N654A
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERICAN AIRLINES, INC. (AALA) | Operator | on 2014-09-15 | 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.
74 reports on file, 1995-11-08 – 2014-04-29.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 70,455 hrs · 24,360 cycles
EMERGENCY EXIT LIGHT AT SEAT 32 INOPERATIVE. RESEATED ESCAPE PATH LIGHT CONNECTOR AT SEAT 32, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,455 hrs · 24,360 cycles
EMERGENCY EXIT LIGHT L60 AT RT NR 4 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT L60 AT RT NR 4 DOOR, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,455 hrs · 24,360 cycles
EMERGENCY EXIT LIGHT L56 AT LT NR 4 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT L56 AT LT NR 4 DOOR, OPERATIONS CHECKED NORMAL.
Part: BULKHEAD — CRACKED (LT PYLON) · airframe 70,176 hrs · 24,260 cycles
LT PYLON INBD MID BULKHEAD CRACKED. REPAIRED LT PYLON MID BULKHEAD IAW EA B757-54-034038.
Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,173 hrs · 24,259 cycles
RIGHT WW LIFE RAFT TUB SUPPORT BRACKET CORRODED AT BS 1160 & RBL 48. INSTALLED NEW BRACKET IAW SRM 51-40-02.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 70,173 hrs · 24,259 cycles
RIGHT WING NR 10 SLAT UPPER EXTERNAL SURFACE CORRODED. ACCOMPLISHED REPAIR TO NR 10 SLAT SKIN IAW SRM 57-43-01-2R-2 FIGURE 201 & AARD 57-43-00-1.
Part: SKIN — DENTED (FUSELAGE) · airframe 70,173 hrs · 24,259 cycles
LEFT LOWER EXTERIOR FUSELAGE SKIN DENTED AT BS 522 & STRINGERS 28 & 29 LT. INSTALLED REPAIR DOUBLER & FILLER AT ZONE A IAW SRM 53-00-01-2R-2 FIGURE 201 DETAIL 1 SHEET 5.
Part: ANTENNA — CORRODED (VHF COMM) · corrosion level 2 · airframe 70,173 hrs · 24,259 cycles
EXTERNAL FUSELAGE UPPER VHF LT ANTENNA HAS CORROSION AT BODY STATION 740, STRINGERS 1 & 2 LT. R & R UPPER VHF ANTENNA LT SYS IAW AMM 23-12-03-424-007.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,173 hrs · 24,259 cycles
MAIN CABIN AFT GALLEY MOUNT AT STATION 1687 & STRINGER 54 RT IS CORRODED. R & R GALLEY MOUNT IAW SRM 51-40-02.
Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,173 hrs · 24,259 cycles
MAIN CABIN AFT GALLEY MOUNT FITTING AT STATION 1713 & STRINGER 54 RT IS CORRODED. R & R THE GALLEY MOUNT FITTING IAW SRM 51-40-02.
Earlier reports · 1995–2012 · 64 reports
2012
Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 65,862 hrs · 22,744 cycles
SEAT 33E FLOOR EMERGENCY LIGHT INOPERATIVE. FOUND WIRED HARNESS STOWED IN WALL BEHIND AIR GRILL DISCONNECTED. RECONNECTED HARNESS. OPS CHECK NORMAL.
Part: MARKER — DAMAGED (CABIN) · airframe 65,862 hrs · 22,744 cycles
LEFT AFT OVERWING EXIT, EMERGENCY EXIT MARKER LIGHT DECAL IS DAMAGED. REPLACED LEFT AFT OVERWING EXIT EMERGENCY EXIT MARKER LIGHT DECAL.
Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 65,862 hrs · 22,744 cycles
SEAT 3E ESCAPE PATH LIGHT INOPERATIVE. RECONNECTED HARNESS FOR SEAT 3E ESCAPE PATH LIGHT. OPS CHECK NORMAL.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 65,404 hrs · 22,577 cycles
FRAME AT STATION 231.25 RIGHT TO LEFT BUTTLINE 7 DAMAGED. INSTALLED DOUBLER REPAIR PER EA B757-53-025619.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 65,404 hrs · 22,577 cycles
CORROSION ON NUMBER 2 SLAT SEVERAL SPOTS ON UPPER SKIN AT INBOARD DRIVE TRACK. REMOVED DAMAGED AREA OF SKIN AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.
2011
Part: HYDRAULIC LINE — LEAKING (NLG) · airframe 62,811 hrs · 21,628 cycles
MIA - CREW REPORTED UNSAFE LANDING GEAR INDICATION AFTER LOSS OF LEFT HYDRAULICS. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND HYDRAULIC LINE TO NOSE LANDING GEAR LEAKING.
