N380AN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERICAN AIRLINES, INC. (AALA) | Operator | on 2010-04-13 | Operator named in NTSB report |
Accident & incident history
Operated by AMERICAN AIRLINES INC (per NTSB report)
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.
96 reports on file, 1995-03-28 – 2017-07-28.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 96,685 hrs · 15,517 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY LED FLASHLIGHT AT THE FORWARD LEFT JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY PER AMM 25-60-00. OPERATIONAL CHECK GOOD.
Part: LENS — MISSING (CABIN) · airframe 96,685 hrs · 15,517 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT SEAT 20B HAS A MISSING LENS COVER. INSTALLED LENS COVER PER AMM 33-51-10. OPERATIONAL CHECK GOOD.
Part: DISPLAY — FAILED (F/O) · airframe 96,631 hrs · 15,505 cycles
FIRST OFFICER`S MULTI-PURPOSE CONTROL DISPLAY UNIT FAILED. EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE. UNEVENTFUL LANDING. REMOVED AND REPLACED LEFT FLAT PANEL DISPLAY UNIT IAW AMM 34-22-11. OPS CHECKED GOOD.
Part: LENS — BROKEN (CABIN) · airframe 96,400 hrs · 15,468 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT AISLE LIGHT BY THE FORWARD GALLEY HAS A BROKEN LENS COVER. REPLACED LENS COVER. OPERATIONAL CHECK GOOD.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 96,336 hrs · 15,454 cycles
AIRCRAFT WAS NOT GROUNDED. CEILING EMERGENCY EXIT LIGHTS FROM ROWS 13B TO 31B AND SEAT EMERGENCY ESCAPE PATH LIGHTS FROM SEATS 20B TO 24B ARE INOPERATIVE. RESEATED LOOSE CONNECTOR D1088 AT M737 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 96,092 hrs · 15,405 cycles
FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE L4 DOOR IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-01. OPS CHECKED GOOD.
Part: FLASHLIGHT — MISSING (CABIN) · airframe 96,063 hrs · 15,401 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IS MISSING IN THE FORWARD GALLEY, AFT WALL, CENTER RIGHT SEAT. INSTALLED FLASHLIGHT IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.
Part: FLASHLIGHT — MISSING (CABIN) · airframe 96,063 hrs · 15,401 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IS MISSING IN THE FORWARD GALLEY, AFT WALL, CENTER LEFT SEAT. INSTALLED FLASHLIGHT IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.
Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 95,661 hrs · 15,323 cycles
EMERGENCY EXIT SIGN AT ROW 20 HJ IS DETACHED FROM WALL. SECURED THE CAMLOCKS ON PANEL. OPERATIONAL CHECKED GOOD.
Part: SPRING — LACK OF LUBE (L1 DOOR) · airframe 95,632 hrs · 15,312 cycles
AIRCRAFT WAS NOT GROUNDED. L1 DOOR WILL NOT GIVE CLOSED INDICATION FROM INSIDE WITH AUTO OPERATION. IT WILL CLOSE OUTSIDE MANUALLY. LUBED DOOR HANDLE SPRING. L1 DOOR LOCKS AND UNLOCKS IAW AMM 52-00-00. ALL COCKPIT INDICATIONS ARE NORMAL.
Part: ARMING LEVER — OBSTRUCTED (L1 DOOR) · airframe 95,424 hrs · 15,254 cycles
AIRCRAFT WAS NOT GROUNDED. L1 DOOR IS DIFFICULT TO ARM. REQUIRES REPEATED CYCLING OF HANDLE. REMOVED DEBRIS FROM GIRT BAR ARM/DISARM HANDLE. OPERATIONAL CHECK GOOD.
Part: CIRCUIT BREAKER — FAULTY (ZONE 200) · airframe 95,044 hrs · 15,154 cycles
AIRCRAFT WAS GROUNDED. STRONG ELECTRICAL BURNING ODOR AT L1 DOOR WHICH DISSIPATED AFTER ENGINES WERE SHUT DOWN. REMOVED AND REPLACED LEFT GENERATOR CONTROL UNIT(AALA20170110021), LEFT GENERATOR CIRCUIT BREAKER C901 AND LEFT BUS TIE BREAKER C902(AALA20170110023). OPERATIONAL CHECK GOOD.
