N378AN
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.
73 reports on file, 1995-02-01 – 2016-01-24.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,908 hrs · 15,143 cycles
AIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH LE SLAT ASYMMETRY LIGHT ILLUMINATED WHEN FLAPS 1 SELECTED. LIGHT EXTINGUISHED UPON ARRIVAL. ACCOMPLISHED FLAP & SLAT PRIMARY DRIVE & INDICATION SYS TEST IAW AMM 27-51-00 WITH NO FAULTS FOUND. ACCOMPLISHED BITE OF FSEU WITH MSG 27-81021 INTERMITTENT & INACTIVE RETURNED. ACCOMPLISHED PSEU BITE & SLAT SENSOR TARGET TESTS WITH NO FAULTS FOUND. ACFT OK FOR SERVICE.
Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 94,785 hrs · 15,122 cycles
AIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE RECEIVED CTR HYD QTY EICAS MSG WITH QTY INDICATION OF .45 RF. ALL CTR PUMPS TURNED OFF. NO FURTHER QTY LOSS. ALL CTR PUMPS BACK ON FOR APPROACH. QTY AT GATE .31 RF. R & R HYD LINE, BETWEEN C1 HYD PUMP & FILLER HOUSING IAW AMM 20-10-00 & SERVICED HYDS IAW AMM 12-12-01. LEAK & OPERATIONAL CHECKED NORMAL.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,731 hrs · 15,112 cycles
GOING FROM FLAPS 20 - 25, THE LE ASYMMETRY, LE SLAT ASYMMRYTY, LIGHT CAME ON. AUTO PILOT HANDLE WENT BACK TO 20. THE FLIGHT DECLARED AN EMER & LANDED WITHOUT FURTHER INCIDENT. NO FAULTS ON FSEU. RAN FLAPS & SLATS UP & DOWN SEVERAL TIMES, NO FAULTS. INSTALLED UPGRADED FSEU ON ACFT FOR BETTER TROUBLESHOOTING, SYS OK FOR SERVICE. THE ACFT WAS NOT GNDED.
Earlier reports · 1995–2015 · 70 reports
2015
Part: PROXIMITY SWITCH — FAULTY (LE SLAT) · airframe 94,386 hrs · 15,034 cycles
LEADING EDGE ASYM LIGHT ON AFTER TAKEOFF & FLAP RETRACTION. FLAP INDICATOR MOVED BACK & FORTH, BETWEEN UP & .5. REPLACED NR 6 INBD PROXIMITY SWITCH M281. OPERATIONALLY CHECKED NORMAL IAW MM 27-88-01.
Part: LEVER — MALFUNCTIONED (COCKPIT) · airframe 93,125 hrs · 14,818 cycles
EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING GO AROUND UNABLE TO MOVE FLAP LEVER OUT OF 25 DEGREE DETENT AT 170 KTS. LE SLAT MSG WHEN SELECTING FLAP 25. PERFORMED TE FLAP SYS ADJUSTMENT TEST IAW AMM 27-51-00. FLAP HANDLE POSITION TEST OPERATIONAL CHECK NORMAL IAW FIM 27-51-00 FLAP BINDING CHECK PROCEDURES. NO DISCREPANCIES FOUND. FSEU BITE PROCEDURES SHOWED NO FAULTS IAW FIM 27-51-815-808. SYS CHECKED NORMAL.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 91,304 hrs · 14,531 cycles
EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH RECEIVED FLAP DISAGREE WARNING WHEN FLAPS SET FOR 5 DEGREES. SWITCHED TO MANUAL, ELEC, MODE & EXTENDED FLAPS. PERFORMED CHECK OF FSEU IAW 27-51-01 & BITE OF FLAP STABILIZER POSITION MODULE IAW AMM 27-58-01 WITH NO FAULTS FOUND. R & R FSEU AS A PRECAUTION. PERFORMED TEST OF FSEU IAW AMM 27-51-01. SYS CHECKED NORMAL.