Part: LENS — DAMAGED (CABIN) · airframe 62,008 hrs · 21,338 cycles
RIGHT NUMBER 2 DOOR EMERGENCY EXIT SIGN TOP LENS DAMAGED. REPLACED LENS FOR EMERGENCY EXIT SIGN AT RIGHT NUMBER 2 DOOR. OPS CHECK NORMAL.
Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 61,955 hrs · 21,317 cycles
MIA - CREW REPORTED RIGHT HYDRAULIC QUANTITY SHOWING DECREASE DURING CLIMBOUT. FLIGHT LANDED MIA WITHOUT INCIDENT. INSPECTED AIRCRAFT AND FOUND LOOSE B-NUT AT RIGHT ENGINE HYDRAULIC PYLON MANIFOLD FILTER HOUSING. RE-SECURED FITTING. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,891 hrs · 21,291 cycles
DAMAGED AREA AT STATION 321 BETWEEN STRINGERS 16 AND 17 LEFT OUT OF LIMITS. INSTALLED DOUBLER PER SRM 51-40-03-0G, SRM 53-00-00-00, AARD 51-20-00-1, AARD 51-10-05-1 AND EA B757-53-017146 DATED 5-25-11.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,891 hrs · 21,291 cycles
CORROSION ON DECK FROM STATIONS 1681 TO 1720 TO RIGHT AND LEFT CREASE ANGLE IS OUT OF LIMITS PER SRM. REPLACED DECK PER AARD 51-10-05-1, SRM 53-60-51-01, AND SRM 51-10-02-0G.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,891 hrs · 21,291 cycles
WEB BEHIND RIGHT CREASE ANGLE AT STATIONS 580 TO 600 HAS CORROSION ON INBOARD FLOORBOARD HOLE. REMOVED AND REPLACED WEB PER EA B757-53-016964.
Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 61,891 hrs · 21,291 cycles
LEFT AILERON OUTBOARD HINGE MOUNT RIB CORRODED. REPAIRED PER AARD 51-10-05.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,891 hrs · 21,291 cycles
CORROSION FOUND AROUND TWO FASTENER HOLES ON RIGHT CREASE ANGLE FORWARD OF STATION 620. REPAIRED PER AARD 53-10-13-1.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,891 hrs · 21,291 cycles
LIGHTNING STRIKE AT STATION 1620 STRINGER 28 RIGHT. ACCOMPLISHED DOUBLER REPAIR PER EA 757-53-016939.
Part: DOOR — CRACKED (CARGO BAY) · airframe 61,891 hrs · 21,291 cycles
RIGHT NUMBER 2 DOOR UPPER HINGE CUTOUT IS CRACKED. INSTALLED DOUBLER REPAIR PER EA COMP 52-016172.
Part: INTERCOSTAL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,891 hrs · 21,291 cycles
FORWARD CARGO DOOR, LOWER EDGE INTERCOSTAL NUMBER 4 HAS CORROSION. REPLACED LOWER EDGE INTERCOSTAL NUMBER 4 PER ESO 90114.
Part: INTERCOSTAL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,891 hrs · 21,291 cycles
FORWARD CARGO DOOR, LOWER EDGE INTERCOSTAL NUMBER 3 HAS CORROSION. REPLACED LOWER EDGE INTERCOSTAL NUMBER 3 PER ESO 90114.
Part: BEAM — DENTED (CARGO DOOR) · airframe 61,891 hrs · 21,291 cycles
FORWARD CARGO DOOR, LOWER BEAM IS DENTED AND HAS EPOCAST FILLING IN AREAS. REMOVED DENTED EDGE BEAM AND INSTALLED NEW LOWER EDGE BEAM PER ESO 90114.
Part: SHIELD — BROKEN (CABIN) · airframe 61,575 hrs · 21,179 cycles
SEAT 9D RED EMERGENCY LIGHT SHIELD BROKEN. REPLACED RED EMERGENCY LIGHT SHIELD ON SEAT 9D. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,575 hrs · 21,179 cycles
LEFT NUMBER 1 DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR SLIDE EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,575 hrs · 21,179 cycles
LEFT NUMBER 4 DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR SLIDE EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,575 hrs · 21,179 cycles
BULLNOSE EMERGENCY LIGHT AT SEAT 1B INOPERATIVE. REPLACED LAMP FOR BULLNOSE EMERGENCY LIGHT AT SEAT 1B. OPS CHECK NORMAL.
Part: CONNECTOR — LOOSE (CABIN) · airframe 61,575 hrs · 21,179 cycles
SEAT 26D EMERGENCY LIGHT INOPERATIVE. SECURED LOOSE CONNECTOR AT SIDEWALL FOR EMERGENCY LIGHT ON SEAT 26D. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,575 hrs · 21,179 cycles
BULLNOSE EMERGENCY LIGHT AT SEAT 1E INOPERATIVE. REPLACED LAMP FOR BULLNOSE EMERGENCY LIGHT AT SEAT 1E. OPS CHECK NORMAL.
