N864GA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
78 reports on file, 2004-09-24 – 2018-07-09.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 57,747 hrs · 37,977 cycles
FOUND AFT MEGAPHONE INOP. R&R AFT MEGAPHONE.
Part: ACM — ODOR (AC BAY) · airframe 57,738 hrs · 37,972 cycles
STRONG EXHAUST SMELL COMING FROM PACKS WHILE USING APU AIR. R&R LT ACM, BOTH COALESCER BAGS AND PERFORMED CLEANING OF DUCTS.
Part: FITTING — CRACKED (FUSELAGE) · airframe 57,085 hrs · 37,651 cycles
RT LOUVER CLIP AT CANTED FRAME 1463 CRACKED AT LONG 7R. REPLACED RT LOUVER CLIP AT LONG 7R STA 1463.
Part: FITTING — CRACKED (FUSELAGE) · airframe 57,085 hrs · 37,651 cycles
LT LOUVER CLIP CRACKED AT CANTED FRAME STA 1463 LONG 8L. REPLACED LT LOUVER CLIP IAW SRM 51-30-5.
Part: FITTING — CRACKED (FUSELAGE) · airframe 57,085 hrs · 37,651 cycles
RT LOUVER CLIP CRACKED AT CANTED FRAME LONG 8R. REPLACED CLIP AT CANTED FRAME STA 1463 LONG 8R.
Part: FITTING — CRACKED (FUSELAGE) · airframe 57,085 hrs · 37,651 cycles
LT LOUVER CLIP CRACKED AT CANTED FRAME 1643 LONG 7L. REPLACED LT LOUVER CLIP IAW SRM 51-30-5.
Earlier reports · 2004–2017 · 72 reports
2017
Part: FITTING — CRACKED (VERTICAL STAB) · airframe 56,540 hrs · 37,374 cycles
INTERNAL VENTRAL CLIP CRACKED. REMOVED AND REPLACED CLIP IAW MD80 SRM 51-30-2 FIG 1, 51-30-5 PARA 7.
Part: FORMER — CRACKED (VERTICAL STAB) · airframe 56,540 hrs · 37,374 cycles
INTERNAL VENTRAL FORMER CRACKED. REMOVED AND REPLACED FORMER IAW SRM 51-30-1 FIG 1, 51-30-5 PARA 7.
Part: SKIN — CORRODED (BS 1303-1315) · corrosion level 2 · airframe 56,540 hrs · 37,374 cycles
FUSELAGE SKIN IS CORRODED AT THE AFT LAVATORY SERVICE PANEL DOOR FWD LOWER CORNER. REPAIRED THE SKIN IAW EA 25-2017-085.
Part: LONGERON — DAMAGED (BS 1295-1316) · airframe 56,540 hrs · 37,374 cycles
LONGERON IN AFT CARGO BAY DAMAGED. REPAIRED THE LONGERON IAW SRM 53-05, FIG 18.
Part: BEAM — CORRODED (BS 1117-1250) · corrosion level 2 · airframe 56,540 hrs · 37,374 cycles
AFT CARGO DOOR FRAME BEAM CORRODED. REMOVED AND REPLACED AFT CARGO DOOR BEAM IAW SRM 51-10-4, 51-30-2, AND 51-30-5.
Part: PANEL — CRACKED (ZONE 300) · airframe 56,540 hrs · 37,374 cycles
PANEL 3804A HAS CRACK IN MIDDLE OF PANEL
Part: DOUBLER — CORRODED (BS 1174-1194) · corrosion level 2 · airframe 56,540 hrs · 37,374 cycles
AFT CARGO BAY, FOUND CORROSION ON THE INTERNAL DOUBLER BS 1174 - 1194.
Part: INTERCOSTAL — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 56,540 hrs · 37,374 cycles
AFT CARGO BAY HAS A CORRODED INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-104, AND 51-30-2,31-30-5.
Part: ENGINE — FAILED (LEFT) · airframe 56,404 hrs · 37,303 cycles
(EMERGENCY DECLARED) LT ENGINE FAILED AFTER LOUD BANG. R&R LT ENGINE.
Part: ENGINE — FAILED (LEFT) · airframe 56,404 hrs · 37,303 cycles
EMERGENCY DECLARED, LT ENGINE FAILED AFTER LOUD BANG. AC AOG.
