EFTA00652198.pdf

Gulfstreame A NNN OVNAMICA COMPANY Part/Model #: INVOICE AC Serial No/Tail No.: 7 Char Drive - Westfield. Massachusetts 01085-1493 Mail Remittance To: Overnight Remittance To: Wire Remittance To: Gu'lantern Aerospace Corporation Gulfstream Aerospace Corporation (Box /I 730349) Gulfstrcam Aerospace Corporation P.O. Box 730349 do JP Morgan Chase Bank. NA JP Morgan Chase Bank, NA Dallas, Texas 75373-0349 ATTN: Dallas National Wholesale Lockbox TXI-0029 Chicago, IL 60670 14800 Frye Road Account No. 10-15825 Ft. Won't TX 76155 Fedwire Routing No. S.W.I.F.T. CHASUS33 ACH Credit Routing No. Invoice Number: 6916001251 Bill To: HYPERION AIR, INC. Invoice Date: 41812016 3800 SOUTHERN BLVD Customer ID: CH200 SUITE 204 P.O. Number: WEST PALM BEACH, Florida 33406 Repair Station: CRS LECR039G United States In Date: 03/05/2016 Out Date: 03/25/2016 Payment Type: Net 30-Open terms Payment Terms: Title: HYPERION AIR, INC. INVOICE SUMMARY FOR WORK ORDER NUMBER: SC13577 Time & Materials Flat Rate Total Labor USD: 523,752.08 50.00 523,752.08 Pans USD: 510,546.36 50.00 510,546.36 Services USD: 513,050.98 50.00 513.050.98 Detail Subtotal USD: $47,349.42 50.00 S47.349.42 Subtotal USD: $47,349.42 Funds on Deposit USD: 50.00 Total USD: $47,349.42 SCHEDULED MAINTENANCE FAR PART 91 LARRY VISOSKI 917-868-6145 N2I2JE RE: PROPOSAL# 7024273 1201 (GAC1015-2422-GIV-)085-R01) 7024691 ROO (GACO216-4691-GIV-)085-120D) HAPP # 4400-529-21 For detail description of the work complied with see the Work Order Detail report. Westfield_GAC_Work Unless otherwise indicated, all financial values listed in this document am in US Dollars (USD). Printed: 4(9/2016 4:26:50AM OrderInvoice.rpt Page 1 of 14 LS MO EFTA00652198  Bill To: IIYPERION AIR, INC. WO #: SCI3577 Invoice Number: 6916001251 Item: 6 AVIONICS Team Manager: Charles Helwig Pan/Model #: Customer Coordinator: Vinny Cicala AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 6.1 CUSTOMER REPORTS #1 TRANSPONDER LOOSES ATC ALTITUDE READ OUT AFTER ONE HOUR. Resolution: UNSEATED ATC NO.1 PN: 622-9210-409 SN: 2376. PERFORMED VISUAL INSPECTION OF BOTII THE RACK AND COMPONENT INSURING NO BENT OR PUSH PINS ARE PRESENT. CLEANED CONTACTS AND RESEATED ATC NO.1 PN: 622-9210-409 SN: 2376. DISCONNECTED INTERCONNECT FOR ATC NO.1 AND FOUND MALE PINS S AND T TO BE BENT AND MAKING LIMITED CONTACT WITH FEMALE PINS. WORK PERFORMED IN ACCORDANCE WITH WIRING DIAGRAM 1159SB41481, GIV AMM 34-02-04 AND GIV WIRING DIAGRAM 34-55-00. REMOVED ATC NO.2 P/N:622-9210-409 SIN: 1G8hil. UNSECURED ATC RACKS TO FACILITATE MAINTENANCE. REPLACED ATC NO.1 DISCONNECT CONNECTORS P/N: MS3120F22-55P SN: UNK AND P/N: M53126F22-55S SN: UNK, RECEIVED P/N: MS3120F22-55P FROM ELECTRO ENTERPRISE REFERENCE CERTIFICATE OF CONFORMANCE ON PACKSLIP NO: 1779462 DATED 03/14/2016. RECEIVED P/N:MS3126F22-55S FROM ELECTRO ENTERPRISES REFERENCE CERTIFICATE OF CONFORMANCE WITH INVOICE NO: 1156087 DATED 05/25/11. PERFORMED WIRING RING OUT CHECK OF ATC NO.1 TRANSPONDER LAW WESTERN COMMANDER WIRING DWG NO:08069197, FOUND GOOD. REINSTALLED SERVICEABLE ATC NO.1 PN: 622-9210-409 SN: 2376 AND SERVICEABLE ATC NO.2 P/N:622-9210-409 SIN: 1G88/1 AND PERFORMED ATC FUNCTIONAL CHECKS IN ACCORDANCE WITII GIV AMM 34-02-04. NOTED NO FURTIIER ISSUES AT TIIIS