK ORDER NUMBER: SC10420 lime & Materials Flat Rate Total Labor USD: $27,009.12 $161,722.63 $188,731.75 Parts USD: $91,680.83 $6,500.00 $98,180.83 Services USD: $33,067.13 S0.00 $33,067.13 Detail Subtotal USD: $151,757.08 $168,222.63 $319,979.71 Subtotal USD: $319,979.71 Funds on Deposit USD: $0.00 Total USD: $319,979.71 For detail description of the work complied with see the Work Order Detail report. Unless (ahem' indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 1 of 98 Printed: 3/23/2012 4:28:32P) BAY. EFTA01080493  Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Item: 1 Airframe Gulfstream GLIB Scheduled N909JE Team Manager: Sean Brown Pan/Model #: GIIB Customer Coordinator: Ray Kraber AC Serial No./Tail No.: 151 / N909JE TSN/TSO: CSN/CSO: 5663 Aircraft Time: 10804.3 Discrepancy: 1.1 Return to Service FAR 91.409 (f) (3) Inspection Resolution: ACTT: 10,804.3 ACTL: 5,663 DATE: March XX, 2012 I certify that this aircraft has been inspected in accordance with a Due List Inspection under the approved manufacturer's recommended inspection program, FAR 91.409 (f)(3) and is approved for return to service with regards to the maintenance accomplished. Further details of this inspection and related maintenance are on file at this repair station under the above work order. Thomas J. Choynowski, Sr. Airworthiness Inspector Gulfstream-PBI 1500-C Perimeter Road West Palm Beach, FL 33406 FAA CRS PB8R624N Step: 1.1.1 Waiting A/C Times and Cycles approval (L) Step: 1.1.2 Waiting A/C Warrant• Status / Contracts approval (L) Discrepancy: 1.2 Inbound/Outbound Inspection Resolution: Complied with inbound inspection as required. Labor USD: No Charge N/ C Step: 1.2.1 Completed Inbound/Preliminary Inspection Step: 1.2.2 Waiting Outbound Inspection approval (L) Discrepancy: 1.3 Preflight Inspection Resolution: Discrepancy: 1.4 Comply with Debrief Checklist For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 2 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080494  Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Resolution: Complied with Debrief Checklist Step: 1.4.1 Completed Arrival/Debrief 90 Day Due List Review Accomplished. Step: 1.4.2 Completed List Operator's Airworthiness Requirements & Special Documentation Requests. Step: 1.4.3 Completed Review Technical Operations Update prior to return to service for newly released bulletins and advise operator. Discrepancy: 1.5 Tool Clearance Resolution: All tooling was returned to the toolroom. Pans USD: No Charge N/C Parts: Ref. No. Part number: Description Quantity 1.5 #1 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 ArrivaUDeparture Assist & Video Aircraft Resolution: Arrival/Departure Assist & Video Aircraft as required. Discrepancy: 1.9 Sample Hydraulic Fluids Resolution: Sampled Hydraulic Fluids as required. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 3 of 98 Printed: 3/23/2012 4:20:32P) Ftst X EFTA01080495  Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 1.10 Remove Valuables & Secure. Resolution: Na Discrepancy: 1.11 Comply with Service Team Manager Checklist Resolution: Discrepancy: 1.12 Fluids Used (OiLs/Skydrol) - (Materials Only) Resolution: Billed as required. Discrepancy: 1.13 STM / Quality review of work order and logbook entry prior to departure Resolution: Discrepancy: 1.14 Towing (Does not include Hangar Moves) Resolution: Towed as required. Labor USD: No Charge N/ C For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 4 of 98 Printed: 3/23/2012 4:28:32P) Flee X EFTA01080496  Bill To: HYPERION AIR, INC. WO*: SC10420 Invoice Number: 7112000954 Discrepancy: 1.15 HazMat - Identify & provide a manifest, and a Shipper's Declaration for Dangerous Goods for all hazardous