N320AA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERICAN AIRLINES, INC. (AALA) | Operator | on 2010-04-29 | 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.
173 reports on file, 1995-01-20 – 2013-09-26.
Part: LENS — MISSING (EXIT SIGN) · airframe 105,170 hrs · 20,166 cycles
EMERGENCY EXIT SIGN WITH ARROWS AT RT SIDE FORWARD WALL OF AFT GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: CONNECTOR — BROKEN (CABIN) · airframe 104,870 hrs · 20,106 cycles
EMERGENCY LIGHT AT SEAT 11B INOPERATIVE. REPLACED CONNECTOR AT SEAT 11B & REPINNED. OPERATIONS CHECKED NORMAL.
Part: CONNECTOR — LOOSE (CABIN) · airframe 104,084 hrs · 19,943 cycles
EMERGENCY LIGHTS AT SEAT 9H INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 9H. OPERATIONS CHECKED NORMAL
Part: SWITCH — INOPERATIVE (LE SLAT) · airframe 103,850 hrs · 19,897 cycles
CREW REPORTED EICAS MESSAGE FOR SLAT ASSEMETRY. EMERGENCY DECLARED FLIGHT RETURNED, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED OTBD SLAT NR 5, SWITCH 280. SYS GROUND CHECK NORMAL OPERATION. (CLOSED)
Earlier reports · 1995–2012 · 169 reports
2012
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 102,162 hrs · 19,557 cycles
OVERHEAD EMERGENCY LIGHT AT SEAT 22B INOPERATIVE. REPLACED POWER SUPPLY FOR OVERHEAD EMERGENCY LIGHT AT SEAT 22B. OPS CHECK NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 102,162 hrs · 19,557 cycles
OVERHEAD EMERGENCY EXIT SIGN AT SEAT 20AB INOPERATIVE. REPLACED POWER SUPPLY FOR OVERHEAD EMERGENCY EXIT SIGN AT SEAT 20AB. OPS CHECK NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 102,162 hrs · 19,557 cycles
OVERHEAD EMERGENCY LIGHT AT SEAT 26B INOPERATIVE. REPLACED POWER SUPPLY FOR OVERHEAD EMERGENCY LIGHT AT SEAT 26B. OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 102,162 hrs · 19,557 cycles
EMERGENCY OVERHEAD CENTER AISLE LIGHT AT 28B INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 102,162 hrs · 19,557 cycles
OVERHEAD EMERGENCY LIGHT AT SEAT 17B INOPERATIVE. REPLACED POWER SUPPLY FOR OVERHEAD EMERGENCY LIGHT AT SEAT 17B. OPS CHECK NORMAL.
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
CORROSION ON SKIN UNDERNEATH RIGHT FAILSAFE STRAP JUST AFT OF STRINGER 20 RIGHT END PIECE. REPLACED FAILSAFE STRAP PER EA B767-53-024878 AND SB 767-53-0116.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER CLIP FOR STRINGER 39 RIGHT AT STATION 742 CORRODED. REPLACED STRINGER CLIP PER SRM 51-40-02.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 101,177 hrs · 19,361 cycles
WEB SKIN ON BODY FRAME STATION 742 AT AFT LOWER SIDE HAS 3 AREAS OF CORROSION BETWEEN STRINGERS 33 TO 36 LEFT. INSTALLED NEW STRINGER CLIPS PER SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1197 BETWEEN STRINGERS 38 AND 39 RIGHT. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SKIN — CRACKED (LT WING) · airframe 101,177 hrs · 19,361 cycles
LOW FREQUENCY EDDY CURRENT INSPECTION OF LEFT WING FRONT SPAR LOWER CHORD AND SKIN SHOWS A CRACK INDICATION AT RIB NUMBER 17 OUTBOARD 2 FASTENERS AT APPROXIMATELY FRONT SPAR STATION 628.36. INSTALLED AND CAP SEALED TWO FASTENERS PER EA B767-57-024018.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 742 BETWEEN STRINGERS 34R AND 35R CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER 37 LEFT JUST AFT OF STATION 434 HAS SURFACE CORROSION AROUND FASTENER AT INBOARD SIDE. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-03-2R.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER 33 LEFT BETWEEN STATIONS 434 TO 456 HAS AREA OF CORROSION AT OUTBOARD SIDE. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-03-2R.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 566 BETWEEN STRINGERS 39 TO 38 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 566 BETWEEN STRINGERS 37 TO 38 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 566 BETWEEN STRINGERS 37 TO 36 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 566 BETWEEN STRINGERS 39 TO 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 742 BETWEEN STRINGERS 39 LEFT AND 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 566 BETWEEN STRINGERS 39 LEFT TO 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 566 BETWEEN STRINGERS 37 TO 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: STRUCTURE — CORRODED (SERVICE DOOR) · airframe 101,177 hrs · 19,361 cycles
CORROSION ON INNER AFT RIGHT LOWER SERVICE ENTRY DOOR CHORD. REMOVE AND REPLACE CHORD.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
RIGHT BUTTLINE 10 LONGITUDINAL FLOORBEAM BETWEEN STATIONS 955 AND 977 IS CORRODED. REMOVE AND REPLACE A SECTION OF THE LONGITUDINAL FLOORBEAM BETWEEN STATIONS 955 TO 977 PER SRM 53-00-51-2R.
