EFTA01074471.pdf
Work Order Snapshot Work Order 14947 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.
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).
Resolution FOR BILLING PURPOSES ONL,
1 5 REMOVE THROTTLE QUADRANT FROM N508P FOR USE ON A/C N62MS. Completed
ReS0/O0n (CSF) REMOVED THROTTLE QUADRANT P/N 11595CF552.S S/N 80511 FOR USE ON N62MS 6550 S/N 5017 AND
INSTALLED SERVICEABLE THROTTLE QUADRANT P/N 1159SCF552-5 SIN 80261 FROM N62MS IAW CMP 761001, REF W.O.
MA14887.2.18. UPDATED CMP CODE 223005, 276203, 277002, 710025, 710026, 783007 & 783008. ALL OPS CHECKS
GOOD.
1 INSTALL THROTTLE QUADRANT ASSEMBLY I.A.W. GAC GV MM. 76-10.00, PERFORM AUTOTHROTTLE OPERATIONAL Completed
CHECK I.A.W. GAC GV MM. 22-30-00 AND PERFORM GUST LOCK SYSTEM - FUNCTIONAL TEST I.A.W. GAC GV MM. 27-
70-00.
2 PERFORM GROUND SPOILER SYSTEM - FUNCTIONAL TEST IA.W. GAC GV MM. 27.62.00. Completed
3 PERFORM THRUST REVERSER - OPERATIONAL CHECK IA.W. GAC GV MM. 78-3000 Completed
4 PERFORM ENGINE (TEST 4) - ENGINE POWER ASSURANCE CHECK LAW. GAC GV MM. 71.00.00. Completed
5 THROTTLE QUADRANT INSTALLED ON AIRCRAFT WAS SWAPPED FOR MAINT CONVENIENCE ANS WAS REMOVED Completed
FROM N62145 SEE V//0 14A14887 SQUAWK 2.18.
1 S COMPLY WITH TOUCH UP CLEANING AFTER MAINTENANCE (INTERIOR AND EXTERIOR) AND BEFORE Completed
DEPARTURE
Resolution COMPLIED WITH TOUCH UP CLEANING AFTER MAINTENANCE
1 7 MISC. MATERIAL / WASTE DISPOSAL FEE Completed
Renditi0n 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 A LIMITED PRELIMINARY INSPECTION AS REQUIRED BY FAR 145.211(c) (1) (ii). NO DEFECTS NOTED.
2 2 MAINTENANCE SUPERVISION REVIEW OF "TOOLING and MATERIAL ACCOUNTABILITY FORM(S) - FORM 181(r Completed
IS REQUIRED TO VERIFY COMPLETENESS OF ALL FORMS BEFORE AIRCRAFT CAN BE RELEASED TO SERVICE.
Resolution COMPLIED WITH FORM 1810
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 REP FASF 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 COMPLETED A MAIN BATTERY STATE OF CHARGE CHECK. NO DEFECTS NOTED.
2 6 UPDATE CMP CODE 346025 AND COMPLY WITH FMS NAV DATABASE UPDATE DUE 9-16-2015. Completed
Resolution OKAY TO DEFER PER GE CAPITALS MEL #34 15.1
Monday, Akron 24 2016 Page! o13
EFTA01074471
Work Order Snapshot Work Order # 14947 Aircraft N62MS
2 7 COMPLY WITH 28 DAY ENGINE PRESERVATION RUN DUE 11-7-2015. Completed
Resolution COMPLIED WITH 28 DAY ENGINE PRESERVATION RUNS.
APU HOURS:I845.50
1 RECORD APU HOURS AFTER 28 DAY ENGINE PRESERVATION RUN APU HOURS:1854.50 Completed
2 8 UPDATE CMP CODE 345004 AND COMPLY WITH FAR 91.171(b)(1) 30 DAY VOR CHECK Completed
NEXT DUE:11-6-2015
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
Resolubon TO BE COMPLIED WITH AT A LATER DATE
2 9 TOUCH UP PAINT ON L/H AND R/H UPPER AND LOWER AILERON COVE PANELS. Completed
ReSO/utlOn TOUCH UP PAINT ON UH MD R/H UPPER AND LOWER AILERON COVE PANELS.AS REQUIRED.
2 10 FOLLOWING THE FIRST ENGINE START,"L SAV MX" CAS MESSAGE ACTIVATED. THE ENGINE WAS SHUT DOWN Completed
AND RESTARTED. UPON RE-START, THE MESSAGE DE-ACTIVATED. MAYBE THIS WAS JUST A 'SIT-ITIS' ISSUE.