Part: BULB — FAILED (CABIN) · airframe 56,094 hrs · 37,141 cycles
BURNED RUBBER ODOR ON TAKE OFF FROM BOTH FORWARD & AFT FA STATIONS. R & R THE BULB.
2016
Part: FRAME — CRACKED (FUSELAGE) · airframe 54,036 hrs · 36,094 cycles
FRAME CRACKED AT FS 937, RBL 4, AT ANTI-ICE DUCT. REPAIRED FRAME IAW SRM 53-05 FIG 81. M301 ITEM 150 WO 1012435 1000 0035.
Part: FRAME — CRACKED (FUSELAGE) · airframe 54,036 hrs · 36,094 cycles
FRAME CRACKED AT FS 937, RBL 4, AT ANTI-ICE DUCT. REPAIRED FRAME IAW SRM 53-05 FIG 81.
2015
Part: BATTERY — DISCHARGED (CABIN) · airframe 53,650 hrs · 35,892 cycles
EMERGENCY LIGHTS OUT, ROW 15, 17 & 19, UPPER CABIN. R & R EMER LIGHT BATTERY ON ROW 17 DEF IAW AMM 33-53-01. OPERATIONS CHECKED GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 53,583 hrs · 35,857 cycles
AFTER SLAT RETRACTION, SLAT DISAGREE ILLUMINATED & LIGHT REMAINED ILLUMINATED. COMPLETED QRH 27.8, LIGHT EXTINGUISHED CLIMBING THROUGH FLIGHT LEVEL 200. FLIGHT CONTINUED, NO ROLLING TENDENCY NOTICED. SLAT FLAP EXTENSION DURING APPROACH & LANDING NORMAL. REFERENCE LOG PAGE 619226. OPERATIONS CHECKED OK IAW AMM 27-80-00-5-0. NO FAULTS NOTED.
Part: BATTERY — DISCHARGED (CABIN)
PORTABLE CABIN EMER LIGHT INOPERATIVE. REPLACED BATTERIES IN PORTABLE CABIN EMER LIGHT IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.
Part: BATTERY — DISCHARGED (PORTABLE LIGHT) · airframe 53,271 hrs · 35,680 cycles
PORTABLE CABIN EMER LIGHT INOPERATIVE. REPLACED BATTERIES IN PORTABLE CABIN EMER LIGHT IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.
Part: CONTROL VALVE — OUT OF ADJUST (BLEED AIR SYS)
DURING CRUISE, PNEU PRESS READ 30 PSI WITH BOTH XFEED LEVERS CLOSED. WHEN EITHER LT OR RT AIRFOIL SWITCH TURNED ON PSI DROPPED TO ZERO. WHEN EITHER LT OR RT AIRFOIL SWITCH TURNED OFF, PNEU PSI WOULD SLOWLY BUILD BACK UP TO 30 PSI WITH BOTH XFEED LEVERS CLOSED. PERFORMED ADJUSTMENT & TEST FOR PNEUMATIC XFEED VLV CONTROLS IAW AMM 36-10-03-2-0. IT IS PERMISSIBLE FOR PRESS TO BE INDICATED ON INDICATOR WITH XFEED VLVS CLOSED. WHEN LT OR RT AIR FOIL SWITCH ON PRESS INDICATED IS 22 PSI OR LESS IS ACCEPTABLE LEAKAGE FOR XFEED VLVS.
Part: TARGET — OUT OF ADJUST (LE SLAT)
AFTER FLAP & SLAT RETRACTION DISAGREE LIGHT REMAINED ILLUMINATED, FOUND LEFT SLAT D PROX SENSOR TARGET HANGING UP. ADJUSTED SAME & OPERATIONS CHECKED IAW MM 27-80-06. OK FOR SERVICE.
Part: FLAP — CRACKED (LT WING) · airframe 52,607 hrs · 35,330 cycles
LEFT OTBD TE OF FLAP IS CRACKED. REPAIRED LT OTBD TE FLAP IAW SRM 57-03.