Part: STRUCTURE — CORRODED (DOOR) · airframe 101,177 hrs · 19,361 cycles
THE LEFT LOWER AFT DOOR CHORD IS CORRODED. REMOVED AND REPLACED CHORD.
Part: SILL — CORRODED (FUSELAGE) · airframe 101,177 hrs · 19,361 cycles
CORROSION ON LEFT SERVICE ENTRY DOOR SILL PLATE. REMOVED AND REPLACED SILL PLATE.
Part: SKIN — CRACKED (RT WING) · airframe 101,177 hrs · 19,361 cycles
CRACK INDICATION AT TWO EACH FASTENER HOLES IN LOWER WING SKIN AT FRONT SPAR LOWER CHORD. FASTENER REMOVED AND HOLES REAMED TO .2621. CHECKED FOR CRACK INDICATION AFTER REAMING, AND NO CRACK INDICATIONS WERE FOUND. RE-INSTALLED FASTENERS.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
RIGHT OUTBOARD SEAT TRACK FROM 1208 TO 1427 IS CORRODED. REPLACED SEAT TRACK PER SRM 51-10-02-0G.
Part: CHANNEL — CRACKED (FUSELAGE) · airframe 101,177 hrs · 19,361 cycles
FLOORBOARD FASTENER HOLE CRACKED. REMOVED AND REPLACED HAT CHANNEL.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1373 BETWEEN STRINGERS 37 AND 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1373 BETWEEN STRINGERS 36 AND 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 101,177 hrs · 19,361 cycles
INTERCOSTAL ANGLE AT CEILING AREA IN AFT CARGO BETWEEN STATIONS 1241 TO 1263 AT LEFT BUTTLINE 40 HAS 2 CRACKS. REMOVED AND REPLACED INTERCOSTAL ANGLE PER AARD 51-00-05-1.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 101,177 hrs · 19,361 cycles
ANGLE AT CEILING AREA IN AFT CARGO BETWEEN STATIONS 1087 TO 1109 AT LEFT BUTTLINE 40 HAS 1 CRACK. REPLACED CHORD PER AARD 51-00-05-1.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 101,177 hrs · 19,361 cycles
ANGLE AT CEILING AREA IN FORWARD CARGO BETWEEN STATIONS 566 TO 588 AT LEFT BUTTLINE 40 HAS 1 CRACK. REPLACED CHORD PER AARD 51-00-05-1.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 101,177 hrs · 19,361 cycles
ANGLE CRACKED JUST AFT OF STATION 347 AT APPROXIMATELY LEFT BUTTLINE 30. REPLACED CHANNEL PER AARD 51-00-05-1.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 101,177 hrs · 19,361 cycles
ANGLE AT CEILING AREA IN AFT CARGO BETWEEN STATIONS 1087 TO 1109 AT RIGHT BUTTLINE 40 CRACKED. REPLACED INTERCOSTAL ANGLE PER AARD 51-00-05-1.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 610 BETWEEN STRINGERS 37 AND 38 LEFT HAS CORROSION. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 654 BETWEEN STRINGERS 35 AND 36 LEFT HAS CORROSION. REPLACED SHEAR TIE PER SRM 53-30-01.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 610 BETWEEN STRINGERS 39 AND 38 LEFT HAS CORROSION. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 698 BETWEEN STRINGERS 39 LEFT AND 39 RIGHT HAS CORROSION. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 654 BETWEEN STRINGERS 39 LEFT AND 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 654 BETWEEN STRINGERS 37 AND 36 LEFT HAS CORROSION. REPLACED SHEAR TIE PER SRM 53-30-00.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 632 BETWEEN STRINGERS 37 AND 38 LEFT. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
CORROSION ON INNER SKIN UNDER STRINGER 36 RIGHT FROM STATIONS 414 TO 430. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01-2R.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER SPLICE FOR STRINGER 39 LEFT, AT STATION 434 HAS CORROSION ON INBOARD SIDE. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-01-2R.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER CLIP FOR STRINGER 39 LEFT AT STATION 1395 CORRODED. INSTALLED NEW STRINGER TIE PER SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 676 BETWEEN STRINGERS 39 AND 38 LEFT CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM 53-00-07.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER 35 LEFT, JUST FORWARD OF STATION 434, AT OUTBOARD SIDE HAS AREA OF CORROSION. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-01-2R.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 720 BETWEEN STRINGERS 36 AND 37 LEFT CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 676 BETWEEN STRINGERS 39 LEFT AND 39 RIGHT CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM 53-00-07.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER 34 RIGHT BETWEEN STATIONS 412 TO 434 HAS AREA OF CORROSION. INSTALLED DOUBLER REPAIR PER SRM 53-00-03-2R.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 676 BETWEEN STRINGER 37 AND 36 RIGHT CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM 53-00-07.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER SPLICE FOR STRINGER 39 RIGHT, JUST FORWARD OF STATION 434 HAS CORROSION ON OUTBOARD SIDE. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-01-2R.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR-TIE AT STATION 676 BETWEEN STRINGERS 37 AND 38 LEFT HAS CORROSION. REMOVED AND REPLACED SHEAR TIE PER SRM 53-00-07.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
