N342AN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERICAN AIRLINES, INC. (AALA) | Operator | on 2018-05-08 | Operator named in NTSB report |
Accident & incident history
Operated by American Airlines (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.
114 reports on file, 2003-03-10 – 2022-01-28.
Part: FAIRLEAD — DAMAGED (ELEVATOR) · airframe 63,521 hrs · 10,722 cycles
FOLLOWING AN INVESTIGATION FOR A MISSING GROMMET ON A ELEVATOR CABLE FAIRLEAD AT BS999 IT WAS IDENTIFIED THAT THE FAIRLEAD WAS REWORKED AND EXTREMELY CLOSE TO TURNBUCKLES, AIRCRAFT AIPC SHOWED NO FAIRLEAD P/NO: INSTALLED AT THIS LOCATION. AIRCRAFT CARGO CONVERSION COMPANY ASKED FOR MORE INFORMATION ON FAIRLEAD. CARGO CONVERSION COMPANY RESPONSE GAVE LOCATIONS OF FAIRLEAD AND IDLER PULLEYS FOR ELEVATOR AND RUDDER CABLES AT MULTIPLE BS LOCATIONS FAIRLEADS MISSING, FAIRLEADS ALSO IDENTIFIED INSTALLED AT INCORRECT LOCATIONS PER CONVERSION DRAWINGS SUPPLIED. A NUMBER OF MISSING IDLER PULLEYS BETWEEN BS654 AN BS1219 ALSO IDENTIFIED FOLLOWING INSPECTION. ELEVATOR CABLE DAMAGE EVIDENT FROM INSPECTION.
Earlier reports · 2003–2021 · 113 reports
2021
Part: NONE — NONE · airframe 63,521 hrs · 10,722 cycles
DURING A FWD ENTRY DOOR CLOSING OPERATION TASK, THE VIEWING WINDOW/PRISM WAS IDENTIFIED NOT INSTALLED CORRECTLY PER AMM. THE VIEWING WINDOW/PRISM WAS DISLODGED FROM ITS CORRECT INSTALLED POSITION AND THE RETAINING HARDWARE IDENTIFIED AS NOT WITHIN AMM REQUIRED FASTENER TORQUE TOLERANCES.
Part: PRESSURE SWITCH — DISCONNECTED (FIRE BOTTLE)
DURING INSPECTION OF THE CARGO FIRE BOTTLE IT WAS IDENTIFIED THE PRESURE SENSING SWITCHES WERE NOT INSTALLED AS PER AMM INSTRUCTION. THE PRESSURE SENSING SWITCHES WERE FOUND DISCONNECTED FROM THEIR CORRECT INSTALLED POSIITONS.
2019
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
R/H WING, OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY M731 IAW MM 33-51-07. OPS CHECK GOOD. IAW MM 33-51-00.
Part: GEARBOX — BINDING (SERVO MOTOR) · airframe 62,205 hrs · 10,375 cycles
AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS BOTH AIRCRAFT THROTTLES REALLY HARD TO MOVE AND BINDING. FOUND SERVO MOTOR GEARBOX BINDING. REMOVED AND REPLACED SERVOMOTOR GEARBOX & SERVOMOTOR GENERATOR IAW AMM 22-32-01. THRUST LEVER LOADS FOR #1 & #2 ENG WITHIN LIMITS IAW AMM 76-11-06.
Part: IDG — FAILED (RT GENERATOR) · airframe 61,473 hrs · 10,235 cycles
AIRCRAFT WAS GROUNDED: PILOT REPORTS UPON REACHING TAKEOFF THRUST, R GEN DRIVE DISCONNECT ILLUMINATED. (ASSOCIATED R GEN OFF AND L 7 R UTILITY BUSS OFF). FOLLOWED QRH PROCEDURE FOR R GEN DRIVE DISCONNECT. MAINTENANCE REMOVED/REPLACED RIGHT IDG IAW AMM:24-11-01. OPS CHECK, LEAK CHECK GOOD.