TIME. SEE STEPS FOR DETAILS. Billing Method Hours Rate Total Labor USD: Time and Material ST 39.91 ® $132.00 $5,268.12 Parts USD: Time and Material $211.08 Total USD: $5,479.20 Parts: Ref. No. Pan number Description Quantity Sell price USD Extended USD 6.1 #1 hIS3120F22-55P CONNECTOR 1 $95.68 595.68 6.1 #2 hIS3126F22-55S CONNECTOR 1 $8536 585.36 6.1 #3 686DM3 SLEEVE. BRAIDED 1/2 BLACK 2 53.92 $7.84 EXPANDO 6.1 #4 SPT.50 SPIRAL WRAP TEFLON 1/2" 2 53.30 56.60 NATURAL 6.1 #5 TY25M TYRAP, WHITE 10 50.78 57.80 6.1 #6 TY242M TIE, CABLE; NYLON 8.19 IN.; 0.14 10 50.78 57.80 IN.; 30 LB. TENSILE STRENGTH For detail description of the work complied with see the Work Order Detail report. Westfield_GAC_Work Unless otherwise indicated, all financial values listed in this document am in US Dollars (USD). Printed: 49/2016 4:26:50AM OrderInvoice.rpt Page 2 of 14 LS MO EFTA00652199  Bill To: HYPERION AIR, INC. WO #: SCI3577 Invoice Number: 6916001251 Step: 6.1.1 Completed APPLIED POWER TO AIRCRAFT. MONITORED ALTITUDE REPORTING ON BOTH ATC TRANSPONDERS USING ATC 600 TEST SET FOUND GOOD. LET IT RUN FOR A LONG TIME, WHILE PERFORMING ASCB BUS SWEEP (REF. SQUAWK 63), FOUND GOOD AT THIS TIME. WORK WAS DONE REFERENCE GIV A.,M.M. 34-02-04. Step: 6.1.2 Completed UNSEATED ATC NO.1 PN: 622-9210-409 SN: 2376. PERFORMED VISUAL INSPECTION OF BOTH RACK AND COMPONENT INSURING NO BENT OR PUSH PINS ARE PRESENT. CLEANED CONTACTORS AND RESEATED ATC NO.1 PN: 622-9210-409 SN: 2376. GAINED ACCESS TO AND DISCONNECTED INTERCONNECT FOR ATC NO.1 AND FOUND MALE PINS S AND T TO BE BENT AND MAKING LIMITED CONTACT WITH FEMALE PINS. STRAIGHTENED PINS AND RECONNECTED DISCONNECT. APPLIED POWER TO AIRCRAFT AND PERFORMED MULTIPLE CHECKS OF ATC SYSTEM USING IF'R 6000. NOTED NO OCCURENCES OF TRANSPONDER FAILING TO REPORT ALTITUDE. ALL WORK PERFORMED IN ACCORDANCE WITH GIV AMM 34-02-04 AND WIRING DIAGRAM I159:O341481. Step: 6.13 Completed STEP ENTERED IN ERROR Step: 6.1.4 Completed CONDUCTED RESEARCH TO FIND PART NUMBER FOR ATC TRANSPONDER INTERCONNECT CANNON PLUG PART NO. PART NUMBER FOR RECEPTACLE IS MS3120F22-55P PART NUMBER FOR PLUG IS MS3126F122-555. REFERENCE WESTERN COMMANDER DRAWING NO. 08069197. TITLED NO. 1 TRANSPONDER (MOD) NO REV, DATED 5/12/89. THIS CONNECTOR CONTAINS VARIOUS 429 DATA INPUTS/OUTPUTS FOR CONTROL AND TUNING, SUPPRESSION SIGNALS AND TCAS INTERFACE. AND POWER. ALL WORK PERFORMED IN ACCORDANCE WITH WESTERN COMMANDER DRAWING NO. 08069197, TITLED NO. I TRANSPONDER (MOD) NO REV, DATED 5/12189 Step: 6.1.5 Completed REMOVED ATC NO.2 P1N:622-9210-409 S/N: IG/thl. UNSECURED ATC RACKS TO FASCILITATE MAINTENANCE. REMOVED ATC NO.1 DISCONNECT CONNECTORS P/N: ItelS3120F22-55P SN: UNK AND P/N: MS3126F22-55S SN: UNK. INSTALLED NEW CONNECTORS P/N: MS3120F22-55P SN: UNK AND P/N: MS3126F22-555 SN: UNK. RECEIVED P/N: MS3120F22-55P FROM ELECTRO ENTERPRISE REFERENCE CERTIFICATE OF CONFORMANCE ON PACKSLIP NO: 1779462 DATED 03/14/2016. RECEIVED P/N:MS3126F22-55S FROM ELECTRO ENTERPRISES REFERENCE CERTIFICATE OF CONFORMANCE WITH INVOICE NO: 1156087 DATED 05/25/11. ALL WORK PERFORMED IN ACCORDANCE WITH WIRING DIAGRAM 1159SB41481.GIV AMM 34-02-04 AND GIV WIRING DIAGRAM 34-55-00. Step: 6.1.6 Completed PERFORMED WIRING RING OUT CHECK OF ATC NO.1 TRANSPONDER IAW WESTERN COMMANDER