CARGO FLOOR INNER J-FRAME CORRODED. INSTALLED STRAP.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 720 BETWEEN STRINGERS 38 AND 39 LEFT CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM 53-00-07.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER 30 RIGHT BETWEEN STATIONS 434 TO 456 HAS AREA OF CORROSION. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-01-2R.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER 38 RIGHT, JUST AFT OF STATION 412, HAS AREA OF CORROSION. INSTALLED DOUBLER REPAIR PER SRM 53-00-01-2R.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER 36 RIGHT BETWEEN STATIONS 412 TO 434 HAS AREA OF CORROSION. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-01-2R.
Part: SKIN — CRACKED (LT PYLON) · airframe 101,177 hrs · 19,361 cycles
LEFT PYLON UPPER TORQUE BOX SKIN CRACKED WHERE INTEGRATED DRIVE GENERATOR FEEDER CABLES PASS THRU. INSTALLED DOUBLER REPAIR PER AARD 54-52-01-1.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER 36 LEFT, JUST AFT OF STATION 434 HAS SURFACE CORROSION AROUND FASTENER AT OUTBOARD SIDE. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-01-2R.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER 35 LEFT, JUST FORWARD OF STATION 434, AT OUTBOARD SIDE HAS AREA OF CORROSION. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-01-2R.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STATION 1087 J-CAP CORRODED. REPLACED INNER J-FRAME PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1351 BETWEEN STRINGERS 33 AND 34 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1153 AT STRINGERS 39 LEFT AND 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1351 BETWEEN STRINGERS 38 AND 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1175 BETWEEN STRINGERS 38 AND 37 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1175 BETWEEN STRINGERS 36 AND 37 LEFT. REPLACED SHEAR TIE PER SRM 51-10-2.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1197 AT STRINGERS 38 AND 37 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1351 BETWEEN STRINGERS 36 AND 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1197 BETWEEN STRINGERS 37 AND 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1307 BETWEEN STRINGERS 35 TO 36 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1263 BETWEEN STRINGERS 36 AND 35 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1175 BETWEEN STRINGERS 38 AND 37 LEFT. REPLACED SHEAR TIE PER SRM 51-10-2.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1351 BETWEEN STRINGERS 36 AND 35 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER SPLICE FOR 37 LEFT AFT OF STATION 1307 HAS SHIM STOCK THAT IS CORRODED UNDER BOTH INBOARD AND OUTBOARD FLANGE. INSTALLED STRINGER REPAIR WET PER EA B767-53-024116.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1175 AT STRINGERS 39 LEFT AND 39 RIGHT. REPLACED SHEAR TIE PER SRM 51-10-2.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1329 BETWEEN STRINGERS 38 AND 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1329 BETWEEN STRINGERS 36 AND 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1219 BETWEEN STRINGERS 38 AND 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEARTIE AT STATION 1197 BETWEEN STRINGERS 36 AND 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1263 BETWEEN STRINGERS 36 AND 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1285 BETWEEN STRINGERS 39 RIGHT TO 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1219 BETWEEN STRINGERS 38 AND 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1307 BETWEEN STRINGERS 34 TO 35 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1219 BETWEEN STRINGERS 35 AND 36 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1307 BETWEEN STRINGERS 33 TO 34 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1219 BETWEEN STRINGERS 36 AND 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1307 BETWEEN STRINGERS 39 LEFT TO 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1263 BETWEEN STRINGERS 37 AND 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1263 AT STRINGERS 39 RIGHT AND 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1263 BETWEEN STRINGERS 38 AND 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1285 BETWEEN STRINGERS 38 TO 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1197 BETWEEN STRINGERS 38 AND 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STATION 1153 CARGO FLOOR INNER J FRAME CORRODED. REPLACED INNER J CHORD PER SRM 51-10-02.