2010
Part: LENS — MISSING (CABIN) · airframe 61,104 hrs · 21,013 cycles
EMERGENCY FLOOD LIGHT NEAR AFT RIGHT LAVATORY MISSING LENS. REPLACED LENS FOR EMERGENCY FLOOD LIGHT NEAR AFT RIGHT LAVATORY. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,179 hrs · 20,707 cycles
RIGHT AFT OVERWING AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT OVERWING EMERGENCY LIGHT. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,179 hrs · 20,707 cycles
BULL NOSE EMERGENCY LIGHT AT 2EF INOPERATIVE. REPLACED LAMP FOR BULLNOSE EMERGENCY LIGHT AT 2EF. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,179 hrs · 20,707 cycles
LEFT NUMBER 4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL
Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,179 hrs · 20,707 cycles
BULL NOSE EMERGENCY LIGHT AT 1AB INOPERATIVE. REPLACED LAMP FOR BULL NOSE EMERGENCY LIGHT AT 1AB. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,179 hrs · 20,707 cycles
LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT FORWARD OVERWING EMERGENCY LIGHT. OPS CHECKED NORMAL.
2009
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,364 hrs · 20,048 cycles
EMERGENCY LIGHT IN MAIN CABIN INOPERATIVE. REPLACED BATTER PACK.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,364 hrs · 20,048 cycles
EMERGENCY LIGHT IN MAIN CABIN INOPERATIVE. REPLACED BATTERY PACK.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,364 hrs · 20,048 cycles
EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK.
Part: CONNECTOR — LOOSE (CABIN) · airframe 57,826 hrs · 19,855 cycles
AFT EMERGENCY LIGHT AT SEAT ROW 9DEF INOPERATIVE. RESET LOOSE CONNECTOR AT AFT EMERGENCY LIGHT AT SEAT ROW 9DEF.
Part: SKIN — CRACKED (NR 7 SLAT) · airframe 57,754 hrs · 19,830 cycles
NUMBER 7 SLAT HAD CORROSION AT LEADING EDGE SKIN SURFACE APPROXIMATELY 24 INCHES IN FROM OUTBOARD END AT FASTENER. CUT AWAY CORROSION AND CRACK DAMAGE AT APPROXIMATELY 24 INCHES FROM OUTBOARD END AND INSTALLED A FLUSH REPAIR PER SRM 57-43-01-2R.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,754 hrs · 19,830 cycles
NUMBER 8 SLAT SKIN CORRODED 36 INCHES FROM INBOARD END. INSTALLED DOUBLER.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,754 hrs · 19,830 cycles
THE LEFT WING NUMBER 2 SLAT TOP SKIN HAS CORROSION AT THE RIVET 16 INCHES FROM THE SLAT BACK END AND 75.5 INCHES FROM THE OUTBOARD END APPROXIMATELY WING STATION 635. REMOVED DAMAGE SKIN AND INSTALLED DOUBLER PER SRM 57-43-01-2R 2.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,754 hrs · 19,830 cycles
NUMBER EIGHT SLAT SKIN CORRODED APPROXIMATELY 46 INCHES FROM INBOARD END. INSTALLED DOUBLER.