2014
Part: LONGERON — CRACKED (FUSELAGE) · airframe 51,946 hrs · 34,989 cycles
LONGERON 30 CRACKED AT APPROX FS 244 & 250. REPAIRED LONGERON 30 IAW SRM 53-02 FIG 18.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 51,946 hrs · 34,989 cycles
LONGERON 29L CRACKED AT APPROX FS 244 & 250. REPAIRED LONGERON 29L IAW SRM 53-02 FIG 8.
Part: FRAME — CORRODED (FUSELAGE) · airframe 51,946 hrs · 34,989 cycles
FRAME AT FS 1250 LONGERON 30 CORRODED. REMOVED PREVIOUS REPAIR, FABRICATED & INSTALLED FRAME & REPAIR PARTS IAW SRM 53-03 FIG 2 A. WORK ACCOMPLISHED ON WORK ORDER 1011099-1000-0087 M301 ITEM 400.
Part: SEAT TRACK — MECHANIC ERROR (FUSELAGE) · airframe 51,946 hrs · 34,989 cycles
CABIN SEAT TRACK DOUBLE DRILLED STATION 1307 AT LBL 22. CUT OUT DAMAGED SEAT TRACK FROM STATION 1260 TO 1309. FABRICATED REPLACEMENT SEAT TRACK, LOCATED, DRILLED & INSTALLED A SPLICE REPAIR AT STATION 1260 IAW SRM 53-05 FIGURE 4F. WORK ACCOMPLISHED ON WORK ORDER 227614 M301 ITEM 356. WORK ORDER 1011099-2000-0016.
Part: PORTABLE LIGHT — INOPERATIVE (CABIN)
FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R PORTABLE FLASHLIGHT IAW MM33-53-00. OPERATIONS CHECKED GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
LEFT & RIGHT FWD EXIT IDENTIFIERS WILL NOT LIGHT UP WHEN TESTING EMERGENCY LIGHTS. R & R BATTERY PACK FOR LT & RT FWD EXIT IDENTIFIERS IAW AMM 33-53-00 & 33-53-01, OPERATIONS CHECKED GOOD.
Part: ACM — OVERSERVICED (AC BAY)
DURING CLIMB OUT MULTIPLE PRESS BUMPS WERE FELT, SMOKE WAS VISIBLE IN COCKPIT. FOLLOWED QRH PROCEDURE & TURNED LEFT PACK OFF. SMOKE DISSIPATED & PRESSURIZATION BEGAN WORKING NORMALLY. PERFORMED WORK ORDER 22195, NO FURTHER DEFECTS NOTED. TROUBLE SHOT LT PACK FOUND LT ACM OVERSERVICED. SERVICED LT ACM TO PROPER LEVEL IAW AMM 12-1-03. CHECKED DUCTING OF LT ACM FOR CONTAMINATION NONE FOUND IAW AMM 21-20-00. OPERATIONS CHECKED LT PACK CHECKED FOR LEAKS. FOUND APU EXHAUST SHROUD CLAMP NOT SECURED BY PASSING EXHAUST INTO APU COMPARTMENT. R & R THE EXHAUST SHROUD SYS, OPERATIONS CHECK & LEAK CHECKED GOOD IAW AMM 49-80-01.
Part: BATTERY — DISCHARGED (FLASHLIGHT)
AFT FLIGHT ATTENDANT`S POSITION, ONE EMERGENCY FLASHLIGHT NOT FLASHING. REPLACED BATTERY IN FLASHLIGHT IAW AMM 25-60-00.
2013
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT)
FWD FA STATION UPPER EMERGENCY FLASHLIGHT INDICATOR DOES NOT BLINK. REF AMM 25-60-00; R & R BATTERY PACK ASSY. OPS CHECKED NORMAL. SECURED FLASHLIGHT IN HOLDER.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R BATTERY PACK IN THE POWER SUPPLY AND LIGHT RELAY, MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
2012
Part: BATTERY — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
2011
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
Part: SKIN PANEL — GOUGED (VERTICAL STAB)
VERTICAL STAB UPPER AFT FAIRING CHAFED AND GOUGED ON RIGHT AFT SIDE. REMOVED, FABRICATED AND INSTALLED SKIN PANEL IAW EA 14483 REV 1R DATED 3 AUG 2011, MD80 SRM 51-30-2, 51-10-4.