Part: LINE — LOOSE (LT ENGINE) · airframe 60,692 hrs · 10,079 cycles
AIRCRAFT WAS GROUNDED: PILOT REPORTS FROM DECENT UNITL 2000' LEFT ENGINE N1 RAGED FROM 10 TO 27 DIFFERENCE WITH ALL GAUGES MATCHING AND ADVERSE YAW. MAINTENANCE FOUND COMPRESSOR BLEED PRESSURE MUSCLE LINE NEAR MAIN ENGINE CONTROL LOOSE AND RE-SECURED. PERFORMED FLIGHT/GROUND IDLE SOLENOID TEST IAW AMM 73-21-04 AND IDLE SPEED TEST IAW AMM 71-00-00 TEST 3. AIRCRAFT OK FOR SERVICE
Part: RELAY — UNRELIABLE (ANTI-ICE SYSTEM) · airframe 60,625 hrs · 10,063 cycles
AIRCRAFT WAS GROUNDED: PILOT REPORTS WHILE THROTTLE BOTH CLOSED, DURING DECENT LEFT ENGINE DID NOT GO TO IDLE LIKE RIGHT ENGINE (WHICH WAS NORMAL) POWER WAS CONFIRMED AS HIGH. CYCLED ENGINE ANTI ICE SEEMED TO CLEAR THE ISSUE. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE TAI T/D CONTROL RELAY IAW FIM 30-21-00-815-806. ACCOMPLISHED FLT/GRD IDLE SOLENOID TEST IAW AMM 73-21-04-725-004 AND APPROACH IDLE CHECK IAW AMM 71-00-00 TEST #3 OK FOR SERVICE.
Part: CHARGER — NO TEST (EMERGENCY LIGHT) · airframe 59,952 hrs · 9,913 cycles
R1 DOOR AND OVERWING EXTERIOR LIGHTS WERE INOPERATIVE DURING TEST. REPLACED THE CHARGER MODULE AND BATTERY IAW AMM 33-51-07.
Part: BATTERY — DISCHARGED (CABIN) · airframe 59,952 hrs · 9,913 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND DOOR 1 AND OVERWING EXTERIOR LIGHTS WERE INOPERABLE DURING TEST. REPLACED CHARGER MODULE (SEE AALA20190211002) AND BATTERY WITH SERVICEABLE UNITS PER AMM 33-51-07.
2018
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,336 hrs · 9,758 cycles
MIA - THE AIRCRAFT WAS NOT GROUNDED. L1 DOOR F/A FLASHLIGHT INOP. MAINTENANCE REPLACED BATTERY FOR L1 DOOR F/A FLASHLIGHT IAW AMM 25-64-00, OPS CK OK.
Part: ENGINE — DEFECTIVE · airframe 59,051 hrs · 9,710 cycles
AIRCRAFT WAS GROUNDED. PHL-BUD DIVERTING JFK ACCOUNT COMPRESSOR STALL DUE TO A POSSIBLE BIRD INGESTION. AN EMERGENCY WAS DECLARED AND THEY LANDED OVERWEIGHT. DURING CLIMB THE "LEFT BLEED OVHT" LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURES AT CRUISE LEVELLING OFF COMPRESSOR STALL TO LEFT ENGINE. EGT NORMAL. #1 ENGINE REPLACED PER MCM 71-93-01.
Part: WIRE SPLICE — FAULTY (LT SLATS) · airframe 58,796 hrs · 9,654 cycles
AFTER TAKE OFF, AND DURING CLIMB OUT, EICAS MESSAGE LEADING EDGE SLAT ASSEMTRY MESSAGE ILLUMINATED. EMERGENCY DELCARED AND AC RETURNED TO THE FIELD, FLIGHT LANDED WITHOUT ISSUE. THE AIRCRAFT WAS GROUNDED. DURING TROUBLESHOOTING, FOUND A BAD SPLICE SM7 AND SENSOR S277. REPLACED THE SPLICE SM7 IAW WDM 27-88-12, AND ACCOMPLISHED LEADING EDGE OPS CHECKED IAW MM 27-88-00. ALL OPS NORMAL.
Part: SENSOR — FAULTED (LT WING SLAT) · airframe 58,796 hrs · 9,654 cycles
AFTER TAKE OFF, DURING CLIMB OUT, AN EICAS MESSAGE FOR THE LEADING EDGE SLAT ASSEMTRY MESSAGE ILLUMINATED. EMERGENCY DELCARED AND RETURNED TO THE FIELD, FLIGHT LANDED WITHOUT ISSUE. THE AIRCRAFT WAS GROUNDED. DURING TROUBLESHOOTING, FOUND A BAD WIRE SPLICE SM7, AND SENSOR S277. REPLACED THE SENSOR , AND ACCOMPLISHED LEADING EDGE OPS CHECK IAW MM 27-88-00. ALL OPS NORMAL.
Part: SENSOR — INTERMITTENT (SLAT SYSTEM) · airframe 58,295 hrs · 9,554 cycles
LEADING EDGE SLAT A59M DISPLAYED INTERMITTENTLY AND AT SAME TIME FLAP INDICATOR WENT BETWEEN O AND 1. DECLARED AN EMERGENCY AND DIVERTED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED LE SLAT SENSOR SWITCH IAW AMM 27-88-00. ACCOMPLISHED ALL REQUIRED TEST.
Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 58,182 hrs · 9,529 cycles
THE AIRCRAFT WAS NOT GROUNDED. REMOVED L1 JUMP SEAT EMERGENCY FLASHLIGHT BATTERY PER MM 25-25-03. REPLACED L1 DOOR FLIGHT ATTENDANT JUMP SEAT EMERGENCY FLASH LIGHT PER 25-25-03. OK FOR SERVICE.
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 57,826 hrs · 9,471 cycles
MID FORWARD LEFT FLASHLIGHT WAS FOUND INOPERATIVE. REPLACED THE FLASHLIGHT IAW CMM 25-48-78.
Part: ENGINE — DAMAGED (LEFT) · airframe 57,766 hrs · 9,457 cycles
ENROUTE, A LOUD COMPRESSOR NOISE AND LT ENGINE VIBRATION 5.0 INDICATIONS, DURING CLIMB FROM 360 - 380 LEVEL FLIGHT. EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. THE ACFT WAS GROUNED. MAINTENANCE FOUND THE LEFT ENGINE SPINNER AND ALL FAN BLADES DAMAGED. REPLACED THE FAN BLADES AND SPINNER IAW MM 72-31-02, AND 72-31-01. ACCOMPLISHED ENGINE FAN TRIM BALANCE IAW MM 72-31-00.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,330 hrs · 9,374 cycles
AIRCRAFT WAS NOT GROUNDED. MID GALLEY FLIGHT ATTENDANT LEFT HAND FORWARD ATTENDANT FLASHLIGHT BATTERY DISCHARGED. REPLACED MID GALLEY FLASHLIGHT BATTERY PER AMM 25-60-00.
2017
Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 56,402 hrs · 9,213 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT MARKER AT THE LOWER LEFT FORWARD OVERWING HATCH IS DAMAGED. REMOVED AND REPLACED FLOOR PROXIMITY LIGHTED INDICATOR PER AMM 33-51-01. OPERATIONAL CHECK GOOD.
Part: O-RING — LEAKING (HYDRAULIC SYS) · airframe 55,834 hrs · 9,108 cycles
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. JFK-ZRH FLIGHT DIVERTED TO LHR ACCOUNT CENTER HYDRAULICS QUANTITY LOSS. LANDING UNEVENTFUL. MAINTENANCE FOUND AIR DRIVEN PUMP CASE DRAIN FILTER MODULE DIFFERENTIAL PRESSURE INDICATOR LEAKING. REMOVED AND REPLACED DPI O-RINGS PER AMM 29-11-19. LEAK AND OPERATIONAL CHECK GOOD.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 55,656 hrs · 9,073 cycles
EMERGENCY EXIT LIGHTS BATTERY PACK FAILED THE 10 MINUTE CHECK. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY. OPS CHECKED GOOD.
Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 55,656 hrs · 9,073 cycles
EMERGENCY EXIT LIGHTS BATTERY PACK FAILED THE 10 MINUTE CHECK. REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY. OPS CHECKED GOOD.
Part: LIGHT — BROKEN (CABIN) · airframe 55,525 hrs · 9,049 cycles
EMERGENCY EXIT DIRECTIONAL FLOOD LIGHT AT THE RIGHT FORWARD GALLEY FLOOR IS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-00. OPS CHECKED GOOD.
Part: CABLE — MISINSTALLED (OVERWING SLIDE) · airframe 55,230 hrs · 8,998 cycles
RIGHT OVERWING SLIDE SAFETY CABLE ON TRIGGER, NOT INSTALLED CORRECTLY. SECURED RIGHT OVERWING SLIDE INFLATION BOTTLE CABLE TRIGGER IAW AMM 25-65-02.
Part: BLADE — BROKEN (LT ENGINE) · airframe 54,550 hrs · 8,884 cycles
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE. LEFT ENGINE HAD MULTIPLE COMPRESSOR STALLS AT HIGH POWER DURING FLIGHT. LEFT ENGINE POWER REDUCED TO IDLE. LANDING UNEVENTFUL. FOUND A BROKEN BLADE. R & R THE ENGINE IAW MCM 71-93-01. LEAK CHECKED AND HIGH POWER RUNS IAW 71-00-00. OPS CHECKED GOOD.
Part: COVER — LOOSE (R2 WINDOW) · airframe 54,073 hrs · 8,798 cycles
FIRST OFFICER`S R2 SIDE WINDOW IS DIFFICULT TO OPEN AND CLOSE. REINSTALLED LOOSE AFT WINDOW COVER IAW AMM 56-11-02. OPERATIONAL CHECKED GOOD.