Part: CIRCUIT BREAKER — FAULTY (ZONE 200) · airframe 95,044 hrs · 15,154 cycles
AIRCRAFT WAS GROUNDED. STRONG ELECTRICAL BURNING ODOR AT L1 DOOR WHICH DISSIPATED AFTER ENGINES WERE SHUT DOWN. REMOVED AND REPLACED LEFT GENERATOR CONTROL UNIT(AALA20170110021), LEFT GENERATOR CIRCUIT BREAKER C901(AALA20170110022) AND LEFT BUS TIE BREAKER C902. OPERATIONAL CHECK GOOD.
Part: GCU — FAULTY (ZONE 200) · airframe 95,044 hrs · 15,154 cycles
AIRCRAFT WAS GROUNDED. STRONG ELECTRICAL BURNING ODOR AT L1 DOOR WHICH DISSIPATED AFTER ENGINES WERE SHUT DOWN. REMOVED AND REPLACED LEFT GENERATOR CONTROL UNIT, LEFT GENERATOR CIRCUIT BREAKER C901(AALA20170110022) AND LEFT BUS TIE BREAKER C902(AALA20170110023). OPERATIONAL CHECK GOOD.
Part: IDG — FAILED (LEFT) · airframe 95,044 hrs · 15,153 cycles
LEFT GENERATOR FAILED DURING CLIMB. EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE. LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE LEFT IDG. OPS CHECKED GOOD.
Earlier reports · 1995–2016 · 81 reports
2016
Part: BULB — BURNED OUT (MLG INDICATOR) · airframe 94,685 hrs · 15,075 cycles
DURING APPROACH WHEN GEAR EXTENDED, OBSERVED ALL THREE GEAR GREEN LIGHTS ILLUMINATE FOLLOWED BY EXTINGUISHING OF LEFT MAIN GEAR GREEN LIGHT. EMERGENCY DECLARED. LANDING UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED BOTH LEFT MAIN GEAR GREEN LIGHT INDICATOR BULBS.
Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 94,617 hrs · 15,062 cycles
SEAT MOUNTED EMERGENCY PATH LIGHTS INOPERATIVE FOR SEATS 32H THROUGH 41H. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY ASSEMBLY AT M734 IAW AMM 33-60-98. REPAIRED SHORTED WIRES AT SEAT 32H. OPERATIONAL CHECK GOOD. REFERENCE AALA20161122004 AND AALA20161122005.
Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 94,617 hrs · 15,062 cycles
SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE FOR SEATS 32H THROUGH 41H. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY ASSEMBLY AT M734 IAW AMM 33-60-98. REPAIRED SHORTED WIRES AT SEAT 32H. OPERATIONAL CHECK GOOD.
Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 94,617 hrs · 15,062 cycles
SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE FOR SEATS 32H THROUGH 41H. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY ASSEMBLY AT M734 IAW AMM 33-60-98. REPAIRED SHORTED WIRES AT SEAT 32H. OPERATIONAL CHECK GOOD.
Part: ACCESS PANEL — MISSING (ZONE 100) · airframe 92,409 hrs · 14,614 cycles
AIRCRAFT WAS GNDED. FOUND HYD SERVICE PANEL 149BL MISSING. INSTALLED PANEL IAW AMM 52-49-10.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,872 hrs · 14,502 cycles
AFT CARGO, STRINGER 34R CORRODED, JUST AFT OF STATION 1351 & SPREADING FWD UNDER BALL MAT MOUNT BOX. REMOVED CORRODED STRINGER SECTIONS & REPAIRED IAW SRM 53-00-03-2R-2 & EA 257277. ACFT IN BASE MX.
Part: WIRE — DAMAGED (CABIN) · airframe 91,872 hrs · 14,502 cycles
AIRCRAFT WAS IN BASE MX. PATHWAY LIGHT AT SEAT 32AB FAILED TO ILLUMINATE. FOUND & REPAIRED DAMAGED WIRE AT M739 IAW 20 20-30-12.
Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,872 hrs · 14,502 cycles
AIRCRAFT WAS IN BASE MX. FLOORBEAM CHANNEL ATTACHED PLATE & FASTENERS AT FS 764 ARE CORRODED, BETWEEN RBL 23 & 26. REPAIRED IAW SRM 53-00-51-2R-1.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 91,872 hrs · 14,502 cycles
AIRCRAFT WAS IN BASE MX. LT WING UPPER SKIN HAS TWO CORRODED AREAS UNDER THE WING TO BODY FAIRING, JUST BELOW & AFT OF THE AFT EMER EXIT HATCH. REPAIRED IAW EA 257121.
Part: FRAME — CRACKED (FUSELAGE) · airframe 91,872 hrs · 14,502 cycles
AIRCRAFT WAS IN BASE MX. DURING ACCOMPLISHMENT OF ECO C3241AC_0001, A CRACK WAS FOUND IN THE RT SIDE OF THE MAIN FRAME AT FS 883.5. ACCOMPLISHED ECO C3241AC_0001 WITH EA 257316.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,872 hrs · 14,502 cycles
AIRCRAFT WAS IN BASE MX. SHEAR TIE AT FS 1395, BETWEEN STRINGER 38L & 39L IS CORRODED. REMOVED SHEAR TIE, FABRICATED REPLACEMENT SHEAR TIE FROM SAMPLE ON SHOP ORDER C7NU, INSTALLED REPLACEMENT SHEAR TIE IAW SRM 51-10-02-0G.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,872 hrs · 14,502 cycles
AIRCRAFT WAS IN BASE MX. UPPER CHORD OF CABIN FLOORBEAM AT FS 347 IS CORRODED, AROUND SCREW HOLES, BETWEEN RBL 55 & RBL 74. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1, 51-10-02-0G, 51-40-02-0G, 51-20-01-0G, EA 256937 & 257128.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,872 hrs · 14,502 cycles
AIRCRAFT WAS IN BASE MX. UPPER CHORD OF CABIN FLOORBEAM AT FS 325 IS CORRODED, BETWEEN RBL 20 & RBL 50. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1, 51-40-02-0G & 51-10-02-0G.
2015
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,872 hrs · 14,502 cycles
AIRCRAFT WAS IN BASE MX. FLOORBEAM CORRODED AT FS 654 + 44 INCHES & RBL 6. REPAIRED FLOORBEAM IAW SRM 53-00-07-2R.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 91,872 hrs · 14,502 cycles
AIRCRAFT WAS IN BASE MX. EMER EXIT LIGHT AT SEAT 25AB IS INOPERATIVE. R & R POWER SUPPLY M739 IAW AMM 33-51-07.
Part: LIGHT — CORRODED (ZONE 200) · airframe 91,872 hrs · 14,502 cycles
LEFT FWD OVERWING EGRESS LIGHT IS DIM. REPLACED LIGHT ASSEMBLY IAW AARD 51-00-05. THE ACFT WAS NOT GNDED.
Part: POWERPACK — DISCHARGED (CABIN) · airframe 91,753 hrs · 14,476 cycles
RIGHT AFT FUSELAGE EMER LIGHTS INOPERATIVE. R & R EMER LIGHTS POWER PACK AT ROW 39 RT IAW AMM 33-51-00. OPERATIONALLY CHECKED NORMAL.
Part: INDICATOR — LEAKING (HYDRAULIC SYS) · airframe 91,670 hrs · 14,457 cycles
EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. HYD QTY IN CTR TANK SLOWLY BLEED DOWN TO 0.03 & C SYS HYD PRESS FAILED. FOUND HYD LEAKING FROM DIFFERENTIAL PRESS INDICATOR AT FILTER MODULE. R & R INDICATOR IAW AMM 29-11-19. OPERATIONAL & LEAK CHECK OK IAW AMM 29-11-02.
Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 90,564 hrs · 14,267 cycles
AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB RECEIVED LT ENG PRESS REGULATING VLV EICAS MSG, LT ENG BLEED LIGHT ILLUMINATED. R & R LT PRESS REGULATING VLV CONTROLLER IAW AMM 36-11-19. ACCOMPLISHED ALL REQUIRED CHECKS & ENG RUN IAW AMM 71-00-00. SYS CHECKED NORMAL.