WIRING DWG NO:08069197 FOUND GOOD. Discrepancy: 6.2 CUSTOMER REQUEST TO EXCHANGE THE #2 COM STICKY COM SELECTOR TO CHANGE FREQUENCY. Resolution: APPLIED POWER AIRCRAFT, CHECKED OPERATION OF NO.2 RADIO TUNING UNIT (RTU), SQUAWK CONFIRMED, FOUND LINE SELECT KEY (1R) IS INTERMITTENT (STICKY) TO CHANGE FREQUENCY. REMOVED RTU NO:2 P/N:822-0836-035 SIN: 267 FOR REPAIR. RECEIVED OK TO INSTALL AND INSTALLED REPAIRED RTU NO:2 P/N:822-0836-035 SIN: 267 IN ACCORDANCE WITH GIV CMP 232336. RECEIVED UNIT FROM ROCKWELL COLLINS REFERENCE 8130-3 WITH FORM TRACKING NO: 105121875 WORK ORDER: WEP016-01211 CERT: ED7Y210Y DATED 16MAR2016. PERFORMED VIIF COMMUNICATIONS SYSTEM - OPERATIONAL CHECK IN ACCORDANCE WITH GIV AMM 23-01-00,MARKER BEACON SYSTEM - OPERATIONAL CHECK IN ACCORDANCE WITH GIV AMM 34-02-02, NAVIGATION / DISTANCE MEASURING EQUIPMENT SYSTEMS - OPERATIONAL CHECK IN ACCORDANCE WITH GIV AMM 34-02-02, AUTOMATIC DIRECTION FINDING SYSTEM - OPERATIONAL CHECK IN ACCORDANCE WITH GIV AMM 34-02-01 Billing Method Hours Rate Total Labor USD: Time and Material ST 8.23 ® S132.00 $1,08636 Services USD: Time and Material S8,572.23 Total USD: 49,658.59 Services: Ref. No. Description Quantity Sell Price USD Extended USD For detail description of the work complied with see the Work Order Detail report. Westficld_GAC_Work Unless otherwise indicated, all financial values listed in this document am in US Dollars (USD). Printed: 4(912016 4:26:50AM Orderinvoice.rpt Page 3 of 14 LS MO EFTA00652200  Bill To: HYPERION AIR, INC. WO #: SCI3577 Invoice Number: 6916001251 Services: Ref. No. Description Quantity Sell Price USD Extended USD 6.2 #2 GAC REPAIRS 1.00 58,57223 58,572.23 Part Ref: 822-0836-035 RTU-4200 (RADIO TUNING UNIT) 62#1 GAC REPAIRS 1.00 50.00 S0.00 Step: 6.2.1 Completed APPLIED POWER AIRCRAFT, CHECKED OPERATION OF NO.2 RADIO TUNING UNIT (RTU), SQUAWK CONFIRMED. FOUND LINE SELECT KEY (1R) IS INTERMITTENT (STICKY) TO CHANGE FREQUENCY. NEED TO REPLACED OR SEND FOR REPAIR RTU NO.2. Discrepancy: 6.3 CUSTOMER REPORTS THE #2 IIF RADIO WILL NOT TUNE ("CP" AND "RT" LIGHT ILLUMINATES). Resolution: GAINED ACCESS ON TAIL COMPARTMENT, VISUALLY INSPECTED THE IIF COUPLERS AND IIF TRANSCEIVERS, FOUND THE RF COAX CONNECTOR ON IIF COUPLER NO.2 IS LOOSE. SECURED COAX CONNECTOR ON IIF COUPLER NO.2. PERFORMED HIGH FREQUENCY COMMUNICATION SYSTEMS NO. 1 AND NO.2 - OPERATIONAL TEST, CHECKED GOOD ON BOTH SYTEM. RF RADIO CHECKS CONDUCTED WITH NY RADIO WITH TXJRX QUALITY 4X4. WORK DONE IAW GULFSTREAM GIV MM ATA 23-03-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 4.48 ® $132.00 559136 Total USD: 5591.36 Step: 6.3.1 Completed APPLIED POWER TO AIRCRAFT, PERFORMED HF NO. I AND NO.2 SYSTEM OPERATIONAL TEST, FOUND NO.2 HF SYSTEM WITH "CP" LIGHT ILLUMINATED AND WITH FAULT 08. ASKED CUSTOMER ABOUT THE HF SQUAWK DUE TO HF SYSTEM NO. I IS THE ONE FAILED ON THE ITEM. PER CUSTOMER. HE IS NOT SURE WHAT SYSTEM IS FAILING. GAIN ACCESS ON TAIL COMPARTMENT, VISUALLY INSPECTED THE HF COUPLERS AND HF TRANSCEIVERS, FOUND THE RF COAX CONNECTOR ON HF COUPLER NO.2 IS LOOSE. SECURED COAX CONNECTOR ON HF COUPLER NO.2. PERFORMED HIGH FREQUENCY COMMUNICATION SYSTEMS NO. I AND NO. 2 - OPERATIONAL TEST, CHECKED GOOD ON BOTH SYTEM. WORK DONE IAW GULFSTREAM GIV MM ATA 23-03-00. Step: 