Work Order Snapshot

Work Order Snapshot Work Order # 15049 Aircraft N62MS 1 ADMINISTRATIVE ITEMS 1 1 AIRCRAFT FLIGHT LOG (AFL) DATA EXTRACTION, REQUIRED AFL MAINTENANCE ENTRIES AND ISSUANCE OF Completed MAINTENANCE/AIRWORTHINESS RELEASE (FAR 43.9, 43.11 OR 135.443, AS APPLICABLE). Resolution FOR BILLING PURPOSES ONLY. 1 2 GENERATION OF REQUIRED MAINTENANCE LOGBOOK ENTRIES FOR AIRFRAME, ENGINES AND AUXILIARY Completed POWER UNIT, AS APPLICABLE. Resolution FOR BILLING PURPOSES ONLY. 1 3 PROCESSING OF COMPLETED WORK INSTRUCTION CARDS WITH THE CUSTOMER'S MAINTENANCE TRACKING Completed PROVIDER FOR ALL MAINTENANCE ACTIVITIES (FAR 91.417 OR 135.439, AS APPLICABLE). Resobtion FOR BILLING PURPOSES ONLY. 1 4 [PAPER SIGNOFF] GREAT LAKES AIRCRAFT TO PERFORM AIRCRAFT PAINT POLISH AND BRIGHT WORK. ALSO Completed PAINTING OF SCREW HEADS AND CHIP. PREP FOR NBAA SHOW Resolution COMPLIED WITH BY OUTSIDE VENDOR. 1 5 SHIP BOX FOR GE CAPITAL Completed Resolution FOR BILLING PURPOSES ONLY. 1 6 MISC. MATERIAL / WASTE DISPOSAL FEE Completed Resolution BILLING ONLY 2 CUSTOMER REQUESTED MAINTENANCE 2 1 COMPLY WITH PRELIMINARY INSPECTION AS REQUIRED BY FAR 145.211(c) (1) (ii). Completed Resolution COMPLIED WITH PRELIMINARY INSPECTION AS REQUIRED BY FAR 195.211(c) (1) (ii). NO DEFECTS NOTED. 2 2 MAINTENANCE SUPERVISION REVIEW OF "TOOLING and MATERIAL ACCOUNTABILITY FORMS) - FORM 1810" Completed IS REQUIRED TO VERIFY COMPLETENESS OF ALL FORMS BEFORE AIRCRAFT CAN BE RELEASED TO SERVICE. Resolution COMPLIED WITH AS REQUIRED 2 3 UPON COMPLETION OF MAINTENANCE THE PERFORMANCE OF A WALK AROUND CHECK OF THE AIRCRAFT IS Completed REQUIRED BY THE AUTHORIZED INSPECTOR APPROVING THE AIRCRAFT FOR RETURN TO SERVICE. Resolution COMPLIED WITH WALKAROUND INSPECTION. 2 4 COMPLY WITH MAINTENANCE RELEASE TASKS, IF REQUIRED. Completed Resolution COMPLIED WITH MAINTENANCE RELEASE TASKS FOR RETURN TO SERVICE. 1 REMOVE RED "AIRCRAFT NOT AIRWORTHY" TAG. (FORM 1650) FROM AIRCRAFT. Completed 2 5 CHECK MAIN BATTERY STATE OF CHARGE PRIOR TO NEXT FLIGHT. Completed Resolution COMPLIED WITH AS REQUIRED, BATTERY VOLTAGE CHECKS NORMAL 2 6 UPDATE CMP CODE 346025 AND COMPLY WITH FMS NAV DATABASE UPDATE DUE 9.16.2015. Completed DEFER PER GE CAPITALS MEL 834-15.1 Resolution TO STAY DEFERRED AT THIS TIME 2 7 COMPLY WITH 28 DAY ENGINE PRESERVATION