2014
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 89,569 hrs · 14,243 cycles
FLIGHT DECK EMER LIGHT INOPERATIVE. REPLACED LAMP FOR FLIGHT DECK EMER LIGHT. OPERATIONS CHECKED NORMAL.
Part: MODULE — INOPERATIVE (CABIN) · airframe 89,569 hrs · 14,243 cycles
EMERGENCY LIGHTS FOR SEAT ROWS 32HJ THRU 41HJ & AISLE LIGHTS FOR THIS AREA FAILED TEST. REPLACED M734 BATTERY MODULE. OPERATIONS CHECKED NORMAL.
Part: MODULE — INOPERATIVE (CABIN) · airframe 89,569 hrs · 14,243 cycles
EMERGENCY LIGHT ON THE RT SIDE OF THE GALLEY & RT AFT DOOR SILL LIGHT ARE INOPERATIVE. REPLACED M734 BATTERY MODULE. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,827 hrs · 14,117 cycles
EMERGENCY LIGHT AT A6 LAVATORY OUTSIDE LOWER INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT A6 LAVATORY. OPERATIONS CHECKED NORMAL.
Part: LENS — UNSECURE (CABIN) · airframe 88,827 hrs · 14,117 cycles
RIGHT AFT OVERWING INTERIOR EMER EXIT LENS FALLING OFF. REINSTALLED LENS FOR RT AFT OVERWING INTERIOR EMER EXIT. OPERATIONS CHECKED NORMAL.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 88,827 hrs · 14,117 cycles
EMERGENCY LIGHT AT SEAT 35H INOPERATIVE. RESEATED LIGHT ASSEMBLY CONNECTOR FOR SEAT 35H EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 88,357 hrs · 14,048 cycles
LEFT OVERWING EMERGENCY LIGHT AT AFT INBD FLAP INOPERATIVE. REPLACED LAMP FOR LT OVERWING EMERGENCY LIGHT AT AFT INBD FLAP, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 88,357 hrs · 14,048 cycles
RIGHT OVERWING EMERGENCY LIGHT AT AFT INBD FLAP INOPERATIVE. REPLACED LAMP FOR RT OVERWING EMERGENCY LIGHT AT AFT INBD FLAP, OPERATIONS CHECKED NORMAL.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 87,933 hrs · 13,982 cycles
SEAT EMERGENCY LIGHTS FROM 32H TO LAST ROW INOPERATIVE. RESEATED CONNECTOR TO POWER SUPPLY. OPERATIONS CHECKED NORMAL.
2013
Part: COOLING FAN — MALFUNCTIONED (E&E BAY) · airframe 84,871 hrs · 13,494 cycles
CREW REPORTED AN EQUIPMENT COOLING STATUS MESSAGE WITH ASSOCIATED ODOR IN THE COCKPIT. EMERGENCY DECLARED FLIGHT RETURNED LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED FORWARD EQUIPMENT COOLING FAN. SYSTEM GROUND CHECK NORMAL OPS.
Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 83,761 hrs · 13,326 cycles
EMERGENCY LIGHT AT 20AB INOPERATIVE. REPINNED PLUG FOR EMERGENCY LIGHT AT 20AB. OPS CHECK NORMAL.
Part: FILTER — DIRTY (CABIN) · airframe 83,761 hrs · 13,326 cycles
RDU - INFLIGHT JFK-MIA. FLIGHT ATTENDANT REPORTED BURNING RUBBER ODOR AND HAZE IN AFT CABIN DURING FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED RDU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RECIRCULATION FAN FILTERS. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SKIN — DENTED (TE FLAP) · airframe 83,761 hrs · 13,326 cycles
FOUND A LARGE DENT TO THE LEFT AFT FLAP UPPER SKIN LOCATED 55 INCHES FROM THE INBOARD EDGE AND 3.5 INCHES FROM THE TRAILING EDGE. BONDED DOUBLER OVER REPAIR AREA. PREPARED SURFACES, SEALED AND REFINISHED REPAIR PER SRM 51-70-10-2R.