6.3.2 Completed USING 0-IS PSIG PRESSURE GAUGE, CHECKED THE PRESSURE IN BOTH NO. 1 AND NO.2 HF COUPLERS. NO. 1 COUPLER WAS AT 7 PSI AND NO. 2 COUPLER WAS AT APPX. 6.75 PSI. BOTH OF THESE READINGS ARE WITHIN ALLOWABLE PRESSURES AS PER GIV A.M.M. 23-03-00, HIGH FREQUENCY COMMUNICATION COUPLER - SERVICING. Discrepancy: 6.4 CUSTOMER REPORTS THE FMS SELECTOR SWITCH NEEDS TO BE CHANGED (1/2 FMS SELECTOR ON CENTER PEDESTAL). Resolution: CONFIRMED CENTER FMS SELECTOR WILL ONLY BRIEFLY ILLUMINATE 1/2 FMS. REMOVED AND CAPSULE AND REMOVED 4 EA. DEFECTIVE LAMPS P/N OL-3335, NO SERIAL NOS. REPLACED WITH 4 EA NEW LAMPS P/N: 01.-3335 FROM GAC WESTFIELD STOCK. PERFORMED OPERATIONAL CHECK OF SWITCHES IN ACCORDANCE WITH GIV AMM 33-01-00 ANNUNCIATOR LIGHT -OPERATIONAL TEST, WITH NO DISCREPANCIES. Billing Method Hours Rate Total Labor USD: Time and Material ST 6.71 ® 5132.00 5885.72 Pans USD: Time and Material 5360.50 Total USD: 41,246.22 For detail description of the work complied with see the Work Order Detail report. Westfield_GAC_Work Unless otherwise indicated, all financial values listed in this document am in US Dollars (USD). Printed: 49/2016 4:26:50AM OrderInvoice.rpt Page 4 of 14 LS MO EFTA00652201  Bill To: HYPERION AIR, INC. WO #: SC13577 Invoice Number: 6916001251 Parts: Ref. No. Part number Description Quantity Sell price USD Extended USD 6.4 #1 OL3335 LAMP 4 $5.15 $20.60 6.1#2 99-212 SWITCH $339.90 $339.90 Step: 6.4.1 Completed GAINED ACCES TO THE FMS SELECTOR SWITCH (1/2 FMS) ON PEDESTAL. REMOVED DEFECTIVE SWITCH (1/2 FMS) P/N: 99-212 FROM ASSEMBLY. RECEIVED OK TO INSTALL AND INSTALLED A NEW SWITCH P/N: 99-212 THAT WAS RECEIVED FROM GAC-SAVANNAH WITH SHIPMENT NO.: SASH316-34302, ENTERPRISE TRANSFER NO.: 000663760, DATED 03/08/2016 TO THE (1/2 FMS) SWITCH POSITION ON ASSEMBLY. SECURED SWITCH ASSEMBLY TO PEDESTAL WORK WAS DONE WITH REFERENCE TO THE JET CENTER DRAWING NO. 08069100, TITLED NO. 3 FMS, DATED 3-11-88. Step: 6.4.2 Completed PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH GIV AMM 33-01-00 ANNUNCIATOR LIGHTS - OPERATIONAL TEST, WITH NO DISCREPANCIES. Discrepancy: 6.5 CUSTOMER REQUESTS ASCB SWEEP Resolution: PERFORMED ASCB BUS SWEEP IAW GIV 31-02-00. FOUND THAT THERE WERE NUMEROUS BUS COUPLER CONNECTIONS THAT REQUIRED CLEANING (NOTICED SIGNAL FLUCTUATION ON OSCILLOSCOPE). CLEANED BUS COUPLER CONNECTIONS AS REQUIRED AND SECURED ALL CONNECTIONS. PERFORMED OPS CIIECK AND FINAL ASCB BUS SWEEP IN ACCORDANCE WITII GIV AMM 31-02-00 AVIONICS STANDARD COMMUNICATION BUS - FAULT ISOLATION WITH NO DISCREPANCIES. Billing Method Hours Rate Total Labor USD: Time and Material ST 13.00 ® $132.00 31,716.00 Total USD: 41,716.00 Step: 6.5.1 Completed PERFORMED ASCB BUS SWEEP 1AW GIV A.M.M. 31-02-00. FOUND THAT THERE WERE NUMEROUS BUS COUPLER CONNECTIONS THAT REQUIRED CLEANING (NOTICED SIGNAL FLUCTUATION ON OSCILLOSCOPE). CLEANED BUS COUPLER CONNECTIONS AS REQUIRED AND SECURED ALL CONNECTIONS. CHECKED ASCB BUS CHANNELS A AND B, FOUND GOOD AT THIS TIME. Discrepancy: 6.7 WHILE PERFORMING SPZ-8000 CND MAINTENANCE TEST NOTICED THAT TFIE LEFT FUEL LOW LEVEL INDICATION STAYS WHITE IN ECIAS AND NO LIGHT ON STANDBY FUEL INDICATION WITII ZERO FUEL ON WING. Resolution: PERFORMED RESISTANCE CIIECK OF THE LEFT WING LOW LEVEL SENSOR AND