materials that are loaded aboard any aircraft. FAR Part 121 or 135 Operators will provide a hazardous material notification letter required by FAR 135.505 (e) prior to maintenance at this Repair Station iaw FAR 145.206 (a) (b). If there is to be loading of hazardous materials it shall be complied with by Hazmat trained authorized GDAS-PBI personnel only. Resolution: Na Discrepancy: 1.16 Aircraft Cleaning Resolution: N/A Discrepancy: 1.17 Billable Consumables & Shop Supplies Resolution: as required. Billing Method Hours Rate Total Pans USD: Flat Rate $4,000.00 Total USD: $4,000.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicespt Page 5 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080497  Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Discrepancy: 1.18 Major Alterations regulatory compliance requirements to be completed by installer as indicated on FAA form 8110-3. Copy and paste from attached statements as needed and edit as required. COMPLY WITH REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d). COMPLIED WITH THE REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d), via GROUND TEST REPORT-REPORT No. CEXXXXXXXX REV. X, ( IN SUPPORT OF STC XXXXXXXXX ) and GR4R216M REPAIR STATION INTERFERENCE TESTING REQUIREMENTS POST MAJOR ALTERATIONS COMPLIANCE FORM. COMPLY WITH REQUIREMENTS OF FAR 25.1529, INSTRUCTIONS FOR CONTINUED AIRWORTHINESS. REF XXXXX MANUAL, P/N XXXXXXX REV. X, FOR INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AND BLOCK 8 OF FAA FORM 337, DATED XX/XX/XXXX. COMPLY WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01.04 AND FAR 25.1353 (B) COMPLIED WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01.04 AND FAR 25.1353 (B) BY ENSURING ROUTING WAS IN ACCORDANCE AC43.13-1B, CHANGE 1 CHAPTER 11, SECTION S. Resolution: N/A Discrepancy: 1.19 Update Weight & Balance Resolution: N/A For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 6 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080498  Bill To: HYPERION AIR, INC. WO #: SC10420 Invoice Number: 7112000954 Discrepancy: 1.20 Exterior Paint and Weight & Balance Requirements. Review scope of aircraft exterior paint touch-up/repairs, and skin replacements resulting in paint reapplication, and determine affect on weight and balance. For surfaces where paint is stripped and reapplied or added on top of existing paint on an area greater than 36 square feet the thickness values will be documented before and after painting . If average thickness values remain the same, weight and balance revision is not required. For surfaces painted with an area greater than 36 square feet and before and after paint thickness average varies, QC review for possible weight and balance revision will be required. * Thickness will be plotted on an aircraft drawing derived from AMM chapter 6 or other suitable sketch, attached to the work order and measurements taken on a two square foot grid. * Reference CAMPS 4000, paragraph 3.5.1 for paint restrictions to flight control surfaces and RVSM certified aircraft. * Reference CAMPS 4000, total average thickness shall not exceed 6 mils. * Per GAC Mass Properties Engineering, paint thickness of 5 mils equals .055 pounds per square foot. * If after QC review, weight change is greater than 2 pounds or .05% of MAC, the weight and balance report will require recomputation. Resolution: N/A Discrepancy: 1.21 "Advise customer of preservation requirements per ATA Chapter 10 of the relevant maintenance manuals for Airframe, Engines, and APU; review requirements in relation to scheduled Date Promised and later potential Date Completed; and perform maintenance or preservation actions as directed by the customer and documented as a Work Order