2011
Part: SLIDE — DAMAGED (DOOR) · airframe 79,156 hrs · 12,591 cycles
WHILE PERFORMING, FOLLOWING WORK CARD 25-92-03 AND AFTER ADJUSTMENT OF THE LEFT HAND OVERWING ESCAPE SLIDE DOOR, REARMED SYSTEM AND SLIDE DEPLOYED. ALSO FOUND THAT THE RAILING/BUMPERS AT THE RIGHT LOWER SIDE OF THE SLIDE NEVER INFLATED DUE A HOLE ON THE SLIDE. REPLACED SLIDE AND BOTTLE.
Part: STRAP — DAMAGED (FUSELAGE) · airframe 78,682 hrs · 12,526 cycles
RIGHT BUTTLINE AT STATION 347 STABILIZATION STRAP SEVERED. ACCOMPLISHED REPAIR PER EA B767-53-018652.
Part: WEB — CRACKED (LT PYLON) · airframe 78,682 hrs · 12,526 cycles
LEFT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CABLE CUTOUT CRACKED. ACCOMPLISHED DOUBLER REPAIR PER EA 018528.
Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 77,769 hrs · 12,392 cycles
BULK CARGO FORWARD LOWER CORNER IS DAMAGED. REPAIRED LOWER CORNER OF BULK CARGO DOOR WITH FILLER AND EXTERNAL DOUBLER PER SRM 52-30-01-2R 6.
Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 77,361 hrs · 12,337 cycles
SMOKE ALARMS IN LAVATORY A6 AND A5 WENT OFF. NO SIGN OF ANY FIRE FLIGHT ATTENDANT TURNED OFF BOTH SMOKE DETECTORS. CLEANED, RESET AND TESTED SMOKE ALARMS. OPS CHECK NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 76,770 hrs · 12,230 cycles
EMERGENCY LIGHTS OUT AT SEAT 20AB THRU 24AB. REMOVED AND REPLACE POWER SUPPLY FOR EMERGENCY LIGHTS AT SEATS 20AB THRU 24AB. OPS CHECK NORMAL.
2010
Part: WIRE — SHORTED (CABIN) · airframe 76,286 hrs · 12,155 cycles
EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED SHORTED WIRE AT ROW 37AB.
Part: MODULE — INOPERATIVE (CABIN) · airframe 75,067 hrs · 11,932 cycles
LEFT AFT SEAT LIGHTING FOR EMERGENCY EXIT INOPERATIVE. REPLACED MODULE. OPS CHECKED NORMAL.
Part: LIGHT — DAMAGED (CABIN) · airframe 75,067 hrs · 11,932 cycles
SEAT 32AB EMERGENCY EXIT PATH LIGHT SMASHED AND SHORTED. REPLACED FIXTURE FOR SEAT 32AB EMERGENCY EXIT LIGHT. OPS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,926 hrs · 11,906 cycles
ESCAPE PATH LIGHTING IN AFT CABIN ROW AB 20 TO REAR INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 73,246 hrs · 11,613 cycles
LEFT AFT SLIDE GROUND EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT AFT SLIDE GROUND EMERGENCY LIGHT. OPS CHECKED NORMAL.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 73,012 hrs · 11,568 cycles
STATIONS 500 TO 522 FRAMES BETWEEN STRINGER 30 LEFT AND 31 LEFT DAMAGED. ACCOMPLISHED REPAIR PER EA B767-53-009146.
2009
Part: CIRCUIT CARD — FAILED (FIRE DETECTION) · airframe 72,394 hrs · 11,432 cycles
ON CLIMB RECEIVED ENGINE FIRE OVERHEAT MESSAGE. SYSTEM WOULD NOT RESET. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE DETECTOR CARD.
Part: WIRE — SHORTED (CABIN) · airframe 72,306 hrs · 11,414 cycles
EMERGENCY LIGHTS AT SEAT ROWS 32B TO 41B AISLE INOPERATIVE. REPAIRED SHORTED WIRES UNDER SEATS 40AB.
Part: LIGHT — BROKEN (ZONE 200) · airframe 69,634 hrs
CDG - EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR FALLING OFF AND INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHT ABOVE COCKPIT.