RUN DUE 12-18-2015. Completed Resolution COMPLIED WITH 28 DAY ENGINE PRESERVATION RUNS AS REQUIRED APU HOURS:1859.00 1 RECORD APU HOURS AFTER 28 DAY ENGINE PRESERVATION RUN Completed APU HOURS: 1859.00 Monday, Mitch 21, 2016 Page! N3 EFTA01074493 Work Order Snapshot Work Order # 15049 Aircraft N62MS 2 8 COMPLY WITH FAR 91.171(b)(1) 30 DAY VOR CHECK NEXT DUE:12-10-2015 RECORD THE FOLLOWING INFORMATION IN THE RESOLUTION: -BEARING TRANSMITTED -BEARING ERROR #1 -BEARING ERROR #2 NOTE: THE INSPECTOR RELEASING THE AIRCRAFT WILL ENTER RESULTS IN THE AFL Resolution COMPLIED WITH FAR 91.171(b)(1) 30 DAY VOR CHECK NEXT DUE: 01.09-16 RECORD THE FOLLOWING INFORMATION IN THE RESOLUTION: BEARING TRANSMITTED:0' -BEARING ERROR *1:0' -BEARING ERROR *2:0' TES1BOX 850217 Completed 2 9 COMPLY WITH A POSTFLIGHT INSPECTION. Completed TIRE GAUGE:850059 Resolution COMPLIED WITH POSTFLIGHT INSPECTION LAW. PENTASTAR G550 POSTFLIGHT SHEET. 2 10 COMPLY WITH INTERIOR, EXTERIOR TOUCH UP, HAND CLEAN WHEELS, GEARS AND DOORS. Completed Resolution COMPLIED WITH 2 11 COMPLY WITH REMOVING STOCK. Completed Resolubon COMPLIED WITH 2 12 LEFT ENGINE CAS MESSAGE PRESENTED ITSELF REQUIRING MAINTENANCE WITHIN 150 HOURS. Completed Resolution PERFORMED 2 SUCCESSFUL ENGINE STARTS ON THE L/H ENGINE NO MESSAGES WHERE NOTED. COULD NOT DUPLICATE. 1 PERFORM 2 ENGINE STARTS TO SEE IF MESSAGE APPEARS. Completed 2 13 LEFT ENGINE IS SLOW TO ACCELERATE ON TAKE-OFF. Completed ReSO/utiOn (CSF) RAN ENGINES AND PERFORMED 2 EACH EPR ACCELERATIONS ON EACH ENGINE ON CHANNEL A AND CHANNEL 8 OF THE FADECS. R/H ENGINE CHANNEL A WAS 12.15 SECONDS AND 11.20 SECONDS CHANNEL 8 WAS 11.66 SECONDS AND 11.66 SECONDS. L/H ENGINE CHANNEL A WAS 11.65 SECONDS AND 11.60 SECONDS CHANNEL B WAS 12.06 SECONDS AND 11.80 SECONDS [NOTE: ALL TIMES ARE APPROXIMATE AS USING A STOP WATCH] . PERFORMED FAN AIR VALVE FUNCTIONAL CHECK ON L/H AND R/H FAN AIR VALVES IAW G-550 MINT MANUAL 36-1400 NO DEFECTS NOTED. SWAPPED L/H AND P/H ENGINE EECS FOR MAINT CONVENIENCE IAW 73.21-21. OPS CHECK GOOD, UPDATED CMP CODES 732001 AND 732002. 1 RUN ENGINES AND PERFORM 2 EACH EPR ACCELERATIONS ON EACH ENGINE IN CHANNEL A AND CHANNEL 8 OF Completed THE FADECS. R/H ENGINE CHANNEL A WAS 12.15 SECONDS AND 11.20 SECONDS CHANNEL B WAS 11.66 SECONDS AND 11.66 SECONDS. L/H ENGINE CHANNEL A WAS 11.65 SECONDS AND 11.60 SECONDS CHANNEL B WAS 12.06 SECONDS AND 11.80 SECONDS [NOTE: ALL TIMES ARE APPROXIMATE AS USING A STOP WATCH]. 