Part: FLASHLIGHT — MISSING (CABIN) · airframe 53,993 hrs · 8,781 cycles
FLIGHT ATTENDANT FLASHLIGHT IN FORWARD GALLEY LEFT JUMPSEAT IS MISSING. REPLACED THE FLASHLIGHT. OPERATIONAL CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,993 hrs · 8,781 cycles
SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 20H, 21H, AND 22H ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY M732 IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.
Part: CYLINDER — UNSERVICEABLE (EVAC SLIDE) · airframe 53,942 hrs · 8,770 cycles
AIRCRAFT WAS NOT GROUNDED. LEFT OVERWING EVACUATION SLIDE INFLATION CYLINDER REQUIRES REPLACEMENT. REMOVED AND REPLACED CYLINDER IAW AMM 25-65-02. OPERATIONAL CHECK GOOD.
Part: FLASHLIGHT — FAILED (CABIN) · airframe 53,599 hrs · 8,711 cycles
AIRCRAFT NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT AFT RIGHT SEAT FAILED TEST. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-60-00. OPERATIONAL CHECK GOOD.
2016
Part: LIGHT — BROKEN (CABIN) · airframe 53,475 hrs · 8,692 cycles
AIRCRAFT NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT COVER PANEL WITH CHORD RIPPED OFF OF 5J ARM REST. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-10. OPERATIONAL CHECK GOOD.
Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 52,495 hrs · 8,539 cycles
ON PS 2 CHECK, FOUND R4 EMERGENCY LIGHT ON DOOR ALL 3 EXIT SIGNS INOPERATIVE. TROUBLESHOOTING FOUND FAULTY BATTERY & CHARGER. REPLACED THE BATTERY & CHARGER IAW MM 33-51-07. ACCOMPLISHED OPSS CHECK OF EMERGENCY LIGHT, CHECKED NORMAL.
Part: PROXIMITY SENSOR — FAULTY (SLATS) · airframe 52,178 hrs · 8,489 cycles
DURING CLIMB THE CREW RECEIVED A LEADING EDGE SLAT ASYMMETRY FAULT INDICATION. EMERGENCY DECLARED. LANDING UNEVENTFUL. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED LEADING EDGE SLAT PROXIMITY SENSOR SWITCH S277 IAW AMM 27-88-01.
Part: ROD — BROKEN (LT MLG BRAKE) · airframe 50,722 hrs · 8,214 cycles
AFTER TAKEOFF, WITH GEAR SELECTED UP, EICAS MSGS, GEAR DOORS, & GEAR DISAGREE, WITH VIBRATION. NORMAL INDICATION WITH GEAR DOWN. NO EMER WAS DECLARED & THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. INSPECTED LT MLG & FOUND NR 2 ANTI-ROTATION BRAKE ROD BROKEN. REPLACED NR 2 & 6 BRAKE RODS WITH ATTACHING PINS. REPLACED NR 2 & 6 BRAKE ASSEMBLIES & WHEEL ASSEMBLIES. ALL OPERATIONAL & SYS TESTED NORMAL. THE ACFT WAS GNDED.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 50,290 hrs · 8,133 cycles
AIRCRAFT WAS NOT GNDED. EMER PATH LIGHTS FROM 35HJ TO 41HJ ARE INOPERATIVE. SECURED SEAT HARNESS CONNECTOR AT SEAT 35HJ. OPERATIONAL CHECKED GOOD IAW AMM 33-51-00.
2015
Part: RELAY — NOT SEATED (ZONE 500) · airframe 49,714 hrs · 8,029 cycles
OVERWING SLIDE SQUIB TEST 1, LT SLIDE FAILS. ACCOMPLISHED TROUBLESHOOTING IAW FIM 25-65-00 FIGURE 103 & MCM CARD 25-92-03. RESEATED TEST RELAYS M1135 K3 & K5, NOW CHECKED OK. SEE ALSO AALA20151110008.
Part: RELAY — NOT SEATED (ZONE 500) · airframe 49,714 hrs · 8,029 cycles
OVERWING SLIDE SQUIB TEST 1, LT SLIDE FAILS. ACCOMPLISHED TROUBLESHOOTING IAW FIM 25-65-00 FIGURE 103 & MCM CARD 25-92-03. RESEATED TEST RELAYS M1135 K3 & K5. NOW CHECKS OK. SEE ALSO AALA20151110001.
Part: SLIDE — UNWANTED DEPLOY (LT OVERWING) · airframe 49,675 hrs · 8,024 cycles
DURING TROUBLESHOOTING, SQUIB TEST PROBLEM. LT WING OVERWING SLIDE DEPLOYED. REPLACED LT WING OVERWING ESCAPE SYS COMPONENTS.