Squawk. Resolution: N/A Item: 6 Avionics Team Manager: Sean Brown ParUModel Customer Coordinator: Ray Kraber AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 6.1 MED emergency light does not illuminate when EMER LT switch is turned on or in the AUTOMATIC mode. Works when switch is placed in MANUAL Resolution: Performed operational check. Found MED emergency light works in manual but not automatic. Gained access to MED emergency lights. Found G-switch tripped. Reset G-switch. Performed operational check. Checks good. All work performed IAW G-II AMM chapter 33.02-00. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WoikOrderPreliminarylnvoice.rpt Page 7 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080499  Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Billing Method Hours Rate Total Labor USD: Time and Material ST 2.83 @ $115.00 $325.45 Total USD: $325.45 Discrepancy: 6.2 AFT entryway light inop. Resolution: Item: 8 Mechanical Team Manager: Sean Brown Part/Model SI: Customer Coordinator: Ray Kraher AC Serial No./Tail No.: TSN/TS0: CSN/CS0: Aircraft Time: Discrepancy: 8.1 Extra time for removing BUL-1 & BUL-2 so that BUL-3 can be removed for elevator removal. Note: these panel not on removal sheet for elevators. Resolution: Complied with info only. Billing Method Hours Rate Total Labor USD: Flat Rate $920.00 Total USD: $920.00 Discrepancy: 8.2 While complying with CMP# 272015, Right aileron removal/installation, found most screws corroded/rusted. Quantity : ( 100 ) ( P/N: NAS 1203.3) screws, ( 40 ) ( P/N: NAS 1203-5 ) screws. NOTE: Quantity included's rusted/corroded Left aileron R&R panel screws. Resolution: Installed new screws as reuired. P/N NAS 1203.3 and NAS 1203.5. lAW GIIB AMM 27-00-00 and 20-00-00. Billing Method Hours Rate Total Labor USD: Flat Rate $230.00 Parts 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 are in US Dollars (USD). GAC_Work0rderPrelintinaryInvoicespt Page 8 of 98 Printed: 3/23/2012 4:28:32PD Rd X EFTA01080500  Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.281 NASI203-3 BOLT 100 $0.26 $26.00 8.2 #2 NASI203-5 BOLT 50 $0.26 $13.00 8.2 #3 GAS550E3S9 SCREW 10 $4.12 8$1.24 47 20 8.2 #4 GAS550E3S10 SCREW 4 $1.81 8.2 #5 NAS583-II BOLT 4 $24.66 $98.64 8.2 #6 NAS583-I3 BOLT 2 $15.68 $31.36 8.2 #7 NAS583-I4 BOLT 2 $23.77 $47.54 8.2 #8 NAS583-I6 BOLT 2 $17.67 $35.34 Discrepancy: 8.3 While comply with CMP 272810 Rudder removal. Found upper bonding wire broken at vert stab Resolution: Removed broken upper rudder bonding wire at vert stab P/N MS25083-2BB13 and replaced with new bonding wire P/N MS25083-2BB13 IAW GIIB AMM 20-00-00. Billing Method Flours Rate Total Labor USD: Flat Rate $230.00 Pans USD: Time and Material $10.30 Total USD: $240.30 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8381 MS25083-2BBI3 JUMPER-ELEC BONDING,I3 IN I $10.30 $1030 Discrepancy: 8.4 While complying with CIHN's 575030/575025 , Wing to fuselage interior LefURight inspection, found ALL screws rusted/corroded. Most needed screwbusters for removal which amounted to considerable time over CMP aloted time. Screws needed as follows: P/N: MS24694s50 : Qty: 330 P/N: 1159B21241-71 Qty: 1 P/N: 1159B21241-78 Qty: 1 P/N: 1159B21241-33 Qty: 1 P/N: 1159B21241-73 Qty: 1 P/N: 1159B21241-81 Qty: 1 P/N: 1159B21241-35 Qty: 1 Resolution: Removed and discarded corroded screws and installed new screws.P/N: M524694550 : Qty: 330 P/N: 1159B21241-71 Qty: 1 P/N: 1159B21241-78 Qty: 1 P/N: 1159B21241-33 Qty: 1 P/N: 1159B21241-73 Qty: 1 P/N: 1159821241.81 Qty: 1 P/N: 1159B21241-35 Qty: 1 All work done i/a/w G-II B SRM ch 51.41.00. No further defects noted. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelititinaryInvoicespt Page 9 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080501  Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $78.00 Total USD: $538.00 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.4 11 M524694S50 SCREW-MACHINE,FLAT CSK HEAD 300 $0.26 $78.00 Discrepancy: 8.5 Change float valve mid point on right wing per customer. Resolution: Remove vent float valve P/N 159SC-P-006 S/N1010. Install a New float valve P/N 159SCP006-1 S/N 4771. Install new O rings under mount screw heads. All work performed IAW GLIB AMM 28.02.00. Billing Method Hours Rate Total Labor USD: Time and Material ST 15.88 @ $115.00 $1,826.20 Labor USD: Time and Material OT 0.13 @ $173.00 $22.49 Parts USD: Time and Material $2,557.27 Total USD: $4,405.96 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.511 1159SCP006-1 PUMP 1 $1,925.35 $1,925.35 8.5 13 HTI83-3-2 SCREW 3 $197.76 $593.28 8.514 GASI3AF6 O-RING 3 $12.88 $38.64 Step: 8.5.1 Completed Remove float valve mid point on right wing P/N159SC-P-006 S/N 1010. Work LAW GLIB MM 28-02-00 Step: 8.5.2 Completed Positioned new float valve in place, P/N 11S9SCP006.1, S/N 4771, and tightened mounting screws. Float valve will have to be removed in order to install 3 o-rings that are to be placed under mounting screws. Refer to Gulfstream BB IPC 28-10-00 figure 6, sheet 1, item 3. O-rings are on order. Step: 8.5.3 Completed Install 3 o rings under float valve mounting screw heads IAW (MB AMM 28-01.01. Discrepancy: 8.6 Nine rivnuts need replaced on R/H wing wedge panel. Required drilling of screws due to rivnuts spinning. Resolution: Removed and replaced nine rivnuts on the R/I4 wing wedge panel. Installed new rivnuts P/N GAN512B3-166 wet with sealant. Had to gain acess to fuel tank area to remove drilled out rivnuts All work done IAW G-IIB SRM 51.41-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 13.44 @ $115.00 $1,545.60 Labor USD: Time and Material OT 4.35 @ $173.00 $752.55 Pans USD: Time and Material $273.47 Total USD: $2,571.62 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.6 11 GAN512B3-166 BLIND NUT 10 $1.52 $15.20 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 10 of 98 Printed: 3/23/2012 4:28:32P) Rd X EFTA01080502  Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.6 #2 GAN512B3-216 NUT 10 $6.10 $61.00 8.6 #3 GAN512B3-266 RIV-NUT 10 $15.88 $158.80 8.6 #4 PR1422-B-2 SEALANT, PRC, CARTRIDGE 1 $38.47 $38.47 Step: 8.6.1 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 Step: 8.6.2 Completed Removed access cover 22-SR-2 on outboard side of sponson Step: 8.6.3 Completed Removed all spinning and bad donuts on the RAI wing wedge panel IAW G-IIB AMM 5140.00. Discrepancy: 8,7 Left wing flap tracts A,B,C, and D have corrosion on roller bearing surfaces. Resolution: Removed corrosion from flap track bearing surfaces on tracks A,B,C and D JAW (MB CPCM 20.50.01.Measured tracks A,B,C and D for thickness as required JAW Gulftream drawing SE05811901. See item 8.88 for details on track C. All others check good. Performed brush cadmium plating repair to all exposed surfaces of flap tracks A,B,C and D IAW Gulftream drawing SE05811901.Cleaned and protected tracks and surrounding area, masked-off track bearing surface, applied two coat epoxy primer 2012 and surface primer, applied top coat, JAW. GAMPS 4000. Billing Method Hours Rate Total Labor USD: Flat Rate $6,900.00 Pans USD: Time and Material $153.12 Total USD: $7,053.12 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.7 #1 PRI440-B-1/2 SEALANT, PRC,CARTRIDGE 4 538.28 $153.12 Step: 8.7.1 Completed Removed corrosion front flap track bearing surfaces on tracks A,B,C and D IAW GIIB CPCM 20-50-01. Step: 8.7.2 Completed Measure tracks A,B,C and Dfor remaining thickness. Step: 8.7.3 Completed Performed