FOUND TIIAT IT WAS WITHIN LIMITS. WITH BOTH EICAS AND STANDBY FUEL QUANTITY INDICATOR SHOWING NO LOW LEVEL WARNING, WITII ZERO FUEL ON TIIE LEFT WING. AT CONNECTOR 15A1P1, SWAPPED PINS C (CLOSE DRY LEFT SIGNAL) WITII PIN D (CLOSE DRY RIGHT SIGNAL), AND THE PROBLEM FOLLOWED. SWAPPED BOTII PINS BACK TO THEIR ORIGINAL POSITIONS. CONFIRMED BAD FUEL LOW LEVEL DUAL CONTROL UNIT. REMOVED FUEL QUANTITY DUAL LOW LEVEL CONTROL UNIT PIN: 1159SCF215-33, SIN: 567 FROM THE AIRCRAFT. RECEIVED OK TO INSTALL AND INSTALLED A REPAIRED FUEL QUANTITY DUAL LOW LEVEL CONTROL UNIT PIN: 1159SCF215-33,S/N: 690 THAT WAS RECEIVED FROM PARKER HANNIFIN CORP., ELECTRONICS SYSTEMS DIV. WITII FAA 8130-3 FORM TRACKING NO.: 9E5210, APPROVAL / CERTIFICATE NO.: FX1R156IC, DATED AUG/23/2010 TO THE AIRCRAFT. APPLIED POWER TO TFIE AIRCRAFT AND FOUND THAT THE LEFT, RIGHT, AND TOTAL FUEL LEVEL INDICATION WAS AMBER ON EICAS, ALSO THERE WAS LIGHT, (LEFT AND RIGHT) ON STANDBY FUEL INDICATOR. WORK WAS DONE IAN' GIV CMP 284020, FUEL QUANTITY DUAL LOW LEVEL CONTROL UNIT - REMOVAL / INSTALLATION. COMPLIED WITII GIV CMP 284029 FUEL LOW LEVEL WARNING SYSTEM - OPERAIONAL TEST WITII NO DISCREPANCIES. For detail description of the work complied with see the Work Order Detail report. Westfield_GAC_Work Unless otherwise indicated, all financial values listed in this document am in US Dollars (USD). Printed: 4(912016 4:26:50AM OrderInvoice.rpt Page 5 of 14 LS MO EFTA00652202  Bill To: HYPERION AIR, INC. WO #: SCI3577 Invoice Number: 6916001251 Billing Method Hours Rate Total Labor USD: Time and Material ST 12.98 ® $132.00 31,713.36 Pans USD: Time and Material $4,737.00 Total USD: $6,450.36 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 6.7 #1 1159SCF215-33 CONTROL UNIT. FUEL, LOW LEVEL 1 $4,737.00 $4,737.00 Step: 6.7.1 Completed PERFORMED RESISTANCE CHECK OF THE LEFT WING LOW LEVEL SENSOR AND FOUND THAT IT WAS WITHIN LIMITS. WITH BOTH EICAS AND STANDBY FUEL QUANTITY INDICATOR SHOWING NO LOW LEVEL WARNING, WITH ZERO FUEL ON THE LEFT WING. AT CONNECTOR 15A1P1, SWAPPED PINS C (CLOSE DRY LEFT SIGNAL) WITH PIN D (CLOSE. DRY RIGHT SIGNAL), AND THE PROBLEM FOLLOWED. SWAPPED BOTH PINS BACK TO THEIR ORIGINAL POSITIONS. CONFIRMED BAD FUEL LOW LEVEL DUAL CONTROL UNIT. ALL WORK WAS DONE WITH REFERENCE TO GIV A.M.M. 28-07-00. Step: 6.7.2 Completed REMOVED FUEL QUANTITY DUAL LOW LEVEL CONTROL UNIT PIN: 1159SCF215-33, S/N: 567 FROM THE AIRCRAFT. RECEIVED OK TO INSTALL AND INSTALLED A REPAIRED FUEL QUANTITY DUAL LOW LEVEL CONTROL UNIT PEN: 1159SCF215-33, S/N: 690 THAT WAS RECEIVED FROM PARKER HANNIFIN CORP., ELECTRONICS SYSTEMS DIV. WITH FAA 8130-3 FORM TRACKING NO.: 9E5210. APPROVAL / CERTIFICATE NO.: F7C1R156K, DATED AUG/23/2010 TO THE AIRCRAFT. APPLIED POWER TO THE AIRCRAFT AND FOUND THAT THE LEFT, RIGHT, AND TOTAL FUEL LEVEL INDICATION WAS AMBER ON EICAS, ALSO THERE WAS LIGHT, (LEFT AND RIGHT) ON STANDBY FUEL INDICATOR. WORK WAS DONE TAW G1V CMP 284020, FUEL QUANTITY DUAL LOW LEVEL CONTROL UNIT - REMOVAL / INSTALLATION. Step: 6.7.3 Completed COMPLIED WITH GIV CMP 284029 FUEL LOW LEVEL WARNING SYSTEM - OPERAIONAL TEST WITH NO DISCREPANCIES. Discrepancy: 6.8 DURING OW CMP GIV 541019 PYLON INTERNAL (LEFT) - INSPECTION FOUND PRECOOLER INLET TEMPERATURE SENSOR CANNON PLUG TO HAVE