Part: SENSOR — FAULTY (LE SLAT) · airframe 48,619 hrs · 7,847 cycles
AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL, ACFT NOT OVERWEIGHT. DURING CRUISE RECEIVED LE ASYMMETRY MSG & FLAP POSITION NEEDLE INDICATION DISPLAYED ERRATIC. FOUND SLAT 5 INBD LT SENSOR S286 RESISTANCE HIGH. R & R SENSOR S286 IAW AMM 27-88-01. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.
Part: RELAY — FAULTY (ZONE 900) · airframe 48,180 hrs · 7,782 cycles
AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CRUISE, ALL RT HAND LAVATORIES FOUND INOPERATIVE IN FLIGHT. R & R RELAY K2310 IAW AMM 38-32-00. SYS CHECKED NORMAL.
Part: LAVATORY — INOPERATIVE (ZONE 900) · airframe 48,179 hrs · 7,781 cycles
DIVERTED & DECLARED EMER DUE TO ALL BUT 2 LAVATORIES INOPERATIVE AFTER DEPARTURE. PROPERLY SERVICED LAVATORIES UPON ARRIVAL.
Part: WIRE — BROKEN (CABIN) · airframe 48,061 hrs · 7,765 cycles
SEAT 3A EMER AISLE LIGHT WIRE BROKEN. REPLACED LIGHT ASSEMBLY IAW 767 33-51-01 WITH GOOD OPERATIONAL CHECK.
Part: WARNING SYSTEM — FALSE ACTIVATION (LE FLAP) · airframe 47,623 hrs · 7,699 cycles
AIR INTERRUPT, RETURNED, EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. AFTER TAKEOFF DURING FLAP RETRACTION FROM FLAPS 5 DEGREES TO FLAPS 1 DEGREE, RECEIVED LE FLAPS ASSYM EICAS MSG. ACCOMPLISHED FIM TASK 27-81-00, LE ASSYM EICAS MSG, WITH NO FAULTS NOTED. PERFORMED OPERATIONAL CHECK OF SLATS & FLAPS. SYS CHECKED NORMAL ON GND.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,596 hrs · 7,694 cycles
27B EMER LIGHT INOPERATIVE. RELAMPED 27B EMER LIGHT IAW AMM 33-51-02. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,596 hrs · 7,694 cycles
LEFT WING AFT OF WING EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED EXTERIOR EMER LIGHT IAW AMM 33-51-06. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,110 hrs · 7,624 cycles
R4 DOOR EMER EXIT LIGHT INOPERATIVE. R & R EXIT LIGHT LAMP IAW AMM 33-51-06. SYS CHECKED NORMAL.
2014
Part: BATTERY — DISCHARGED (EVAC SLIDE) · airframe 46,593 hrs · 7,549 cycles
OFF WING EMER ESCAPE SLIDE SQUIB FAILED FUNCTION TEST, R & R. REPLACED CHARGER & BATTERY ASSEMBLY M962 IAW AMM 25-65-17. SYS CHECKED NORMAL.
Part: BATTERY — DISCHARGED (EVAC SLIDE) · airframe 46,593 hrs · 7,549 cycles
OFF WING EMER ESCAPE SLIDE SQUIB FAILED FUNCTION TEST, R & R. REPLACED CHARGER & BATTERY ASSEMBLY M961 IAW AMM 25-65-17. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,593 hrs · 7,549 cycles
L4 DOOR EXTERNAL EMER LIGHT IS INOPERATIVE ON TEST. RE LAMPED IAW AMM 33-51-00. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,593 hrs · 7,549 cycles
LEFT FUSELAGE EMER LIGHT AFT OF WING BODY FAIRING IS INOPERATIVE ON TEST. R & R LAMP IAW AMM 33-51-00. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,593 hrs · 7,549 cycles
L1 DOOR EXTERNAL EMER LIGHT INOPERATIVE. RE LAMPED EXTERNAL EMER LIGHT AT L1 DOOR IAW AMM 33-51-00. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,593 hrs · 7,549 cycles
R1 DOOR EXTERNAL EMER LIGHT IS INOPERATIVE. RE LAMPED EXTERNAL EMER LIGHT AT R1 DOOR IAW AMM 33-51-00. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,593 hrs · 7,549 cycles
RIGHT SIDE AFT OF WING, FIRST LIGHT AFT OF FLAPS, EMER LIGHT INOPERATIVE. RE LAMPED IAW AMM 33-51-00. SYS CHECKED NORMAL.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,121 hrs · 7,478 cycles
FLOORBEAM CORRODED AT STATION 347. ACCOMPLISHED SPLICE REPAIR IAW SRM 53-00-51 & EA B767-53-037091.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,121 hrs · 7,478 cycles
NUMBER 8 TRACK CORRODED BETWEEN FUSELAGE STATION 347 & 355. R & R SECTION OF SEAT TRACK.