brush cadmium plating repair to all exposed surfaces of flap tracks A,B,C and D IAW Gulftream drawing SE05811901. Step: 8.7.4 Completed Cleaned and protected tracks and surounding area, masked-off track bearing surface, applied two coat epoxy primer 2012 and surface primer, Prep. tracks to top coat. IAW. CAMPS 4000. Discrepancy: 8.8 Right wing flap tracts A,B,C, and D have corrosion on roller bearing surfaces. Resolution: Removed corrosion from flap track bearing surfaces on tracks A,B,C and D IAW GlIB CPCM 20.50.01.Measured tracks A,B,C and D for thickness as required IAW Gulftream drawing SE05811901, with no defects noted. Performed brush cadmium plating repair to all exposed surfaces of flap tracks A,B,C and D [ASV Gulftream drawing SE05811901.Masked off flaps tracks A B C and D, washed with solvent and primed with 2012 primer, and applied topcoat IAW GAC CAMPS 4000. Billing Method Hours Rate Total Labor USD: Flat Rate $6,900.00 Total USD: $6,900.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoice.rpt Page I I of 98 Printed: 3/23/2012 4:28:32P) Flet X EFTA01080503  Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Step: 8.8.1 Completed Removed corrosion from flap track bearing surfaces on tracks A,B,C and D IAW GIIB CPCM 20-50-01. Step: 8.8.2 Completed Measure tracks A,B,C and Dfor remaining thickness. Step: 8.8.3 Completed Performed brush cadmium plating repair to all exposed surfaces of flap tracks A,B,C and D IMV Gulftream drawing SE05811901. Step: 8.8.4 Completed Cleaned and protected tracks and surounding area, masked-off track bearing surface, applied two coat epoxy primer 2012 and surface primer, Prep. tracks to top coat. IAW. CAMPS 4000. ( Written in ERROR this step belongs under item 8.7 ) Refer to squawk 8.7.4. Step: 8.8.5 Completed Masked off flaps tracks A B C and D, washed with solvent and printed with 2012 primer ready to spray paint. Discrepancy: 8.9 L/H wing wedge has 18 drilled off screw heads because rivnuts were spining. Resolution: Removed and replaced eighteen rivnuts on the UH wing wedge panel. Installed new rivnuts P/N GAN512B3-166 wet with sealant. Had to gain acess to fuel tank area to remove drilled out rivnuts All work done IAW G-IIB SRM 51.41.00. Billing Method Hours Rate Total Labor USD: Flat Rate $2,300.00 Pans USD: Time and Material $117.00 Total USD: $2,417.00 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.9#1 GAB511GA3-7 HI-BOLT I $2.06 $2.06 8.9 #2 PR1422-B-2 SEALANT, PRC, CARTRIDGE I $38.47 $38.47 8.9 #3 GAN512B3-166 BLIND NUT 25 $1.52 $38.00 8.9 #4 PR1422-B-2 SEALANT, PRC, CARTRIDGE I $38.47 $38.47 Step: 8.9.1 Completed Removed all spinning and bad rhnuts on IJH wing wedge IAW G-IIB MOM 51-40-00. Discrepancy: 8.10 Aileron trim tab has cracked skin in the area of the inner and outter hinges on the bottom side of the tab. Resolution: Trimmed aileron tab hinge skin areas as required IAW Gulfstream drawing SE35813107. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Total USD: $460.00 Discrepancy: 8.11 R/H elevator, top, inbd, hinge cover attach screw hole, heli-coil is bad. Resolution: Replaced bad R/H elevator, top, inbd, hinge cover attach screw hole, hell-coil with a new one JAW CAMPS 2212. Checks good. Billing Method Flours Rate Total Labor USD: Flat Rate $460.