BROKEN WIRE. Resolution: REMOVED AND REPLACED CONNECTOR LEFT ENGINE PYLON TEMP SENSOR P/N 3153106F12S-35 NEW FROM ELECTRO ENTERPRISES INC ., WITH CERTIFICATE OF CONFORMANCE, PACK SLIP NO. 1781911 DATED MAR 18, 2016. PERFORMED OPS CHECK WITH NO DISCREPANCIES. WORK DONE TAW WESTERN COMMANDER , INC . WIRING DIAGRAM NO. 08030131 - BLEED AIR CONTROL MONITOR, DATED 2/10/89. Billing Method Hours Rate Total Labor USD: Time and Material ST 8.14 ® $132.00 $1,074.48 Pans USD: Time and Material $27.90 Total USD: $1,102.38 Pans: Ref. No. Pan number Description Quantity Sell price USD Extended USD 6.8#1 NIS3106F12S-35 CONNECTOR 527.90 $27.90 For detail description of the work complied with see the Work Order Detail report. Westficld_OAC_Work Unless otherwise indicated, all financial values listed in this document am in US Dollars (USD). Printed: 49/2016 4:26:50AM OrderInvoice.rpt Page 6 of 14 LS MO EFTA00652203  Bill To: HYPERION AIR, INC. WO #: SC13577 Invoice Number: 6916001251 Step: 6.8.1 Completed REMOVED AND REPLACED CONNECTOR LEFT ENGINE PYLON TEMP SENSOR P/N MS3106F12S-35 NEW FROM ELECTRO ENTERPRISES INC., WITH CERTIFICATE OF CONFORMANCE, PACK SLIP NO. 1781911 DATED MAR 18, 2016. WORK DONE JAW WESTERN COMMANDER , INC. WIRING DIAGRAM NO. 08030131 - BLEED AIR CONTROL MONITOR, DATED 2/10189. Step: 6.8.2 Completed PERFORMED OPS CHECK IN ACCORDANCE WITH WESTERN COMMANDER, INC. WIRING DIAGRAM NO. 08030B1 - BLEED AIR CONTROL MONITOR. DATED 2/10/89. Discrepancy: 6.9 DURING AIRCRAFT POWER "ON", FOUND DC VOLTS ON ELECTRICAL POWER MONITOR TO READ 8.2 VOLTS WHEN SWITCH IS SET TO "AUX" Resolution: APPLIED POWER TO AIRCRAFT AND OBSERVED 8.2 VOLTS DC DISPLAYED IN TILE POWER MONITOR WITH AUX SELECTED. NOTED ALSO THAT IT WOULD ERRATICALLY JUMP FROM Si VOLTS TO 48.2 VOLTS TO 88.2 VOLTS AND BACK TO 8.2 VOLTS. WHEN SELECTING RADIO MASTER TO ON 28 VOLTS IS DISPLAYED ON THE MONITOR WITH AUX SELECTED. CAN ALSO GET 28 VOLTS TO BE DISPLAYED BY SELECTING THE PILOT, EICAS, AND COPILOT DISPLAYS TO ON. WHEN SELECTED BACK TO OFF, Si VOLTS IS DISPLAYED ON TIIE MONITOR AGAIN. CHECKED DC ESS TEST POINT ON PILOT CIRCUIT BREAKER PANEL AND READ 28 VOLTS WHILE POWER MONITOR STILL READ 8.2 VOLTS. ALL WORK PERFORMED IN ACCORDANCE WITH GIV WIRING DIAGRAM MANUAL 24-30-00 DC POWER SUPPLY SYSTEM. CUSTOMER HAS INDICATED TIIAT TIIIS IS A KNOWN ISSUE, AND THAT IT EXISTS IN NO CONFIGURATION OTHER THAN AUX. CUSTOMER ELECTS NO FURTHER ACTION AT THIS TIME. Billing Method Hours Rate Total Labor USD: Time and Material ST 7.76 ® 5132.00 51,024.32 Total USD: 51,024.32 Step: 6.9.1 Completed APPLIED POWER TO AIRCRAFT AND OBSERVED 8.2 VOLTS DC DISPLAYED IN THE POWER MONITOR WITH AUX SELECTED. NOTED ALSO THAT IT WOULD ERRATICALLY JUMP FROM 8.2 VOLTS TO 48.2 VOLTS TO 88.2 VOLTS AND BACK TO 8.2 VOLTS. WHEN SELECTING RADIO MASTER TO ON 23 VOLTS IS DISPLAYED ON THE MONITOR WITH AUX SELECTED. CAN ALSO GET 28 VOLTS TO BE DISPLAYED BY SELECTING THE PILOT, EICAS, AND COPILOT DISPLAYS TO ON. WHEN SELECTED BACK TO OFF, 8.2 VOLTS IS DISPLAYED ON THE MONITOR AGAIN. AFTER POWER WAS ON FOR ABOUT AN HOUR THE SAME 8.2 VOLT INDICATION COULD BE SEEN ON THE POWER MONITOR BUT THIS TIME WITH EITHER AUX OR ESSENTIAL SELECTED. CHECKED DC ESS TEST POINT ON PILOT CIRCUIT BREAKER PANEL AND READ 28 VOLTS