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Gu]£stream' PRELIMINARY INVOICE A OSSISIMIL DYNAMICS COMPANY Bldg C. - West Palm Beach, Florida 33406 ParUModel SIN: Mail Remittance To: Gulfstream Aerospace Corporation Box 730349 Dallas, Texas 75373-0349 Overnight Remittance To: Gulfstream Aerospace Corporation (Box 0 730349) do JP Morgan Chase Bank, NA ATTN: Dallas National Wholesale Lockbox TX l-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 Fedwire Routing No. (ABA) 021 000 021 S.W.I.F.T. CIIASUS33 ACI1 Credit Routing No. (ABA)071 000013 Bill To: JEGE LLC C/O GALAXY AVIATION INC MTN: LARRY VISOSKI 3800 SOUTHERN BLVD, SUITE 204 WEST PALM BEACH, Florida 33406 United States Title: JEGE LLC (Rolls Royce Fan Balance) Invoice Number: Invoice Date: Customer ID: Number: Repair Station: In Date: Out Date: Payment Type: Payment Terms: 7115002405 8/19/2015 BJ419 FAA CRS PB8R624N 08/03/2015 08/09/2015 COD - Certified Check INVOICE SUMMARY FOR WORK ORDER NUMBER: Time & Materials SC17734 Flat Rate Total Labor USD: $14,227.81 $0.00 $14,227.81 Parts USD: S354.72 $0.00 $354.72 Detail Subtotal USD: $14,582.53 $0.00 $14,582.53 Subtotal USD: $14,582.53 Funds on Deposit USD: $0.00 Total USD: $14,582.53 Customer on the following programs:MSP(APU) HAPP and Corp care 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 2011 Page I of 3 Printed: 8/19/2015 1:18:19P? Rot EFTA00704739 Bill To: JEGE LLC WO It SC17734 Invoice Number: 7115002405 Item: 2 Engine Team Manager: Sean Brown Customer Coordinator: Benny Rios Part/Model #: SM: TSN/TSO: 8967.4 CSN/CSO: 4129 Aircraft Time: Discrepancy: 2.1 Assist Rolls Royce with LH fan clocking 180, to include fan trim balance test#9 Resolution: Repositioned the No. 1 engine fan blades approximately 180 degrees from original position as required. Work performed IAW TAY -611-8 MM 72-31-12. REF Items 2.2 thru 2.25 for actual work performed and present location of each blade. Performed Rolls Royce Test No. 9 Trim Balance of the No. 1 engine LP Compressor Fan Blades IAW RR Tay-611-8 EMM 71-00.00-700-012-B02. Added balance weights as required. 9.5g at Pos. 7, 9.5g at Pos. 10, 9.5g at Pos12. REF Trim Balance sheet provided by Rolls Royce. Billing Method Hours Rate Total Labor USD: Time and Material ST 58.34 ® $127.00 $7,409.18 Labor USD: Time and Material OT 22.37 ® $127.00 $2,840.99 Total USD: 810,250.17 Step: 2.1.1 Completed Repositioned the No. 1 engine fan blades approximately 180 degrees as required. Work performed IAW TAY -611-8 MM 72-31-12. REF Items 2.2 thru 2.25 for actual work performed. Step: 2.1.2 Completed Performed Rolls Royce Test No. 9 Trio, Balance of the No. 1 engine LP Compressor Fan Blades IAW RR Tay-61I-8 EMM 71.1111-011-700.012-B02. Added balance weights as required. 9.5g at Pos. 7, 9.5g at Pos. 10, 9.5g at Pos12. REF Trim Balance sheet provided by Rolls Royce. Item: 3 Engine Team Manager: Sean Brown Customer Coordinator: Benny Rios PartfModel 0: S/61: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 3.1 R/H engine - While removing #10 fan ring bolt, found threaded insert threads damaged. Removed threaded insert and bolt per Rolls Royce rep. Parts ordered under item 2.1. Resolution: Removed bad nut P/N AS27870 and installed a NEW nut P/N AS27870 IAW RR Tay-611-8 EMM 70-42-09 Billing Method Routs Rate Total Labor USD: Time and Material ST 2.50 kr $127.00 $317.50 Parts USD: Time and Material $354.72 Total USD: $672.22 Parts: Ret No. Part number: Description Quantity Sell price USD Extended USD 3.1 #1 AS27870 NUT 3 $83.84 $251.52 3.1 #2 AS2I125 BOLT 3 $34.40 $103.20 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_WorkOrderPreliminaryInvoice.rpt 2011 Page 2 of 3 Printed: 8/19/2015 1:18:19PI Rot EFTA00704740 Bill To: JEGE LLC WO #: SC17734 Invoice Number: 7115002405 Discrepancy: 3.2 With Assistance from Rolls Royce perform fan dynamic trim balance test#9 Resolution: Complied wth Rolls Royce Dynamic Trim Balance test #9. Please see Rolls Royce Form T1-011-8 for details. All ssork In accordance with RRTAY611-8EMM 71-00-00-700-013-B02TEST No-9 Billing Method Flours Rate Total Labor USD: Time and Material ST 23.92 @ $127.00 53,037.84 Labor USD: Time and Material OT 4.90 @ $127.00 $622.30 Total USD: $3,660.14 Communications concerning disputed debts, including a check or other instrument tendered as full satisfaction of a debt, must be forwarded to: Gulfstream Aerospace Atm: Credit Manager M/S B-05 PO BOX 2206, Savannah, GA 31402 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliininaryInvoice.rpt 2011 Page 3 of 3 Printed: 8/19/2015 1:18:19P1 Rot EFTA00704741