PLEASE ADVISE YOUR RECOMMENDATIONS. PERHAPS CHECK CMC AND ADVISE.
NOTE; FAULT INDICATES EEC COMMAND TO OPEN START VALVE BUT SOV REMAINS CLOSED.
Resoktion PERFORMED TWO SUCCESSFUL ENGINE STARTS AND SHUTDOWNS IAW G-550 MAINT MANUAL 71-00-00. NO FAULTS
WHERE NOTED ON STMT UP AND SHUTDOWN, COULD NOT DUPLICATE.
2 11 'CPCS MX REQD' AND CPCS CH 2 FAIL'CAS MESSAGE ACTIVE FOR ENTIRE FLIGHT. PLEASE EVALUATE. Completed
(CHECK CP CONTROLLER FOR FAULT LIGHTS LOCATED IN THE (PEER)
Resolution REMOVED AND REPLACED INOP LAMP FOR CABIN PRESSURE MANUAL CONTROL WITH NEW P/N 387. RESET CABIN
PRESSURE CONTROLLER AND COULD NOT DUPLICATE FAULT. PERFORMED CABIN PRESSURIZATION CONTROLLER
ADJUSTMENT TEST IAW G-5S0 MAINT MANUAL 31-31.0185 THRU B8. ALL OPS CHECKS GOOD.
1 REMOVE AND REPLACE INOP MANUAL INDICATION BULB ON PRESSURIZATION PANEL 0/N 387 Completed
2 PERFORM STEPS BS, B6, B7, AND 88 IAW G550 MAINT MANUAL 21-31.01 CABIN PRESSURIZATION CONTROLLER Completed
ADJUSTMENT TEST NO DEFECTS NOTED.
3 RESET CABIN PRESSURE CONTROLLER JAW G-5S0 MAINT MANUAL 21.31-01 COULD NOT DUPLICATE FAULT. Completed
2 12 THIRD CREW MEMBER JUMPSEAT LATERAL TRACKING IS JAMMED AND JUMPSEAT WILL NOT STOW. Completed
Resolution ri FANED SEAT TRACK AND LUBRICATED JUMP SEAT TRACKING MECHANISM, OPERATED JUMP SEAT LATERAL TRACKING
SEVERAL TIMES, OPS CHECK GOOD IAW G-550 MAINT MANUAL 25-11-02.
2 13 MAIN ENTRANCE DOOR FAILED TO CLOSE PRIOR TO LEAVING THE RAMP. AUX PUMP WAS OPERATING,BUT Completed
DOOR MOVED MINIMALLY. APPEARED THAT THE FIRST STEP IN THE PROCESS OF ACTUATING THE RELEASE
LOCKS FOR THE DOOR HALVES WAS NOT OCCURRING. MAYBE THIS IS A RIGGING ISSUE. DID NOT SEEM LIKE
AIR IN THE SYSTEM AS AUX PUMP OPERATION SOUNDED NORMAL. PLEASE EVALUATE.
Resoblion CYCLED MAIN ENTRANCE DOOR OPEN AND CLOSED FIVE TIMES WITH NO DISCREPANCIES,
REF- G-550-AJIM-52.1000,
NO DEFECTS NOTED.
2 14 ENTERED IN ERROR Completed
Resolubon ENTERED IN ERROR
1 REMOVE LOANER MEDAIRE KIT AND RETURN TO STOCK. Completed
2 15 COMPLY WITH A POSTFLIGHT INSPECTION. Completed
TIRE GAUGE:850246
Resolution COMPLIED WITH A POSTFLIGHT INSPECTION REF GV-SP (GS50) PFC-PLC DATED 7/2012.
APU HOURS: 1845.50
2 16 ENGINE OILIER IN THE TAIL COMPT IS LOW. Completed
Resolution SERVICED ENGINE OILIER IN THE TAIL COAIPT TO FULL AS REQUIRED.
2 17 HYDRAULIC OILIER IN THE TAIL COMPT IS LOW. Completed
Resolubon SERVICED HYDRAULIC OILIER IN THE TAIL COMPT TO FULL AS REQUIRED.
2 18 CREW OXYGEN PRESSURE IS LOW. Completed
ReSO/utiOn SERVICED CREW OXYGEN TO 1800 PSI MAW G-SSO MAINT MANUAL 12-19-00
lilonaray, Akron 24 2016 Page 2 at?
EFTA01074472
Work Order Snapshot Work Order # 14947 Aircraft N62MS
Monday, Arch 21, 2016 Page3of 3
EFTA01074473
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.