Part: PANEL — DAMAGED (LT WING) · airframe 57,187 hrs · 19,649 cycles
AIRCRAFT TOOK A BIRD STRIKE UPON APPROACH TO THE LEFT WING, INBOARD OF NUMBER ONE ENGINE FILLET PANEL BEHIND NUMBER FOUR SLAT. THE DAMAGE IS APPROXIMATELY FOURTEEN INCHES LONG (OUT OF LIMITS). AIRCRAFT WAS FERRIED TO JFK. HOT BOND REPAIR. INSTALLED NEW HONEYCOMB. REPAIR LAYERS APPLIED AND INSTALLED PLATE, BREATHER CLOTH, AND BAGGING MAT. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 56,341 hrs · 19,336 cycles
STL RIGHT HYDRAULIC QUANTITY WENT TO ZERO AND SUBSEQUENT PRESSURE LOSS IN FLIGHT. EMERGENCY DECLARED LANDED STL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEAK ON THE PRESSURE LINE GOING TO NUMBER 11 SPOILER ACTUATOR. REPLACED HYDRAULIC LINE BETWEEN SPOILERS 11 AND 12 OM RIGHT WING. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)
2008
Part: LENS — MISSING (CABIN) · airframe 53,347 hrs
DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 3B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,347 hrs
DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 25D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)
MIA - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SHUTOFF VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 52,662 hrs
AUA INFLIGHT T1036/05JAN - LOST CABIN PRESSURE AND LIGHT SMOKE IN CABIN. OXYGEN MASKS WERE DEPLOYED. RETURNED TO AUA AND LANDED WITHOUT INCIDENT. SMOKE IN CABIN CLEARED PRIOR TO LANDING. REPLACED RIGHT ENGINE PRESSURE REGULATING SHUT OFF VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: COVER — MISSING (EMERGENCY LIGHTS)
FLL - EMERGENCY EXIT LIGHT AT RIGHT NUMBER TWO DOOR MISSING COVER. REPLACED COVER FOR EMERGENCY EXIT LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: IDG — MALFUNCTIONED (LT ENGINE)
JFK INFLIGHT T1567/01APR - DURING CLIMB, LEFT ENGINE GENERATOR DRIVE LIGHT ILLUMINATED BUT GENERATOR NEVER WENT OFF LINE. APU WAS ON PLACARD. EMERGENCY DECLARED. LANDED JFK OVERWEIGHT WITHOUT INCIDENT. REPLACED INTEGRATED DRIVE GENERATOR FOR LEFT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BATTERY PACK — DISCHARGED (CABIN)
LGA - EMERGENCY ESCAPE PATH LIGHT AT ROWS 16 TO 25 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHT AT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — INOPERATIVE (CABIN)
SFO - EMERGENCY EGRESS LIGHTS AT RIGHT HAND AFT FORWARD TO ROW 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EGRESS LIGHTS AT RIGHT HAND AFT FORWARD TO ROW 26. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REPINNED CONNECTOR AT SEAT 24D FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: FAN — INOPERATIVE (CABIN)
LAS - INFLIGHT T392/26 AIRCRAFT AIR INTERRUPT INTO LAS WITH BURNING SMELL AND LITE HAZE IN CABIN. LANDED WITHOUT INCIDENT. FOUND RIGHT RECIRCULATON FAN CIRCUIT BREAKER POPPED. FOUND BAD BEARINGS IN FAN. REPLACED RIGHT RECIRCULATION FAN. OPERATED BOTH ENGINES AND PACKS WITH NO SMELL FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHTS AT L561 AND L562 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT L561 AND L562. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: PIN — BACKED OUT (CONNECTOR)
MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 24D INOPERATIVE. FOUND PIN PUSHED BACK AT CONNECTOR. RESECURED PIN FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
MIA EMERGENCY LIGHT ON FUSELAGE AT L4 INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHT AT L4. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN)
MIA - EMERGENCY LIGHT AT L4 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT L4. SYSTEM GROUND CHECKED NORMAL OPERATION.
2002
Part: TRANSMITTER — INOPERATIVE (TE FLAPS)
LAX - FLT 397 - EN ROUTE DFW-SNA, RECEIVED EICAS MESSAGE OF LEADING EDGE SLAT DISAGREEMENT. AIRCRAFT LANDED AT LAX WITHOUT INCIDENT. FOUND RIGHT SLAT POSITION TRANSMITTER OUT OF TOLERANCE. MADE ADJUSTMENTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (EXTERIOR)
DFW - LEFT NR 2 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: CONNECTOR — LOOSE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CAIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: SKIN — GOUGED (L1 DOOR CUTOUT)
AFW - FOUND FUSELAGE SKIN AT L-1 DOOR CUTOUT HAD GOUGE BLENDED BEYOND SRM LIMITS, PER MRB 757-933. (M)
Part: SUPPORT — CORRODED (CABIN)
AFW - GALLEY SUPPORTS WITH CORROSION REMOVED, MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR PER MRB 757-892. TST: 15,172 HOURS. CYCLES: 5,361. (X)
Part: DECK PLATE — CORRODED (BS 1680)
AFW - DECK PLATE WITH CORROSION REMOVED. REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIR PER MRB 757-889. TST: 15,172 HOURS. CYCLES: 5,361. (X)
Part: FLOOR BEAM — CORRODED (BS 1640)
AFW - FLOOR BEAM WITH CORROSION REMOVED. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR PER MRB 757-890. TST: 15,172 HOURS. CYCLES: 5,361. (X)
Part: DOOR — DAMAGED (CARGO COMPT)
AFW - DOOR EDGE DAMAGE AFT EDGE AT BOTTOM OF DOOR. REPAIR PER MRB 96C039. TST: 15,172 HOURS. CYCLES: 5,361. (X)
Part: RIB — CORRODED (AILERON)
AFW - AILERON SUPPORT RIB WITH CORROSION REMOVED. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR PER MRB 757-894. TST: 15,172 HOURS. CYCLES: 5,361. (X)
1995
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 35D FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 35D. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)