2008
Part: LIGHT — INOPERATIVE (EXTERIOR)
DFW EXTERIOR EMERGENCY LIGHT AT RT NR 1 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.
Part: SILL — CORRODED (FUSELAGE) · airframe 67,058 hrs · 10,586 cycles
AFW OUTER CHORD AT FORWARD CARGO DOOR CUT OUT LOWER MAIN SILL HAD CORROSION. AREA OF DISCREPANCY IS 1.2 INCH BY 1 INCH WITH A DEPTH OF .019 INCH. REPAIRED PER SRM 530001. SYSTEM GROUND CHECKED NORMAL OPS.
Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 67,058 hrs · 10,586 cycles
AFW FAIL SAFE STRAP AT FORWARD CARGO DOOR CUT OUT LOWER MAIN SILL HAD CORROSION. AREA OF DISCREPANCY IS 2 INCHES BY 1.8 INCH WITH A DEPTH OF .024 INCH. REPAIRED PER SRM 530001 AND PERFORMED HIGH FREQUENCY EDDY CURRENT TEST. NO CRACKS FOUND. SYSTEM GROUND CHECKED NORMAL OPS.
Part: LIGHT — INOPERATIVE (CABIN)
DFW EMERGENCY LIGHT AT SEAT 36B INOPERATIVE. REPLACED LAMP FOR INOPERATIVE EMERGENCY LIGHT AT SEAT 36B. SYSTEM GROUND CHECKED NORMAL OPS.
Part: BUSS — FAILED (ELECTRICAL)
LHR INFLIGHT T93/05AUG DUB TO ORD. CREW REPORTED UTILITY BUSS FAULT. LANDED LHR WITHOUT INCIDENT. REPLACED RELAYS K1 AND K2 ON ELECTRONIC CONTROL PANEL. ALSO REPLACED BUSS POWER CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
2007
Part: STRAP — BROKEN (FLASHLIGHT) · airframe 64,328 hrs
SFO - EMERGENCY FLASHLIGHT AT AFT LEFT CENTER FORWARD FLIGHT ATTENDANT POSITION HAS BROKEN STRAP. REPLACED STRAP FOR EEMRGENCY FLASHLIGHT AT AFT LEFT CENTER FORWARD FLIGHT ATTENDANT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: EXHAUST VALVE — BROKEN (EQUIP COOLING)
CVG INFLIGHT T1697/01NOV - FORWARD EQUIPMENT OVERHEAT CAUTION LIGHT ILLUMINATED. LANDED CVG WITHOUT INCIDENT. FOUND EQUIPMENT COOLING EXHAUST VALVE BROKEN. REPLACED EQUIPMENT COOLING EXHAUST VALVE AND DUCT WORK. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)
MIA - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 10GH INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 10GH. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT SEAT 35B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 35B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHT AT SEAT 22B HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (CABIN)
JFK - EMERGENCY LIGHT AT SEAT 25B INOPERATIVE. RESECURED CONNECTOR AT WALL AT SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SWITCH — OUT OF POSITION (CABIN)
GRU - AFTER AIRCRAFT TOWED TO THE REMOTE AREA, EMERGENCY LIGHT ILLUMINATED. UNABLE TO TURN OFF. FOUND FORWARD FLIGHT ATTENDANT PANEL P21 EMERGENCY LIGHT SWITCH OUT OF NORMAL CONFIGURATION. SELECTED EMERGENCY LIGHT TO NORMAL. CHARGED EMERGENCY LIGHT POWER PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SWITCH — OUT OF POSITION (CABIN)
GRU - AFTER AIRCRAFT TOWED TO THE REMOTE AREA, EMERGENCY LIGHT ILLUMINATED. UNABLE TO TURN OFF. FOUND FORWARD FLIGHT ATTENDANT PANEL P21 EMERGENCY LIGHT SWITCH OUT OF NORMAL CONFIGURATION. SELECTED EMERGENCY LIGHT TO NORMAL. CHARGED EMERGENCY LIGHT POWER PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
LAX - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 20 AND 21HJ INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 20 AND 21HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: O-RING — BLOWN (HYD INDICATOR)