Part: LUG — LOOSE (IDG) · airframe 89,495 hrs · 14,088 cycles
RETURNED DUE TO CAPTAIN FLIGHT INSTRUMENT TRANSFER BUSS STATUS MESSAGE ILLUMINATED. EMERGENCY DECLARED, LANDING UNEVENTFUL. REPLACED CAPTAINS INSTRUMENT BUSS VOLTAGE SENSING UNIT. SYS CHECKED NORMAL. DISCREPANCY REPEATED 3/23 & 3/25. FOUND THE NEUTRAL LUG HARDWARE NOT PROPERLY TORQUED & LOOSE. SECURED INSTALLATION. PERFORMED ENGINE RUN & VERIFIED LT IDG OPERATED NORMALLY.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,468 hrs · 14,083 cycles
RIGHT SIDE AISLE OVERHEAD EXIT IDENTIFIER SIGN ADJACENT TO RT OVERWING EXIT DOORS & SEVERAL ASSOCIATED SEAT MOUNTED ESCAPE PATH LIGHTS INOPERATIVE. R & R BATTERY PACK & CHARGER ASSEMBLY M00723 IAW AMM 33-51-07. SYS CHECKED NORMAL.
2014
Part: TIRE — FAILED (MLG) · airframe 88,866 hrs · 13,960 cycles
ON LANDING, NR 3 & 4 TIRES BLEW. REPLACED NR 3 & 4 TIRES.
Part: TRANSDUCER — INOPERATIVE (MLG) · airframe 88,111 hrs · 13,836 cycles
AIRCRAFT HAD A MAIN BREAK ISSUE. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 8 WHEEL TRANSDUCER. SYS GND CHECKED NORMAL, OPERATION CLOSED.
Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 87,352 hrs · 13,709 cycles
LEFT NR 1 DOOR WAS NOT DISARMED PRIOR TO OPENING. SLIDE PARTIALLY DEPLOYED. REPLACED LT NR 1 DOOR SLIDE.
Part: SKIN — DENTED (FUSELAGE) · airframe 87,352 hrs · 13,709 cycles
DENT IN LOWER FUSELAGE AT STATION 1197+66 & STRINGER 33 LT. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01-2R-14, SRM 53-00-01-2R-29 & SUPPORTING EA B767-53-035965.
Part: LIGHT — DEFECTIVE (EXTERIOR) · airframe 87,170 hrs · 13,672 cycles
LEFT CTR OVERWING EXTERNAL EMER EGRESS LIGHTS EXTREMELY DIM. REPLACED LAMP FOR LT CTR OVERWING EXTERNAL EMER EGRESS LIGHT. OPERATIONS CHECKED NORMAL.
2013
Part: ACTUATOR — BLOWN (ZONE 100) · airframe 84,972 hrs · 13,322 cycles
NR 6 SPOILER OVERRIDE ACTUATOR FOR OVERWING SLIDE SYSTEM, PISTON EXTENDED ABOUT A QUARTER INCH & IS IN CONTACT WITH SPOILER ROLLER ARM. R & R NR 6 SPOILER OVERRIDE ACTUATOR FOR OVERWING SLIDE SYSTEM.
Part: CHARGER — INOPERATIVE (MAIN BATTERY) · airframe 84,015 hrs · 13,172 cycles
GYE INFLIGHT MIA-LIM CREW REPORTED MAIN BATTERY CHARGER EICAS MESSAGE. FLIGHT DIVERTED GYE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SWAPPED OUT MAIN BATTERY CHARGER WITH AUXILIARY POWER UNIT BATTERY CHARGER & MESSAGE CLEARED. REPLACED APU BATTERY CHARGER AT MIA ON 10/02/2013. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 83,963 hrs · 13,165 cycles
EMERGENCY LIGHTS ESCAPE PATH SEATS 32HJ THROUGH 41HJ INOPERATIVE. UNDER SIDE WALL BOTTOM SEATS 40J FOUND DISCONNECTED PLUG. RECONNECTED AT BATTERY PACK. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,963 hrs · 13,165 cycles
SEAT 29B EMERGENCY PATH LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 29B. OPERATIONS CHECKED NORMAL.