2 DOWNLOAD THE CMC FAULT HISTORY IAW G-SSO MAINT MANUAL 45-00-00 AND FORWARD TO GAC TECH OPS FOR Completed FURTHER EVALUATION AT 3 PERFORM FAN AIR VALVE FUNCTIONAL CHECK ON L/H AND R/H FAN AIR VALVES IAW G-550 MAINT MANUAL 36.14- Completed 00 NO DEFECTS NOTED. 4 (CSF) SWAP L/H AND P/H ENGINE EEC'S JAW G-SSO MAINT MANUAL 73.21.21 Completed 2 14 AT HIGH ALTITUDE AND HIGH POWER SETTINGS-LEFT ENGINE POWER LEVER HUNTS TO TRY TO MAINTAIN Completed POWER WITH AUTOTHRO1TLES ON. WITH AUTOTHROTTES OFF, MC POWER TARGET ON EICAS MOVES UP AND DOWN ERRATICALLY AND POWER OUTPUT OF THE ENGINE IS UNSTABLE. RATED MAX CONTINUOUS POWER FROM THE LEFT ENGINE IS NOT AVAILABLE. Resolution (CSF) INTERROGATED THE CNC FOUND STORED FAULTS, FAULT *1 FADEC REVERSION [ATA1]: AUTO THROTTLE FAILS TO ENC.ACS WHEN COMMANDED OR DISENGAGES WITHOUT COMMAND. An IS INHIBITED DUE TO A FADEC IN ALTERNATE OR REVERSION MODE. FAULT*2 TOLD *1 FAULT[ATAI]: LOSS OF ENGINE SYNC OR LOSS OF AT THRUST CONTROL MODE. PERFORMED AUTO THROTTLE ADJUSTMENT TEST IAW G-550 MINT MANUAL 22-30-00. NO DEFECTS NOTED. PERFORMED ASCB TELENET SWEEP IAW 31-41.00. NO DEFECTS NOTED. PERFORMED FM AIR VALVE FUNCTIONAL CHECK ON UM AND R/H FAN AIR VALVES IAW 36-14-00 NO DEFECTS NOTED. (CSF) SWAPPED L/H AND Rai ENGINE EEC'S IAW 73-21.21. OPS CHECK GOOD, UPDATED CMP CODES 732001 AND 732002. 1 INTERROGATE CMC FOUND STORED FAULTS, FAULT *I FADEC REVERSION [ATA1]: AUTO THROTTLE FAILS TO Completed ENGAGE WHEN COMMANDED OR DISENGAGES WITHOUT COMMAND. AT IS INHIBITED DUE TO A FADEC IN ALTERNATE OR REVERSION MODE. FAULTY/2 TOLD 1 FAULT[ATA I]: LOSS OF ENGINE SYNC OR LOSS OF AT THRUST CONTROL MODE. 2 PERFORM AUTO THROTTLE ADJUSTMENT TEST LAW G-550 MAINT MANUAL 22.30-00. NO DEFECTS NOTED. Completed 3 PERFORM ASCB TELENET SWEEP IAW G-550 MAINT MANUAL 3141.00. NO DEFECTS NOTED. Completed 4 DOWNLOAD THE CMC FAULT HISTORY IAW G-550 MAINT MANUAL 45-00-00 AND FORWARD TO GAC TECH OPS FOR Completed FURTHER EVALUATION AT Monday, Mitch 21, 2016 Page 2 of.? EFTA01074494 Work Order Snapshot Work Order # 15049 Aircraft N62MS 5 PERFORM FAN AIR VALVE FUNCTIONAL CHECK ON 1/H AND R/H FAN AIR VALVES TAW 6.550 MAINT MANUAL 36.14. Completed 00 NO DEFECTS NOTED. 