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).
Resolution FOR BILLING PURPOSES ONL,
1 5 REMOVE THROTTLE QUADRANT FROM N508P FOR USE ON A/C N62MS. Completed
ReS0/O0n (CSF) REMOVED THROTTLE QUADRANT P/N 11595CF552.S S/N 80511 FOR USE ON N62MS 6550 S/N 5017 AND
INSTALLED SERVICEABLE THROTTLE QUADRANT P/N 1159SCF552-5 SIN 80261 FROM N62MS IAW CMP 761001, REF W.O.
MA14887.2.18. UPDATED CMP CODE 223005, 276203, 277002, 710025, 710026, 783007 & 783008. ALL OPS CHECKS
GOOD.
1 INSTALL THROTTLE QUADRANT ASSEMBLY I.A.W. GAC GV MM. 76-10.00, PERFORM AUTOTHROTTLE OPERATIONAL Completed
CHECK I.A.W. GAC GV MM. 22-30-00 AND PERFORM GUST LOCK SYSTEM - FUNCTIONAL TEST I.A.W. GAC GV MM. 27-
70-00.
2 PERFORM GROUND SPOILER SYSTEM - FUNCTIONAL TEST IA.W. GAC GV MM. 27.62.00. Completed
3 PERFORM THRUST REVERSER - OPERATIONAL CHECK IA.W. GAC GV MM. 78-3000 Completed
4 PERFORM ENGINE (TEST 4) - ENGINE POWER ASSURANCE CHECK LAW. GAC GV MM. 71.00.00. Completed
5 THROTTLE QUADRANT INSTALLED ON AIRCRAFT WAS SWAPPED FOR MAINT CONVENIENCE ANS WAS REMOVED Completed
FROM N62145 SEE V//0 14A14887 SQUAWK 2.18.
1 S COMPLY WITH TOUCH UP CLEANING AFTER MAINTENANCE (INTERIOR AND EXTERIOR) AND BEFORE Completed
DEPARTURE
Resolution COMPLIED WITH TOUCH UP CLEANING AFTER MAINTENANCE
1 7 MISC. MATERIAL / WASTE DISPOSAL FEE Completed
Renditi0n 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 A LIMITED PRELIMINARY INSPECTION AS REQUIRED BY FAR 145.211(c) (1) (ii). NO DEFECTS NOTED.
2 2 MAINTENANCE SUPERVISION REVIEW OF "TOOLING and MATERIAL ACCOUNTABILITY FORM(S) - FORM 181(r Completed
IS REQUIRED TO VERIFY COMPLETENESS OF ALL FORMS BEFORE AIRCRAFT CAN BE RELEASED TO SERVICE.
Resolution COMPLIED WITH FORM 1810
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 REP FASF 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 COMPLETED A MAIN BATTERY STATE OF CHARGE CHECK. NO DEFECTS NOTED.
2 6 UPDATE CMP CODE 346025 AND COMPLY WITH FMS NAV DATABASE UPDATE DUE 9-16-2015. Completed
Resolution OKAY TO DEFER PER GE CAPITALS MEL #34 15.1
Monday, Akron 24 2016 Page! o13
EFTA01074471
Work Order Snapshot Work Order # 14947 Aircraft N62MS
2 7 COMPLY WITH 28 DAY ENGINE PRESERVATION RUN DUE 11-7-2015. Completed
Resolution COMPLIED WITH 28 DAY ENGINE PRESERVATION RUNS.
APU HOURS:I845.50
1 RECORD APU HOURS AFTER 28 DAY ENGINE PRESERVATION RUN APU HOURS:1854.50 Completed
2 8 UPDATE CMP CODE 345004 AND COMPLY WITH FAR 91.171(b)(1) 30 DAY VOR CHECK Completed
NEXT DUE:11-6-2015
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
Resolubon TO BE COMPLIED WITH AT A LATER DATE
2 9 TOUCH UP PAINT ON L/H AND R/H UPPER AND LOWER AILERON COVE PANELS. Completed
ReSO/utlOn TOUCH UP PAINT ON UH MD R/H UPPER AND LOWER AILERON COVE PANELS.AS REQUIRED.
2 10 FOLLOWING THE FIRST ENGINE START,"L SAV MX" CAS MESSAGE ACTIVATED. THE ENGINE WAS SHUT DOWN Completed
AND RESTARTED. UPON RE-START, THE MESSAGE DE-ACTIVATED. MAYBE THIS WAS JUST A 'SIT-ITIS' ISSUE.