Part: SKIN — DENTED (FUSELAGE) · airframe 46,121 hrs · 7,478 cycles
DENT AT STATION 1330 BETWEEN STRINGER 32 & 33 LT WITH GOUGE. INSTALLED DOUBLER IAW SRM 53-00-01-2R-29.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,117 hrs · 7,476 cycles
RIGHT SEAT ROWS 5 TO 13 EMER ESCAPE PATH LIGHTING INOPERATIVE. R & R EMER LIGHT BATTERY PACK. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,117 hrs · 7,476 cycles
EMERGENCY LIGHT ON LT EXTERIOR INOPERATIVE. CLEANED CONTACTS FOR LIGHT SOCKET & REPLACED LAMP FOR EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,117 hrs · 7,476 cycles
EMERGENCY LIGHT ON LT EXTERIOR INOPERATIVE. CLEANED CONTACTS FOR LIGHT SOCKET & REPLACED LAMP FOR EXTERIOR EMER FLOOD LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,117 hrs · 7,476 cycles
EMERGENCY LIGHT ON LT EXTERIOR INOPERATIVE. CLEANED CONTACTS FOR LIGHT SOCKET & REPLACED LAMP FOR LT EXTERIOR EMER FLOOD LIGHT. OPERATIONS CHECKED NORMAL.
Part: WIRE — CUT (CABIN) · airframe 46,117 hrs · 7,476 cycles
FOUND CONNECTOR WIRES CUT AT RT CEILING PANEL NR 3. RETERMED W1222-022-20 & W1222-037-20 EMER LIGHT CABLES AT CEILING PANEL AREA RT NR 3 IAW WDM 33-51-12.
Part: LIGHT — BROKEN (EXTERIOR) · airframe 46,117 hrs · 7,476 cycles
RIGHT EXTERIOR SLIDE LIGHT L644 BROKEN. CLEANED SOCKET & REPLACED LAMP FOR RT EXTERIOR SLIDE LIGHT. OPERATIONS CHECKED NORMAL.
Part: LENS — BROKEN (EXTERIOR) · airframe 46,117 hrs · 7,476 cycles
RIGHT EXTERIOR SLIDE LIGHT LENS BROKEN. REPLACED LENS FOR RT EXTERIOR SLIDE LIGHT. OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,868 hrs · 7,436 cycles
RIGHT NR 2 DOOR EMER EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 44,924 hrs · 7,286 cycles
LEFT NR 1 DOOR LOWER AFT EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LT NR 1 DOOR LOWER AFT EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,924 hrs · 7,286 cycles
EMERGENCY LIGHT AT SEAT 12H INOPERATIVE. RESEATED CONNECTOR TO SEAT HARNESS & REPLACED LAMP. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 44,924 hrs · 7,286 cycles
RIGHT NR 1 DOOR LOWER AFT EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR LOWER AFT EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — LOOSE (EXTERIOR) · airframe 44,924 hrs · 7,286 cycles
RIGHT OVERWING SLIDE ESCAPE PATH EMERGENCY LIGHT INOPERATIVE. SECURED LOOSE LAMP ON LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,709 hrs · 7,253 cycles
EMERGENCY EXIT LIGHTS AT RT & LT NR 2 DOORS EXIT SIGNS INOPERATIVE. REPLACED M1210 BATTERY PACK. OPERATIONS CHECKED NORMAL.
2013
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 43,176 hrs · 7,009 cycles
LT NR 4 DOOR INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONS CHECKED NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 43,176 hrs · 7,009 cycles
RT NR 4 DOOR INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONS CHECKED NORMAL.
Part: LIGHT — DEFECTIVE (COCKPIT) · airframe 42,986 hrs · 6,978 cycles
FLIGHT DECK EMERGENCY LIGHT REMAINED ON WITH SWITCH OFF. INSTALLED SERVICEABLE LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,725 hrs · 6,933 cycles
LT & RT NR 2 EMERGENCY DOOR LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY DOOR LIGHTS AT LT & RT NR 2 DOORS. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,188 hrs · 6,539 cycles
LEFT LOWER FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT LOWER FUSELAGE EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,188 hrs · 6,539 cycles
RIGHT LOWER FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT LOWER FUSELAGE EMERGENCY LIGHT. OPS CHECK NORMAL.