6 (CSF) SWAP L/H AND R/H ENGINE EEC'S JAW G-SSO MAINT MANUAL 73.21.21 Completed 2 15 COMPLY WITH AD 2015-23-09 AMDT 39-18325 DATED 12/28/2015 PARAGRAPHS (g) AND (h)- ZODIAC Completed AEROTECHNICS FLIGHT CREW OXYGEN MASK REGULATORS P/N MC10, MF10, AND MF20 WITH S/M LISTED IN APPENDIX I OF ZODIAC SERVICE BULLETIN MCF-SBU-35-001 REVISION 1 DATED 12/03/2012. Resolution COMPLIED WITH AC) 2015.23-09 AMDT 39.18325 DATED 12/28/2015 PARAGRAPH (g) BY REVIEW OF MAINTENANCE RECORDS TO DETERMINE APPUCABIUTY. PARAGRAPH (h) DOES NOT APPLY BY INSTALLED UNITS' PM AND St NO FURTHER ACTION REQUIRED. UPDATED CLIP. 2 16 EMERGENCY LANDING GEAR BOTTLE PRESSURE LOW. Completed ReRiutiOn SERVICED EMERGENCY LANDING GEAR BOTTLE LAW. GAC GSSO M. 32.39-03. 2 17 PERFORM AUDIT OF AIRCRAFT MANUALS Completed Resokition COMPLETED 2 18 COMPLY WITH INSTALLING ENGINE COVERS AND PITOT TUBE COVERS (AND REMOVING ALL OF THE ABOVE Completed BEFORE DEPARTURE) AS REQUESTED Resobtron REMOVED ENGINE COVERS AND PITOT COVERS AS REQUIRED 2 19 REF SQUAWK 2.14 PYLON PANEL 411 GB HAS A THREADED PORTION OF A SCREW SHANK STUCK IN A Completed NUTPLATE. ReRiutiOn REPLACED NAS1791C3.3 NUTPLATE WITH NEW NAS1791C3.3 NUTPLATE. 2 20 REF SQUAWK 2.14 FOUND 2 EA PYLON BONDING STRAPS CORRODED UNDER L/H ENGINE PYLON PANELS Completed 411GB AND 411EB ATTACHING HARDWARE GAB512808-04H, GAC5808A08, GAB512GB08-03H AND, GAC.580BA08. EST 3.0 HOURS TO REPLACE APPROVED PM 12-10-15 Reggition CONTACTED GAC TECHNICAL OPERATIONS FOR BONDING STRAP ADHESIVE INFORMATION. REPLACED BONDING STRAP PM 1159P50267.59 AND, 1159P50267-61. REFERENCE DRAWING 1159P57900 AND GAMPS 4108. 2 21 REF SQUAWK 2.14 FOUND 2 EA PYLON BONDING STRAPS CORRODED UNDER R/H ENGINE PYLON PANELS Completed 421GB AND 421EB BONDING STRAP P/IN 1159P50267-60 AND, 1159P50267-62 ATTACHING HARDWARE GAB512B08-04H, GAC580BA08, GAB512GB08-03H AND, GAC.580BA08. EST 3.0 HOURS TO REPLACE APPROVED PM 12-10-15 Resobtion CONTACTED GAC TECHNICAL OPERATIONS FOR BONDING STRAP ADHESIVE INFORMATION. REPLACED BONDING STRAP PM 1159950267.60 AND, 1159P50267-62. REFERENCE DRAWING 1159P57900 AND GAMPS 4108. 2 22 COMPLY WITH TOUCH UP CLEANING AFTER MAINTENANCE (INTERIOR AND EXTERIOR) Completed Resobaon COMPLIED WITH TOUCH UP CLEANING AFTER MAINTENANCE AND CLEANED WHEELS,GEMS AND DOORS Monday, Mitch 21, 2016 Page 3 of.? EFTA01074495