LAS - EN ROUTE LAX-ORD RIGHT HAND HYDRAULIC SYSTEM QUANTITY LOSS. CONFIRMED CONTINUING LOSS OF FLUID FROM .48 TO .11 INDICATED. LANDED LAS WITHOUT INCIDENT. REPLACED BLOWN OUT O-RING ON THE HYDRAULIC DIFFERENTIAL PRESSURE INDICATOR LOCATED ON THE RIGHT ENGINE HYDRAULIC SYSTEM MODULE. SERVICED HYDRAULICS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: HINGE FITTING — CRACKED (AILERON)
AFW - RIGHT HAND AILERON HINGE FITTING HAS A TIME LIMITED REPAIR INSTALLED AT WING STATION 467. CRACK LENGTH INITIALLY MEASURED WAS 1.24 INCHES AND FINAL MEASUREMENT IS 1.70 INCHES. REMOVED TIME LIMITED REPAIR (STRAP) AND REPLACED WITH PERMANENT REPAIR (CUP). REPAIR ANGLE (CUP) FABRICATED AND FASTENED TO AILERON RIB TO PROVIDE SUPPORT FOR FIXED TRAILING EDGE PANEL STIFFENER PER MRB 767-2560 DATED 2/18/04.
Part: FITTING — CRACKED (AILERON HINGE)
AFW - RIGHT HAND INBOARD AILERON HINGE FITTING HAS A TIME LIMITED REPAIR INSTALLED AT WING STATION 467. CRACK LENGTH INITIALLY MEASURED AT 1.24 INCHES. FINAL MEASUREMENT AT 1.70 INCHES. REMOVED TIME LIMITED REPAIR (STRAP) AND REPLACED WITH PERMANENT REPAIR (CLIP). REPAIR ANGLE CLIP FABRICATED OUT OF 7075-T6 AND FASTENED TO AILERON RIB TO PROVIDE A SUPPORT FOR FIXED TRAILING EDGE PANEL STIFFENER PER MRB 767-2560 DATED 2/18/04.
2003
Part: SEAT — LOOSE (CABIN)
FOUND SEATS 33C, E, G, HAVE COME OFF BRACKET AND ARE LOOSE. SECURED SEAT 33C, E, G IAW AA MM 25-25-01-2. (M)
2002
Part: LIGHT — INOPERATIVE (CABIN)
AFW - DURING MAINTENANCE, FOUND EPL LIGHT BULBS INOPERATIVE AT SEATS 27 HJ, 26HJ, 30AB, 37HJ AND 40 HJ. REMOVED AND REPLACED EPL LIGHT BULBS AT SEATS 27HJ, 26HJ, 30AB, 37HJ AND 40 HJ. OPS CHECK NORMAL. (M)
Part: WIRE — BROKEN (CABIN)
AFW - EPL WIRE BROKE AT CONNECTORS ON HARNESS COMING FROM SIDE WALL AT SEAT 29HJ. FOUND DURING MAINTENANCE. REPAIRED CONNECTORS AT SEAT 29HJ FOR EP. OPS CHECK NORMAL. (M)
Part: CONNECTOR — LOOSE (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE FLOOR PATH LIGHTING AT ROWS 29 INOPERATIVE. RE-SECURED CONNECTOR AT SIDE WALL FOR EMERGENCY ESCAPE FLOOR PATH LIGHTING AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: WIRE — DAMAGED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 26J INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE AT SEAT 26J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — BROKEN (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: FIRE LOOP — INOPERATIVE (RT ENGINE)
JFK - FLT 48 - DURING FLIGHT, RIGHT ENGINE FIRE DETECTION LOOP 2 CYCLED ON AND OFF. ON STEADY FOR APPROXIMATELY 10 MINUTES THEN STARTED TO CYCLE ON AND OFF. DIVERTED AND LANDED JFK WITHOUT INCIDENT. REPLACED FIRE DETECTION LOOP 2 HARNESS. SYSTEM GROUND CHECK NORMAL OPERATION. REPLACED ALL THREE DETECTORS AS PRECAUTION. (M)
1999
Part: OVEN — DIRTY (GALLEY)
MAD - FLT 0068 - EN ROUTE MIA/MAD, NR 2 FIRST CLASS GALLEY OVEN EMITTED SMOKE AND SPARKS. CIRCUIT BREAKER PULLED AND AIRCRAFT CONTINUED TO MAD AND LANDED WITHOUT INCIDENT. CLEANED DIRT AND FOOD RESIDUE FROM NR 2 FIRST CLASS CABIN OVEN AND FAN. OVEN OPERATED FOR 20 MINUTES AT ALL POWER SETTINGS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1998