2012
Part: INDICATOR — FAILED (COCKPIT) · airframe 39,418 hrs · 6,421 cycles
JFK - INFLIGHT ORD-CDG. CREW REPORTED ISFD ATTITUDE INDICATOR FAILED. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. REPLACED ISFD ATTITUDE INDICATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 37,593 hrs · 6,137 cycles
GRU - CREW REPORTED LEFT ENGINE COMPRESSOR STALLED. EMERGENCY DECLARED FLIGHT RETURNED GRU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND METAL IN TAILPIPE. REPLACED LEFT ENGINE AT GRU ON 06/04/2012. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,067 hrs · 6,058 cycles
LEFT NUMBER 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 2 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 36,051 hrs · 5,883 cycles
RIGHT AFT OVERWING EMERGENCY EXIT SIGN ON LOWER SIDEWALL HAS LAMPS INOPERATIVE. REPLACED LAMPS FOR RIGHT AFT OVERWING EMERGENCY EXIT SIGN. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,051 hrs · 5,883 cycles
NUMBER 6 LEFT SIDE EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR NUMBER 6 LEFT SIDE EXTERNAL EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,051 hrs · 5,883 cycles
NUMBER 7 LEFT SIDE EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR NUMBER 7 LEFT SIDE EXTERIOR EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,707 hrs · 5,827 cycles
RIGHT UNDERWING ESCAPE PATH EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT UNDERWING ESCAPE PATH EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,707 hrs · 5,827 cycles
LEFT AFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT AFT FUSELAGE EMERGENCY LIGHT. OPS CHECK NORMAL.
2011
Part: RELIEF VALVE — OPEN (BLEED AIR SYS) · airframe 33,037 hrs · 5,402 cycles
HNL - CREW REPORTED RIGHT ENGINE PRESSURE RELIEF VALVE STATUS DISPLAYED. EMERGENCY DECLARED FLIGHT RETURNED HNL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PRESSURE RELIEF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: INDICATOR — FAULTY (COCKPIT) · airframe 30,287 hrs · 4,951 cycles
MIA - CREW REPORTED INTEGRATED STANDBY ATTITUDE INDICATOR CIRCUIT BREAKER POPPED. EMERGENCY DECLARED, RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED INTEGRATED STANDBY/AIRSPEED ALTIMETER AND BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,900 hrs · 4,879 cycles
EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN CABIN. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,259 hrs · 4,750 cycles
EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT IN CABIN. OPS CHECK NORMAL.
Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 28,370 hrs · 4,592 cycles
SJU - INFLIGHT STI-JFK. AFTER TAKEOFF CLIMBING THROUGH 12000 EICAS AMBER LEFT ENGINE FUEL FILTER MESSAGE. EMERGENCY DECLARED FLIGHT DIVERTED SJU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH AND FUEL FILTER. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: PRESSURE SWITCH — INOPERATIVE (FUEL SYSTEM) · airframe 28,370 hrs · 4,592 cycles
SJU - INFLIGHT STI-JFK. CREW REPORTED EICAS AMBER LEFT ENGINE FUEL FILTER. ENGINE PERFORMED NORMALLY. EMERGENCY DECLARED DIVERTED SJU LANDED WITHOUT INCIDENT. REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH AND FUEL FILTER. SYSTEM GROUND CHECK NORMAL OPERATION.
2009
Part: SHROUD — MISSING (CABIN) · airframe 27,004 hrs · 4,318 cycles
EMERGENCY LIGHT AT SEAT ROW 11H HAS SHROUD MISSING. REPLACED SHROUD LENS AND LAMPS AT SEAT 11H.
Part: PSEU — FAILED (LE SLAT) · airframe 26,692 hrs · 4,265 cycles
CREW REPORTED EICAS MSG LEADING EDGE ASYMMETRY INDICATION. ABORTED INITIAL LANDING. LANDED AT 157 KNOTS WITH FLAPS 20 USING ALTERNATE TRAILING EDGE FLAPS. LANDED MIA WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRICAL UNIT.
Part: PSEU — FAULTED (TE FLAP) · airframe 26,670 hrs · 4,257 cycles
MIA - CREW REPORTED FLAP ASYMMETRY STATUS MESSAGE. EMERGENCY DECLARED, LANDED AT MIA WITHOUT INCIDENT. BITE CHECK INDICATED PROXIMITY SWITCH ELECTRONIC UNIT SHOWS FAULT. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SENSOR — INOPERATIVE (LE SLAT) · airframe 26,452 hrs · 4,219 cycles
MIA - CREW REPORTED LEADING EDGE SLAT ASYMMETRY FAULT. EMERGENCY DECLARED RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: RELAY — INOPERATIVE (AIR/GROUND SYS) · airframe 25,493 hrs · 4,065 cycles
EZE - CAPTAIN REPORTED PITOT HEATER EICAS MESSAGE ILLUMINATED. RETURNED EZE WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AIR/GROUND RELAY. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
DFW - RIGHT NUMBER 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER 1 DOOR.