Part: SKIN PANEL — GOUGED (VERTICAL STAB)
VERTICAL STAB UPPER AFT FAIRING CHAFED AND GOUGED ON LEFT SIDE. REMOVED, FABRICATED AND INSTALLED NEW SKIN PANEL IAW EA 14482 REV 1R DATED 3 AUG 2011 AND MD80 SRM 51-10-4, 51-30-2.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
2010
Part: BATTERY — DISCHARGED (CABIN)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.
2009
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE.
Part: UNKNOWN — ODOR (CABIN)
ON TAKEOFF, ODOR OF SMOKE IN CABIN, NO VISIBLE SMOKE, RETURNED TO FIELD. MAINTENANCE DEPARTMENT PERSONNEL REPORTED CONTINUOUS USE OF APU DURING GROUND OPERATIONS, OPS CHECK OF BOTH PACKS IAW MM 21-20-00, NO DEFECTS OR LEAKS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.
Part: BALLAST — SMOKE (CABIN LIGHTS)
FLIGHT CREW REPORTED ELECTRICAL SMOKE MID CABIN. DIVERTED FLIGHT TO LAS VEGAS AND LANDED WITHOUT INCIDENT. MAINTENANCE DEPARTMENT PERSONNEL REPLACED TWO LIGHT BALLAST AT SEAT ROW 16 AND 17 DEF, AMM 33-21-03. SYSTEM OPERATION CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.
2008
Part: BATTERY PACK — FAILED (EMERGENCY LIGHT)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (S)
Part: COALESCER BAG — SMOKE (RT A/C PACK)
FLIGHT CREW REPORTED RIGHT AIR CONDITIONING PACK ON, SMOKE WAS ENTERING THE CABIN. THE DISCREPANCY WAS DEFERRED PER MEL 21-01 SITUATION 1 WITH ALL M PROCEDURES COMPLIED WITH. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIR CONDITIONING SYSTEM AND REPLACED THE RIGHT AND LEFT COALESCER BAGS IAW AMM 21-20-02. RIGHT AND LEFT AIR CONDITIONING SYSTEM OPERATIONAL CHECK WAS NORMAL. NO SMOKE NOTED IN CABIN. THE AIRCRAFT WAS RETURNED TO SERVICE.
2007
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.
Part: PIN — BROKEN (TRANSDUCER)
DURING TAKEOFF ROLL THE WHEEL NOT TURNING LIGHT ILLUMINATED, TAKEOFF ABORTED AND AIRCRAFT RETURNED TO THE GATE IN LAS VEGAS. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIRCRAFT AND FOUND THE NR 1 WHEEL TRANSDUCER PINS LAYING IN THE HUB CAP. TRANSDUCER PINS REINSTALLED AND OPERATIONAL CHECK PERFORMED NORMAL IAW M/M 32-43-02. AIRCRAFT RETURNED TO SERVICE.
Part: RELAY — FAILED (A/C PACK)
AIRCRAFT 864GA WHILE TAXING FOR TAKEOFF FROM GPT ON FLT 778, FLIGHT CREW DETECTED A PUNGENT ODOR AND LIGHT SMOKE HAZE IN THE COCKPIT AND FWD CABIN, AFTER NR 2 ENGINE STARTED. ADDITIONALLY IT WAS NOTED AT THE GATE THE LEFT PACK FAN DID NOT COME ON. FLIGHT CREW RETURNED TO THE GATE AND NOTIFIED MTX CONTROL. ON CALL MTX WAS DISPATCHED AND THE ACM WAS DEFERRED IAW MEL 21-01 SITUATION NR 1, M PROCEDURE COMPLIED WITH. AIRCRAFT PROCEEDED TO SFB AND MAINTENANCE DEPARTMENT PERSONNEL INSPECTED AND TROUBLESHOOT THE AIR CONDITIONING SYSTEM, DETERMINING THE COOLING FAN TIME DELAY RELAY WAS INOPERATIVE. THE RELAY WAS REPLACED AND A SYSTEM OPERATIONAL CHECK WAS PERFORMED IAW AMM 21-20-06. SYSTEM OPS CHECKS NORMAL AND TH
Part: CONTROL SWITCH — MALFUNCTIONED (NLG INDICATOR)
RED NOSE GEAR LIGHT ILLUMINATED INFLIGHT WITH GEAR HANDLE UP. FLIGHT CREW FOLLOWED QRH AND LIGHT DID NOT EXTINGUISH. AIRCRAFT RETURNED TO LAS AND LIGHT WENT OUT ON DESCENT AND REDUCED AIRSPEED. MAINTENANCE DEPARTMENT REMOVED AND REPLACED CONTROL SWITCH REF AMM 32-21-01 AND PERFORMED OPERATIONAL CHECK OF NOSE GEAR LANDING GEAR REF AMM 32-60-00. OPERATIONAL CHECK NORMAL. AIRCRAFT HAS RETURNED TO SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION LAS VEGAS MAINTENANCE REPORTED THAT THE CEILING EMERGENCY LIGHTS AT SEATROWS 21 THRU 24 WOULD NOT TEST. LAS VEGAS FURTHER REPORT THE REMOVAL AND REPLACEMENT OF THE EMERGENCY LIGHT POWER SUPPLY BATTERY PACK AT FUSELAGE STATION 901. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. THE AIRPLANE HAS RETURNED TO SERVICE.