WHILE POWER MONITOR STILL READ 8.2 VOLTS. ALL WORK PERFORMED IN ACCORDANCE WITH GIV WIRING DIAGRAM MANUAL 24-30-00 DC POWER SUPPLY SYSTEM. Step: 6.9.2 Completed GAINED ACCESS TO CONNECTORS 318A1A5P2 AND 318A1A5P3 BY REMOVING THE COCKPIT ENTRYWAY CENTER HEADLINER. DISCONNECTED 318A1A5P2 AND BACKPINNED PIN "BB". APPLIED POWER TO AIRCRAFT. WHILE MONITORING ELECTRICAL POWER MONITOR PANEL -AUX PWR SW SELECTED, FOUND THAT DC VOLTAGE INDICATION WOULD FLUCTUATE BETWEEN 8.2, 48.2, AND 88.2 VD( INTERMITTENTLY WHILE INPUT VOLTAGE AT PINN BB OF CONNECTOR 318A1A5P2 PIN BB SHOWS STEADY 14.7 VOLTS DC. CONNECTED 318A1A5P2. DISCONNECTED 318A1A5P3 AND BACKPINNED PIN "BB". APPLIED POWER TO AIRCRAFT. WHILE MONITORING ELECTRICAL POWER MONITOR PANEL WITH ESS PWR SW SELECTED, AGAIN FOUND THAT DC VOLTAGE INDICATION WOULD FLUCTUATE BETWEEN 8.2.48.2. AND 88.2 VDC INTERMITTENTLY WHILE THE INPUT VOLTAGE AT PIN ^BB^ OF CONNECTOR 318A1A5P3 SHOWS A STEADY VOLTAGE READING. SECURED CONNECTOR 318A1A5P3. SECURED COCKPIT ENTRYWAY CENTER HEADLINER. CONFIRMED BAD EPMP. WORK WAS DONE WITH REFERENCE TO GIV A.M.M. 24-02-00. DC ELECTRICAL POWER - ELECTRICAL SCHEMATIC. Discrepancy: 6.10 PILOTS WIPER MOTOR ONLY OPERATES AT LOW SPEED. For detail description of the work complied with see the Work Order Detail report. Westfield GAC Work Unless otherwise indicated, all financial values listed in this document am in US Dollars (USD). Printed: 4(912016 4:26:50AM OrderInvoice.rpt Page 7 of 14 LS MO EFTA00652204  Bill To: HYPERION AIR, INC. WO #: SCI3577 Invoice Number: 6916001251 Resolution: APPLIED POWER TO AIRCRAFT AND CHECKED FOR PROPER CONTROL VOLTAGE AT PILOT WIPER CONTROL ASSEMBLY AND FOUND NO HALO VOLTAGE PRESENT. SWAPPED PILOT AND COPILOT WIPER ON/OFF SWITCHES ON COP AND FOUND DISCREPANCY FOLLOWED SWITCH. RETURNED COPILOT SWITCH BACK TO ITS ORIGINAL LOCATION. CONFIRMED PILOT WIPER ON/OFF SWITCH (P/N: 4271-503) IS FAULTY. RECEIVED OK TO INSTALL. RECEIVED AND INSTALLED NEW WIPER ON/OFF SWITCH (P/N: 4271-503) FROM GAC SAVANNAH, REFERENCE 8130-3 DATED 16DEC2015, FORM TRACKING NUMBER: 20151216093100, APPROVAL / AUTHORIZATION NUMBER: ODA-511131-CE, INTO THE PILOT POSITION. WORK PERFORMED IAA' GIV WDM 30-43-00. REFERENCE GULFSTREAM WESTFIELD WORK ORDER SC13577.18.15 FOR SYSTEM OPS CHECK. Billing Method Hours Rate Total Labor USD: Time and Material ST 6.35 @ $132.00 511311.20 Pans USD: Time and Material 5694.90 Total USD: $1.53.3.10 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 6.10#1 4271-503 SWITCH LIGHT ASSEMBLY I 5674.10 $674.10 6.10#2 D436-37 SLEEVE 10 51.42 514.20 6.10#3 D436-38 SLEEVE 4 51.65 $6.60 Step: 6.10.1 Completed APPLIED POWER TO AIRCRAFT AND CHECKED FOR PROPER CONTROL VOLTAGE AT PILOT WIPER CONTROL ASSEMBLY AND FOUND NO HULO VOLTAGE WAS PRESENT. SWAPPED PILOT AND COPILOT WIPER ON/OFF SWITCHES ON COP AND FOUND DISCREPANCY FOLLOWED SWITCH. RETURNED SWITCHES BACK TO THERE ORIGINAL LOCATIONS, CONFIRMED PILOT WIPER ON/OFF SWITCH PIN 4271-503 IS FAULTY. REFERENCED GIV WDM 30-43-00 FOR WORK PERFORMED. Discrepancy: 6.11 DURING COCKPIT COMPARTMENT ABOVE FLOOR INSP CMP 532017 NOTED ON CO-PILOTS SIDE CONSOLE AREA AFT END IS A BROKEN SWITCH LABLED ON/OFF. Resolution: ACCOMPLISHED MINOR ALTERATION AND REMOVED DISCREPANT SWITCH P/N MTL-206N LABELED COCKPIT