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelititinaryInvoicespt Page 12 of 98 Printed: 3/23/2012 4:28:32P) our X EFTA01080504  Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Total USD: $460.00 Discrepancy: 8.12 L/H elevator No.3 hinge, attach bolt bore is corroded. Resolution: Removed corrosion as required and remeasured L/H elevator No.3 hinge, attach bolt bore. Hole measurement is within limits. Work performed IAW GLIB MM 27-01-00. and SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Total USD: $460.00 Discrepancy: 8.13 R/H elevator, oubd top skin, has a spot of corrosion. Resolution: Removed light corrosion spot on R/H elevator outbd top skin, Sanded treated and primed top coat as required IAW GB' gamps 4000 Billing Method Hours Rate Total Labor USD: Flat Rate $345.00 Total USD: $345.00 Step: 8.13.1 Completed Removed and blend out light surface corrosion from the R/H elevator, upper surface Treated bare metal, and spot primer as required. IAN'. SRM.51-13-20. Discrepancy: 8.14 R/H wing upper sponson plate is corroded. Resolution: Mechanically removed corrosion from edges of the R/H upper sponson plate, Strip heavy paint for a better look IAW. GAC. 5E45802903. Removed all old sealant from around sponson plate. Treated and primed all bare metal. Resealed sponson plate. All work done IAW Standard Repair/Corrosion of Sponson Plates DWG No. 5E45802903 REV.D. Performed cadmium plating repair on R/H upper sponson plate. All work done IAW Standard Repair/Corrosion of Sponson Plates DWG No. SE45802903 REV.D Billing Method Hours Rate Total Labor USD: Time and Material ST 17.65 @ $115.00 $2,029.75 Labor USD: Time and Material OT 433 @ $173.00 $749.09 Services USD: Time and Material $400.00 Total USD: $3,178.84 Services: Ref. No. Description Quantity Sell Price USD Extended USD For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPrelintinaryInvoicespt Page 13 of 98 Printed: 3/23/2012 4:28:32P) Ftst X EFTA01080505  Bill To: HYPERION AIR, INC. WO It: SC10420 Invoice Number: 7112000954 Services: Ref. No. Description Quantity Sell Price USD Extended USD 8.14 #1 SERVICE I.00 $400.00 $400.00 Step: 8.14.1 Completed hlechanically removed corrosion front edges of the R/H upper sponson plate, Strip heavy paint for a better look JAW. GAC.SE,15802903. Step: 8.14.2 Completed Removed all old sealant front around sponson plate. Treated and primed all bare metal. Resealed sponson plate. All work done IAW Standard Repair/Corrosion of Sponson Plates DWG No. SE45802903 REV.D Step: 8.14.3 Completed Performed cadmium plating repair on R/H upper sponson plate. All work done IAW Standard Repair/Corrosion of Sponson Plates DWG No. 5E45802903 REV.!) Discrepancy: 8.15 R/H wing flap has 2 spots of corrosion. (Marked) Resolution: Removed light surface corrosion from R/H flap upper surface [outboard flap track &mid track]. Cleaned treated bare metal, primer and top coat as required. All work performed IAW. GAMPS 4000. Billing Method Hours Rate Total Labor USD: Flat Rate $1,150.00 Total USD: $1,150.00 Step: 8.15.1 Completed Removed and blend out light surface corrosion front the R/H Flap, upper surface around #4 track, Treated bare metal, and spot primer as required. IAN'. SRhl.51.13.20. Discrepancy: 8.16 R/H wing flap outbd Yoke is cracked in radius. Resolution: Removed damaged flap "C" track yoke assembly ( PN - 1159CM20621-3) and discarded. Installed a new replacement yoke assembly ( PN - 1159CM 20621-3) by reference of the Gulfstream IIB M/M chapter 27.06.00 entitled, Flap Actuator Yoke - Inspection. During this install, no defects were noted at this time. Billing Method Hours Rate Total Labor USD: Flat Rate $460.00 Pans USD: Time and Material $988.80 Total USD: $1,448.80 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.16 #2 I 159CM20621-3 YOKE ASSY, FLT CONT - FLAP $494.40 $494.40 DRIVE 8.16 #3 1159CM20621-3 YOKE ASSY, FLT CONT - FLAP $494.40 $494.40 DRIVE Step: 8.16.1 Completed Removed damaged flap "C" track yoke assembly ( PN I159CM20621.3) and discarded. Installed a new replacement yoke assembly ( PN - 1159CM 20621-3) by reference of the Gulfstreant IIB M/N1 chapter 27-06-00 entitled, Flap Actuator Yoke •