Part: INDICATOR — MALFUNCTIONED (NLG)
FLIGHT 591, THE FLIGHT CREW REPORTED THAT AFTER RETRACTING THE GEAR, THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE NLG INDICATOR PIN (MECHANICAL) INDICATED NOSE GEAR UP. CYCLED GEAR AND RED UNSAFE LIGHT EXTINGUISHED AND DID NOT REOCCUR FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE REPORT THE INSPECTION OF THE MECHANICAL AND ELECTRICAL COMPONENTS OF THE NOSE GEAR WITH NO FAULTS FOUND. JACKED AIRPLANE NOSE IAW AMM 07-12-00 AND PERFORMED A SATISFACTORY NOSE GEAR SWING IAW AMM 32-30-00. THE AIRPLANE HAS RETURNED TO SERVICE.
Part: UNKNOWN — UNKNOWN (VHF RADIOS)
FLIGHT 833 PIE/SBN - DURING CLIMB-OUT, FLT CREW REPORTED THAT BOTH THE CAPTAIN'S & FIRST OFFICER'S VHF RADIOS WERE INTERMITTENT USING EITHER HEADSET OR HAND MIC. THE ISSUE WAS TRANSMISSION RATHER THAN RECEPTION. RETURNED TO POINT OF DEPARTURE & LANDED WITHOUT INCIDENT. MX REPORT THAT VHF TRANSCEIVERS NR 1 & 2 WERE REMOVED, CONNECTORS CLEANED/INSPECTED, AND RE-INSTALLED IN ORIGINAL POSITIONS. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 23-20-00. THE AIRPLANE WAS RETURNED TO SERVICE.
2006
Part: LANYARD — MISROUTED (ESCAPE SLIDE)
LAS - MAINTENANCE FOUND THE L1 EMERGENCY SLIDE LANYARD ROUTED WRONG. ATTACHED L1 SLIDE LANYARD CORRECTLY IAW MM 25-62-00. AIRCRAFT RETURNED TO SERVICE.
Part: LANYARD — MISROUTED (EMERGENCY SLIDE)
LAS - MAINTENANCE FOUND THE R1 EMERGENCY SLIDE LANYARD ROUTED WRONG. ATTACHED R1 SLIDE LANYARD CORRECTLY IAW MM 25-62-00. AIRCRAFT RETURNED TO SERVICE.
Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHTS)
LAS - MAINTENANCE FOUND THE EMERGENCY FLOOR LIGHTS INOPERATIVE AT ROWS 27 TO 31. RESECURED THE WIRE HARNESS FROM ROWS 27 TO 31 IAW MM 33-50-00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CONTROL BOX — MALFUNCTIONED (ANTI SKID)
LAS - FNL, CREW REPORTED THE WHEEL NOT TURNING LIGHT CAME ON DURING THE TAKEOFF ROLL AT 80 KNOTS THEN WENT OUT DURING ROLL OUT AFTER ABORTED TAKEOFF. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE ANTI-SKID CONTROL BOX. OPERATIONALLY CHECKED GOOD IAW MM 32-43-04 AND 32-43-00. FOUND BOTH DRIVE COUPLING STUDS MISSING IN THE NR 1 POSITION WHEEL SPEED TRANSDUCER. INSTALLED DRIVE COUPLING STUDS IAW MM 32-43-02. OPERATIONALLY CHECK OF NR 1 POSITION WHEEL SPEED TRANSDUCER GOOD IAW MM 32-43-02. AIRCRAFT RETURNED TO SERVICE.