PLEASE ADVISE YOUR RECOMMENDATIONS. PERHAPS CHECK CMC AND ADVISE.
NOTE; FAULT INDICATES EEC COMMAND TO OPEN START VALVE BUT SOV REMAINS CLOSED.
Resoktion PERFORMED TWO SUCCESSFUL ENGINE STARTS AND SHUTDOWNS IAW G-550 MAINT MANUAL 71-00-00. NO FAULTS
WHERE NOTED ON STMT UP AND SHUTDOWN, COULD NOT DUPLICATE.
2 11 'CPCS MX REQD' AND CPCS CH 2 FAIL'CAS MESSAGE ACTIVE FOR ENTIRE FLIGHT. PLEASE EVALUATE. Completed
(CHECK CP CONTROLLER FOR FAULT LIGHTS LOCATED IN THE (PEER)
Resolution REMOVED AND REPLACED INOP LAMP FOR CABIN PRESSURE MANUAL CONTROL WITH NEW P/N 387. RESET CABIN
PRESSURE CONTROLLER AND COULD NOT DUPLICATE FAULT. PERFORMED CABIN PRESSURIZATION CONTROLLER
ADJUSTMENT TEST IAW G-5S0 MAINT MANUAL 31-31.0185 THRU B8. ALL OPS CHECKS GOOD.
1 REMOVE AND REPLACE INOP MANUAL INDICATION BULB ON PRESSURIZATION PANEL 0/N 387 Completed
2 PERFORM STEPS BS, B6, B7, AND 88 IAW G550 MAINT MANUAL 21-31.01 CABIN PRESSURIZATION CONTROLLER Completed
ADJUSTMENT TEST NO DEFECTS NOTED.
3 RESET CABIN PRESSURE CONTROLLER JAW G-5S0 MAINT MANUAL 21.31-01 COULD NOT DUPLICATE FAULT. Completed
2 12 THIRD CREW MEMBER JUMPSEAT LATERAL TRACKING IS JAMMED AND JUMPSEAT WILL NOT STOW. Completed
Resolution ri FANED SEAT TRACK AND LUBRICATED JUMP SEAT TRACKING MECHANISM, OPERATED JUMP SEAT LATERAL TRACKING
SEVERAL TIMES, OPS CHECK GOOD IAW G-550 MAINT MANUAL 25-11-02.
2 13 MAIN ENTRANCE DOOR FAILED TO CLOSE PRIOR TO LEAVING THE RAMP. AUX PUMP WAS OPERATING,BUT Completed
DOOR MOVED MINIMALLY. APPEARED THAT THE FIRST STEP IN THE PROCESS OF ACTUATING THE RELEASE
LOCKS FOR THE DOOR HALVES WAS NOT OCCURRING. MAYBE THIS IS A RIGGING ISSUE. DID NOT SEEM LIKE
AIR IN THE SYSTEM AS AUX PUMP OPERATION SOUNDED NORMAL. PLEASE EVALUATE.
Resoblion CYCLED MAIN ENTRANCE DOOR OPEN AND CLOSED FIVE TIMES WITH NO DISCREPANCIES,
REF- G-550-AJIM-52.1000,
NO DEFECTS NOTED.
2 14 ENTERED IN ERROR Completed
Resolubon ENTERED IN ERROR
1 REMOVE LOANER MEDAIRE KIT AND RETURN TO STOCK. Completed
2 15 COMPLY WITH A POSTFLIGHT INSPECTION. Completed
TIRE GAUGE:850246
Resolution COMPLIED WITH A POSTFLIGHT INSPECTION REF GV-SP (GS50) PFC-PLC DATED 7/2012.
APU HOURS: 1845.50
2 16 ENGINE OILIER IN THE TAIL COMPT IS LOW. Completed
Resolution SERVICED ENGINE OILIER IN THE TAIL COAIPT TO FULL AS REQUIRED.
2 17 HYDRAULIC OILIER IN THE TAIL COMPT IS LOW. Completed
Resolubon SERVICED HYDRAULIC OILIER IN THE TAIL COMPT TO FULL AS REQUIRED.
2 18 CREW OXYGEN PRESSURE IS LOW. Completed
ReSO/utiOn SERVICED CREW OXYGEN TO 1800 PSI MAW G-SSO MAINT MANUAL 12-19-00
lilonaray, Akron 24 2016 Page 2 at?
EFTA01074472
Work Order Snapshot Work Order # 14947 Aircraft N62MS
Monday, Arch 21, 2016 Page3of 3
EFTA01074473