Part: CONNECTOR — LOOSE (CABIN)
DFW - CEILING EMERGENCY LIGHT AT SEAT 17B INOPERATIVE. RESECURED LOOSE CONNECTOR FOR CEILING EMERGENCY LIGHT AT SEAT 17B.
2008
Part: SENSOR — FAULTED (ZONE 100) · airframe 23,729 hrs
CREW REPORTED ON TAKEOFF CONFIGURATION INDICATION ILLUMINATED AND MASTER WARNING LIGHT FLASHED ON AND OFF. LEADING EDGE SLAT ASYMMETRY EICAS AND LEADING EDGE LIGHT ILLUMINATED. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. FOUND SLAT SENSOR S301 SLAT INBOARD TRACK FAULTED. REPLACED SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,614 hrs
AFW - RIGHT AFT FUSELAGE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT FUSELAGE EMERGENCY EXIT LIGHT.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 23,614 hrs · 3,764 cycles
FUSELAGE SKIN, SECTION 45 STATION 832-903 STRINGER 6 RIGHT HAS SOME PREVIOUSLY ACCOMPLISHED BLENDS. MATERIAL REMAINING ON SOME LOCATIONS BEYOND SRM LIMITS. HIGH FREQUENCY EDDY CURRENT ACCOMPLISHED, NO CRACKS NOTED. REPAIRED UNDER MRB 767-3343 AND SRM 53-50-01-0I.
Part: SKIN — DAMAGED (RT MLG DOOR) · airframe 23,614 hrs · 3,764 cycles
AFW - RIGHT MAIN LANDING DOOR UNDER SKIN HAS SMALL HOLE. REPAIRED THE HOLE DAMAGE TO THE INNER SKIN USING 250 DEGREE CURE WITH TWO ADDITIONAL PLIES.
Part: WIRE — DISCONNECTED (CABIN) · airframe 23,614 hrs
AFW - EMERGENCY LIGHTING DID NOT STAY ILLUMINATED. RIGHT SIDE EMERGENCY PATH LIGHTING AT ROW 41 DISCONNECTED. RECONNECTED WIRING.
Part: PSEU — FAULTED (LE FLAPS)
LAX INFLIGHT T8/26AUG HNL TO DFW. CREW REPORTED FLAP ASYMMETRY EICAS MSG. ON FINAL APPROACH LIGHT EXTINGUISHED. LANDED LAX WITHOUT INCIDENT. ON TAXI IN LIGHT ILLUMINATED AGAIN. FOUND PROXIMITY SWITCH ELECTRONIC UNIT (PSEU) FAULTING CARDS 007, 010, AND 014 CAUSING FALSE ASYMMETRY INDICATION. REPLACED PSEU. SYSTEM GROUND CHECKED NORMAL OPS.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,583 hrs
DFW EMERGENCY LIGHT AT OVERHEAD SEAT 9E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 9E. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - EMERGENCY LIGHT AT SEAT ROW 20B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LIGHT — INOPERATIVE (CABIN)
DFW EMERGENCY LIGHT AT SEAT 27H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 27H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)
Part: SHROUD — DAMAGED (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT SEAT 38H SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
SFO - EMERGENCY EXIT SIGN LIGHT AT RIGHT AFT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)
SFO - EXTERIOR EMERGENCY LIGHT AT AFT LEFT EXIT DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT AFT LEFT EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHTS)
SFO - EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. RECONNECTED WIRES AT LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: GUARD — BROKEN (COCKPIT)
JFK - EMERGENCY LIGHT SWITCH GUARD IN COCKPIT BROKEN. REPLACED EMERGENCY LIGHT CONTROL PANEL IN COCKPIT OVERHEAD FOR BROKEN EMERGENCY LIGHT SWITCH GUARD IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BULB — INOPERATIVE (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHTS ON RIGHT SIDE OF CABIN INOPERATIVE. RELAMPED EMERGENCY LIGHTS ON RIGHT SIDE OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: SOCKET — CORRODED (EXTERIOR)
DFW - DURING OVERNIGHT MAINTENANCE, RIGHT ADF ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED RIGHT ADF ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SOCKET — CORRODED (EXTERIOR)
DFW - DURING OVERNIGHT MAINTENANCE, LEFT SLIDE GROUND EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED LEFT SLIDE GROUND EXTERNAL EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)