Part: LIGHT — MISSING (CABIN) · airframe 83,961 hrs · 13,164 cycles
SEAT 29B EMERGENCY LIGHT PATH MISSING LAMP. REPLACED LAMP FOR SEAT 29B SEAT MOUNTED EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL
Part: PIN — NOT SEATED (EMERGENCY LIGHT) · airframe 82,237 hrs · 12,887 cycles
SEAT 20 H-J EMERGENCY LIGHT LAMPS INOPERATIVE. RESEATED PIN. OP CHECK NORMAL.
2012
Part: SHUTOFF VALVE — FAILED (HYDRUALIC SYS) · airframe 81,698 hrs · 12,804 cycles
JFK - CREW REPORTED HEARING LOUD BANG DURING GEAR RETRACTION AND CENTER HYDRAULIC SYSTEM PRESSURE LIGHT ILLUMINATED. FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HYDRAULIC PUMP REGULATOR SHUTOFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: ACTUATOR — FAILED (LT SPOILER) · airframe 79,874 hrs · 12,534 cycles
LEFT SPOILER ACTUATOR OVERIDE FAILED. REPLACED SPOILER OVERIDE ACTUATOR. OPS CHECK NORMAL.
Part: BRAKE — SEIZED (NR 8 WHEEL) · airframe 78,166 hrs · 12,259 cycles
NUMBER 8 WHEEL FOUND TO BE DAMAGED AND MATERIAL GROUND AWAY FROM WHEEL ASSEMBLY. BRAKE SEMI LOCKED. REPLACED NUMBER 8 BRAKE ASSEMBLY. REPLACED NUMBERS 7 AND 8 WHEEL AND TIRE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL.
2011
Part: WEB — CRACKED (LT PYLON) · airframe 76,615 hrs · 12,019 cycles
LEFT PYLON FORWARD UPPER WEB CRACK REPAIR AT POWER FEEDER CABLE CUTOUT. ACCOMPLISHED DOUBLER REPAIR PER EA B767-54-019251.
Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 74,535 hrs · 11,688 cycles
LHR - CREW REPORTED NUMBER 8 COFFEEMAKER HAS STRONG ELECTRICAL ODOR. FLIGHT LANDED LHR WITHOUT INCIDENT. REPLACED NUMBER 8 COFFEEMAKER. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: STRUT — FAULTY (NLG) · airframe 72,652 hrs · 11,383 cycles
JFK - CREW REPORTED FLAP CONFIGURATION WARNINGS DURING TAKEOFF. EMERGENCY DECLARED RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND PROBLEM RELATED TO NOSE LANDING GEAR STRUT ASSEMBLY. REPLACED NOSE LANDING GEAR ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: RELAY — FAULTY (WARNING SYSTEM) · airframe 72,651 hrs · 11,381 cycles
JFK - CREW REPORTED FLAP/SLAT DISAGREE CONFIGURATION WARNING DURING CLIMB. EMERGENCY DECLARED RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED K215 RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 70,797 hrs · 11,032 cycles
FRAME STATIONS 500 TO 522 BETWEEN STRINGERS 30 AND 31 LEFT DAMAGED. ACCOMPLISHED REPAIR PER EA B767-53-009500.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,797 hrs · 11,032 cycles
STATION 347 FLOORBEAM UPPER CAP RIGHT BUTTLINES 34 TO 55 CORRODED. ACCOMPLISHED REPAIR PER EA 009619.
2009
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 66,915 hrs
SFO - EMERGENCY LIGHTS LEFT COLUMN ON SEATS FROM ROW 32 THRU 42 INOPERATIVE. REPLACED BATTERY PACK FOR ROWS 32 THRU 42.
2008
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · 65,449 cycles
JFK EMERGENCY LIGHTS AT LT AND RT NR 1 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LT AND RT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.
Part: BUSHING — CORRODED (PYLONS) · airframe 65,262 hrs · 10,129 cycles
AFW RT UPPER SPAR FITTING HAD PITTING ON BUSHINGS. REPAIRED PER SRM 54 52 90 2R WITH THE FOLLOWING DEVATION. AFTER PERFORMING STEP 5 IT IS ACCEPTABLE TO SKIP TO STEP 16.