Part: FLOORBEAM — CORRODED (BS 1480)
AFW - FLOORBEAM AT STATION 1480 HAS CORROSION. BLEND OUT ALL CORROSION, ALODINE ALL BARE SURFACES FINISH WITH 2 COATS OF PRIMED FILL BLENDED AREA WITH BMS PER MRB 767-1693. (M)
Part: FLOORBEAM — CORRODED (BS 347)
AFW - FLOORBEAM STATION 347 HAS CORROSION REMOVAL ON UPPER SURFACE. FABRICATE REPAIR STRAPS, ALODINE ALL BARE ALUMINUM FILL BLENDS WITH BMS. INSTALL REPAIR STRAP WET WITH SEALANT PER MRB 767-1701. (M)
Part: FLOORBEAM — CORRODED (BS 347)
AFW - FLOORBEAM AT STATION 347 AND APPROX RBL 50 HAD CORROSION BLENDED. FABRICATE REPAIR STRAPS, ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS PER MRB 767-1695. (M)
Part: FLOORBEAM — CORRODED (BS 904)
AFW - FLOORBEAM AT STATION 904 LBL 33 HAD CORROSION BLENDED ON TOP SURFACE. BLEND OUT GOUGES, ENSURED THAT ALL DAMAGE HAS BEEN REMOVED. ROTO/FLAP PEEN BLENDED AREA PER SRM 51-20-06 ALODINE AND APPLY 2 COATS OF PRIMER FILL WITH BMS-5-95 REF MRB 767-1703. (M)
Part: CONNECTOR — FAILED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 41H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FIRE LOOP — MALFUNCTIONED (LT ENGINE)
GIG - FLT 904 - LT ENGINE FIRE LOOP 1 STATUS MSG WILL NOT ERASE FIRE LOOP DEF INOP AS PER MEL REF MIC SHEET ENTERED. REPLACED LOWER FWD LOOP AND UPPER AFT LOOP FOR LEFT ENGINE PER MM. OPS CHECK NORMAL. REMOVED PLACARD AND CLRD MIC SHEET. (M)
Part: CONNECTOR — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH MARKING LIGHTS INOPERATIVE AT PASSENGER SEAT 37HJ. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT CONNECTOR PASSENGER SEAT 37HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: CONNECTOR — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH MARKING LIGHTS INOPERATIVE AT PASSENGER SEAT 24HJ. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT CONNECTOR PASSENGER SEAT 24HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: CONNECTOR — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT CONNECTOR PASSENGER SEAT 29HJ. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT CONNECTOR PASSENGER SEAT 29HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1997
Part: WIRE — SHORTED (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 32H FOUND INOPERATIVE. REPAIRED SHORTED WIRE AT SEAT 32H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1996
Part: OVEN — DIRTY (GALLEY)
BRU - FLT 88 - EN ROUTE ORD/BRU DURING CRUISE, NR 2 OVEN EMITTED SMOKE WHEN DOOR OPENED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO BRU, LANDING WITHOUT INCIDENT. CLEANED INTERIOR OF NR 2 OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO SMOKE NOTED. (M)
1995
Part: EEL — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR PROXIMITY AISLE LIGHTS AT MID GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR PROXIMITY AISLE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z)
Part: EEL WIRE — DISCONNECTED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEATS 7H AND 21H FOUND INOPERATIVE. SECURED DISCONNECTED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKS NORMAL OPERATION. (X)