2005
Part: CONTROL UNIT — MALFUNCTIONED (ANTI SKID)
MSN TO LAS - WHEEL NOT TURNING LIGHT ILLUMINATED ON TAKEOFF AT 60 KNOTS, ABORTED TAKEOFF. MAINTENANCE REMOVED AND REPLACED ANTI-SKID CONTROL UNIT SYSTEM OPERATIONALLY CHECKED GOOD IAW AMM 32-43-04. AIRCRAFT RETURNED TO SERVICE.
Part: BRAKE — SEIZED (NR 2)
FNL - DURING TAKEOFF ROLL WHEEL NOT TURNING, LIGHT CAME ON. ABORTED TAKEOFF BELOW 80 KIAS. NR 2 BRAKE OVERHEAT LIGHT CAME ON, TEMP PEAK AT 350 DEGREES. MAINTENANCE FOUND NR 2 BRAKE SEIZED. MAINTENANCE REMOVED AND REPLACED NR 2 BRAKE AND NR 2 TIRE ASSEMBLY IAW 32-40-01 AND 32-42-01. SERVICED TIRE TO 200 PSI IAW 12-16-01. AIRCRAFT RETURNED TO SERVICE.
2004
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
LAS - MAINTENANCE REPORTED OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT BATTERY PACK IAW 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: AUTOTHROTTLE SYS — MALFUNCTIONED (COCKPIT)
SCHEDULED FLIGHT MSN TO LAS, CREW ABORTED TAKEOFF AFTER BRAKE RELEASE ON TAKEOFF ROLL AT ABOUT 60 KNOTS DUE TO AUTO THROTTLES CLICKING OFF. CREW REPORTED THE AUTO THROTTLES KICKED OFF AS SOON AS POWER WAS SET FOLLOWED BY A POWER LOSS TO THE NR 1 FMA, NR 1 FD FAILURE AND DFGS FAILURE. AIRCRAFT CLEARED THE RUNWAY WITH VERY LIGHT BRAKING. MAINTENANCE CONTROL ADVISED CREW TO DE-POWER THE AIRCRAFT TO RESET THE SYSTEM. AFTER POWER WAS RESTORED ALL SYSTEMS FUNCTIONED PROPERLY AND AIRCRAFT CONTINUED THE SCHEDULED FLIGHT.
Part: ACTUATOR — FAILED (NLG)
AFTER TAKEOFF FROM PIA EN ROUTE TO LAS, CREW REPORTED NOSE GEAR WOULD NOT RETRACT PROPERLY. AIRCRAFT RETURNED TO PIA , CREW PERFORMED NORMAL OVERWEIGHT LANDING UNDER THE FOLLOWING CONDITIONS; SINK RATE 256 TO 300 FEET PER MINUTE, NO SIDE LOADS, LANDING WEIGHT 144,800 LBS. CONTRACT MX ACCOMPLISHED OVERWEIGHT LANDING INSPECTION IAW MM 05-51-04 WITH NO DEFECTS FOUND. MX REMOVED NOSE GEAR HYDRAULIC RESTRICTORS, CLEANED, INSPECTED AND FLOW CHECKED FOR TROUBLESHOOTING. RESTRICTORS OPERATIONALLY GOOD IAW MM 32-60-00. RESTRICTORS REINSTALLED. AIRCRAFT FERRIED TO GYR. MX REMOVED AND REPLACED NLG ACTUATOR IAW MM 32-32-06. UNIT LEAK CHECKED AND OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS, ROW 31 TO 35 AND EMERGENCY POWER OVERHEAD LIGHTS, ROW 25, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN BATTERY PACK IAW 33-53-00. LIGHTS ROW 31 TO 35 OPERATIONALLY CHECK GOOD. MAINTENANCE REPLACED BULBS AT ROWS 25, 29 AND 33 LIGHTS OPERATIONALLY CHECKED GOOD IAW 33-53-00. AIRCRAFT RETURNED TO SERVICE