2007
Part: PUMP — LEAKING (HYD SYSTEM)
DFW INFLIGHT T963/20OCT - RIGHT HYDRAULIC QUANTITY LIGHT ILLUMINATED WITH LOSS OF PRESSURE. FLIGHT DUMPED 33000 POUNDS OF FUEL AT FLIGHT LEVEL 330. FOUND DAMAGED O-RING IN RIGHT PYLON. LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT ENGINE DRIVEN PUMP AND BOTH FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: STRAP — DAMAGED (BS 1725)
AFW - CHORD STRAP AT STATION 1725 WAS DAMAGED. TRIMMED OUT DAMAGED PORTION OF CHORD STRAP. FABRICATED A REPAIR PIECE USING 7075 T6 0.125 INCH THICK MATERIAL. INSTALLED THE REPAIR PIECE USING RIVETS OF THE SAME TYPE AND SIZE AS THE ORIGINAL.
Part: LENS — MISSING (CABIN)
MIA EMERGENCY LIGHT AT SEAT 13H HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 13H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
Part: BATTERY PACK — DISCHARGED (CABIN)
MIA EMERGENCY LIGHTS FROM SEAT ROWS 30B TO 35B INOPERATIVE. RECHARGED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 30B TO 35B. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
2006
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT SEAT 24H INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 24H. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHTS)
MIA - EMERGENCY LIGHT AT SEAT 24H HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24H. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT SEATS 3B, 21B, AND 25B INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT SEATS 3B, 21B, AND 25B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — LOOSE (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT LENS AT AFT LEFT HAND DOOR LOOSE. SECURED EMERGENCY LIGHT LENS AT AFT LEFT HAND DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHTS AT SEATS 32H AND 36H INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 32H AND REPINNED CONNECTOR AT SEAT 36H FOR INOPERATIVE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DFW - EMERGENCY PATH LIGHT FROM SEAT 24D TO 41D INOPERATIVE. REPLACED BATTERY PACK M734 FOR INOPERATIVE EMERGENCY PATH LIGHT FROM SEAT 24D TO 41D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHT)
DFW - EMERGENCY PATH LIGHT AT SEAT 3B HAS MISSING LENS. REPLACED EMERGENCY PATH LIGHT LENS AT SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: POWER SUPPLY — DISCHARGED (CABIN)
JFK - EMERGENCY PROXIMITY LIGHTS AT ROWS 20A TO 24B ARE INOPERATIVE. REPLACED POWER SUPPLY M737 FOR EMERGENCY PROXIMITY LIGHTS AT ROWS 20A TO 24B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
LAX - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 20 THROUGH 24AB INOPERATIVE. REPLACED BATTERY PACK AT M737 FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 20 THROUGH 24AB. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
LAX - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 20B TO 24B INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 20B TO 24B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: WIRE — BROKEN (GALLEY)
SFO ARROW EMERGENCY LIGHT BEHIND AFT RT GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR ARROW EMERGENCY LIGHT BEHIND AFT RT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED
Part: TERMINAL — BROKEN (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHT FORWARD OF M-2 LAVATORY INOPERATIVE. REPLACED BROKEN TERMINAL AT EMERGENCY EXIT CEILING LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: PIN — BROKEN (CONNECTOR)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32B INOPERATIVE. REPLACED BROKEN PINS AT CONNECTOR AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 21H INOPERATIVE. RESECURED LOOSE CONNECTOR AT SEAT 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — INOPERATIVE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEATS 21B AND 23B INOPERATIVE. REPAIRED PUSH PIN TO CONNECTOR AT SEATS 21B AND 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: PROXIMITY SWITCH — MALFUNCTIONED (MLG)
DFW - FLT 2485 - UPON LANDING, GEAR DOOR AMBER LIGHT REMAINED ON AFTER GEAR EXTENSION FOR 20 TO 25 SECONDS. EICAS AMBER GEAR DOOR WARNING SOUNDED AFTER GO-AROUND. GEAR LEFT DOWN UNTIL LANDING. REPLACED UPLOCK PROXIMITY SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1999