LCD FROM COCKPIT SIDE CONSOLE AND BAGGED AND STOWED CONNECTOR AT SWITCH, REFERENCE KC AVIATION DWG NO. GIV-31085-31-52. CAPPED AND STOWED WIRE "AS100CC20" AT AIRSHOW C/B, REFERENCE KC AVIATION DWG NO. GIV-31085-31-52. DISCREPANT SWITCH WAS GIVEN TO CUSTOMER FOR FURTHER EVALUATION AND REPAIR. INSTALLED A PLUG TO COVER REMAINING HOLE DUE TO SWITCH REMOVAL. WEIGHT AND BALANCE CHANGE NEGLIGIBLE. Billing Method Hours Rate Total Labor USD: Time and Material ST 6.21 @ $132.00 58 19.72 Pans USD: Time and Material 55.16 Total USD: $824.88 Parts: Ref. No. Part number. Description Quantity Sell price USD Extended USD 6.11 #1 AN525-10-7 SCREW 2 S2.58 $5.16 Item: 7 INTERIOR For detail description of the work complied with see the Work Order Detail report. Westficld_GAC_Work Unless otherwise indicated, all financial values listed in this document am in US Dollars (USD). Printed: 49/2016 4:26:50AM Orderinvoice.rpt Page 8 of 14 LS MO EFTA00652205  Bill To: HYPERION AIR, INC. WO #: SCI3577 Invoice Number 6916001251 Team Manager: Charles Heinle Part/Model 4: Customer Coordinator: Vinny Cicala AC Serial No.fTail No.: TSN/TSO: CSN/CSO: Aircraft Timc: Discrepancy: 7.1 1 @ PROVIDE DOCUMENTATION OF REMOVED/REINSTALLED INTERIOR COMPONENTS ONLY. Resolution: THE INTERIOR COMPONENTS REFERENCED IN TFIE R&D LOG (RDS 002) HAVE BEEN REMOVED AND REINSTALLED USING GENERAL SHOP PRACTICES AND EXISTING HARDWARE. ANY COMPONENT REQUIRING OPERATIONAL OR LEAK CHECK HAS BEEN CHECKED FOR NORMAL OPERATIONS WITH NO DISCREPANCIES NOTED. Discrepancy: 7.2 CUSTOMER REPORTS THE COPILOTS AIR VENT IS INOP AND BROKEN. Resolution: PROVIDED ACCESS TO GASPER. FOUND AIRVENT BROKEN .INSTALLED NEW CUSTOMER SUPPLIED AIR OUTLET P/N 1747-2. REFERENCE PART AND MATERIAL CERTIFICATION FORM , REFERENCE/SO# 726461 DATED 3/1412016 PERFORMED A OPERATIONAL CHECK OF GASPER . GASPER CHECK IS GOOD. NO DEFECTS NOTED AT THIS TIME. REF. R/ D LOG FOR OPERATIONAL CHECK OF GASPER ON APU RUN . Billing Method Hours Rate Total Labor USD: Time and Material ST 9.77 (fr, $132.00 $1,289.64 Pans USD: Time and Material $1.56 Total USD: 41,291.20 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 7.2#3 MS27039-0814 SCREW 2 50.78 $1.56 Step: 7.2.1 Completed FOUND AIRVENT BROKEN .ORDERED NEW AIR OUTLET P/N 1747-2 NSN , RECIEVED AND INSTALLED NEW AIR OUTLET P/N 1747-2. REFERENCE PART OR MATERIAL CERTIFICATION FORM , REFERENCE/SO/I 726461 DATED 3/14/2016 Step: 7.2.2 Completed COPILOTS AIR VENT REQUIRES OPS CHECK DURING A/C RUNS. Discrepancy: 73 CUSTOMER REPORTS THE CAPTAIN'S AIR-VENT IS BROKEN. Resolution: PROVIDED ACCESS TO CAPTAINS GASPER. FOUND AIRVENT BROKEN. INSTALLED NEW CUSTOMERS SUPPLIED GASPER AIR OUTLET P/N 1747-2. REFERENCE PART AND MATERIAL CERTIFICATION FORM , REFERENCE/SO# 726461 DATED 3/14/2016. PERFORMED A OPERATIONAL CHECK OF GASPER. GASPER CHECK IS GOOD . NO DEFECTS NOTED AT THIS TIME. REF. R/ D LOG FOR OPERATIONAL CHECK OF GASPER ON APU RUN . Billing Method Hours Rate Total Labor USD: Time and Material ST 7.93 @ $132.00 $1,046.76 Total USD: 41,046.76 For detail description of the work complied with see the Work Order Detail report. Westfield_GAC_Work Unless otherwise indicated, all financial values listed in this document am in US Dollars (USD). Printed: 4/912016 4:26:50AM OrderInvo