Part: CONNECTOR — LOOSE (ROW 9H)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON SIDE OF SEAT 9H INOPERATIVE. RESEATED SEAT EMERGENCY EXIT LIGHT CONNECTOR FOR SEAT 9H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: WIRE — BROKEN (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTS AT SEAT 21B INOPERATIVE. REPAIRED WIRE AT SEAT 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — FAILED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTS AT SEAT 33H INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR LIGHT CONNECTOR AT SEAT 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — FAILED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR LIGHTS AT SEAT 41B INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR LIGHT CONNECTOR AT SEAT 41B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT SEAT 20 THROUGH 31 INOPERATIVE. REPLACED TWO EMERGENCY EXIT SEAT LIGHT CONNECTORS AND BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SMOKE DETECTOR — DIRTY (FWD LAVATORY)
LHR - DURING CRUISE JFK-LHR, FORWARD LAVATORY FIRE DETECTION LIGHTS ILLUMINATED INTERMITTENTLY. CLEANED FORWARD LAVATORY SMOKE DETECTOR AND LAVATORY COMPARTMENT INSPECTION REVEALED NO FURTHER ABNORMALITIES. SYSTEM GROUND CHECKED NROMAL OPERATION. (M)
Part: CONNECTOR — BROKEN (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 21H INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: MODULE — MISSING (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EVACUATION ALERT MODULE WAS MISSING AT FLIGHT ATTENDANT STATION RIGHT SIDE NEAR MID GALLEY. REPLACED MISSING EMERGENCY EVACUATION ALERT MODULE AT FLT ATTENDANT STATION RIGHT SIDE NEAR MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: FLOOR BEAM — CORRODED (BS 346)
AFW - FLOOR BEAM HAD CORROSION BEYOND SRM LIMITS IN DEPTH, BUT WITHIN LIMITS PER CROSS-SECTION REMOVED. ALODINED AND REFINISHED AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1448. TST: 190,457.26 HOURS. CYCLES, 2,975. (X)
Part: IDG — FAILED (RT ENGINE)
LAX - RT GEN DRIVE LIGHT ON EICAS IDG DISCONNECTED PER PROCEDURE. REMOVED AND REPLACED RT ENG IDG PER MM 24-11-00-5. ACCOMPLISHED OPS CHECK. (M)
Part: VCR PLAYER — ELECTRICAL ODOR (CABIN)
LHR - FLT 142 - EN ROUTE JFK/LHR, DURING CRUISE, ELECTRICAL ODOR NOTED COMING FROM MAIN VIDE SYSTEM OPPOSITE BUSINESS CLASS GALLEY. TURNED OFF VIDEO UNIT NR 1 AND ODOR WENT AWAY. AIRCRAFT PROCEEDED TO LHR AND LANDED WITHOUT INCIDENT. REPLACED NR 1 MAIN VCR PLAYER. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ODOR NOTED. (M)
1996
Part: WARMING CART — FAILED (GALLEY)
LHR - FLT 116 - EN ROUTE JFK/LHR DURING CRUISE, SLIGHT SMOKE NOTED IN B/C GALLEY WHEN WARMING CART AND OVEN TURNED ON. TURNED OFF B/C GALLEY WARMING CART AND OVEN AND AIRCRAFT PROCEEDED TO LHR, LANDING WITHOUT INCIDENT. WARMING CART REPLACED BY CATERING AND B/C GALLEY OVEN PLACARDED INOPERATIVE. SUBSEQUENTLY AT SFO/18, B/C GALLEY OVEN OPERATION CHECKED BY RUNNING AT 375 DEGREES FOR ONE HOUR WITH NO SMOKE NOTED. UNABLE TO DUPLICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. (M)
Part: FLOOR BEAM — CORRODED (BS 865)
AFW - FLOOR BEAM AT LBL 33, STA 865, HAS CORROSION. REPAIRED PER MRB 767-1136. TST: 12,783.33 HRS. CYCLES, 2,028. (X)
1995
Part: FUSE — FAILED (POWER SUPPLY)
SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR LIGHTS INOP, BETWEEN BUSINESS AND COACH. REPLACED FUSE IN EMERGENCY POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT ASSY — FAILED (CABIN)
SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 17B INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL CONNECTOR — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PASSENGER SEAT ROW 36H AND AFT GALLEY INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 42H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 25JH THROUGH 35JH INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH CONNECTOR AT SEAT ROW 25JH. SYSTEM GROUND CHECKS NORMAL OPERATION. (Z)