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STRINGER SPLICE FOR 39 RIGHT BETWEEN STATIONS 1285 TO 1307 ON INBOARD SIDE HAS SHIM STOCK THAT IS CORRODED UNDER FLANGE. INSTALLED NEW SHIM WET PER SRM 53-00-03-1A.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1087 BETWEEN STRINGERS 37 AND 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1307 BETWEEN STRINGERS 38 TO 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1395 BETWEEN STRINGERS 38 AND 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1329 BETWEEN STRINGERS 38 AND 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1285 BETWEEN STRINGERS 38 TO 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1329 AT STRINGERS 39 LEFT AND 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1219 BETWEEN STRINGERS 37 AND 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1285 BETWEEN STRINGERS 36 TO 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1175 BETWEEN STRINGERS 38 AND 39 LEFT. REPLACED SHEAR TIE PER SRM 51-10-2.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1329 BETWEEN STRINGERS 36 AND 35 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1197 AT STRINGERS 39 LEFT AND 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1307 BETWEEN STRINGERS 37 TO 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1285 BETWEEN STRINGERS 38 TO 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1219 AT STRINGERS 39 LEFT AND RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1351 BETWEEN STRINGERS 38 AND 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1351 BETWEEN STRINGERS 34 AND 35 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 522 BETWEEN STRINGERS 39 LEFT AND 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
STATION 1087 J CAP CORRODED. REPLACED INNER J FRAME PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1540 BETWEEN STRINGERS 37 TO 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1540 BETWEEN STRINGERS 38 TO 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 53-00-07.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 522 BETWEEN STRINGERS 39 AND 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 522 BETWEEN STRINGERS 37 AND 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
J-CAP AT STATION 1131 CORRODED. REPLACED J-CAP PER SRM 51-10-02.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 101,177 hrs · 19,361 cycles
STATION 1087 STRINGER 37 RIGHT CLIP CORRODED. REPLACED STRINGER CLIP PER SRM 51-10-02.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 101,177 hrs · 19,361 cycles
STATION 1087 STRINGER 39 RIGHT CLIP CORRODED. REPLACED STRINGER CLIP PER SRM 51-10-02.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 101,177 hrs · 19,361 cycles
STATION 1087 STRINGER 39 LEFT CLIP CORRODED. REPLACED STRINGER CLIP PER SRM 51-10-02.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
CORROSION ON INTERNAL FUSELAGE SKIN AT FORWARD LAVATORY VENT NOZZLE. PERFORMED BLEND OUTSKIN REPAIR PER EA B767-53-024283.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1241 BETWEEN STRINGERS 38 TO 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1241 BETWEEN STRINGERS 38 TO 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1241 BETWEEN STRINGERS 39 LEFT TO 39 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1241 BETWEEN STRINGERS 38 TO 37 RIGHT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1241 BETWEEN STRINGERS 38 TO 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1241 BETWEEN STRINGERS 34 TO 35 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 101,177 hrs · 19,361 cycles
SHEAR TIE AT STATION 1241 BETWEEN STRINGERS 36 TO 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
Part: TARGET — BROKEN (LE SLAT) · airframe 100,665 hrs · 19,259 cycles
LAX - CREW REPORTED LEADING EDGE SLAT ASYMMETRY ECIAS AND LEADING EDGE LIGHT WITH FLAPS SELECTED AT 20 AND INDICATING 20 DURING APPROACH. EMERGENCY DECLARED FLIGHT LANDED LAX WITHOUT INCIDENT. PROXIMITY SENSOR TARGET BROKEN AT SLAT NUMBER 8 INBOARD TRACK. REPLACED SENSOR TARGET. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — BROKEN (CABIN) · airframe 100,128 hrs · 19,149 cycles
SEAT MOUNTED EMERGENCY AISLE PATH LIGHT AT 28B BROKEN. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY AISLE PATH LIGHT AT 28B. OPS CHECK NORMAL.
2011
Part: WIRE — DEFECTIVE (CABIN) · airframe 99,177 hrs · 18,958 cycles
SEAT MOUNTED EMERGENCY LIGHT AT 22H INOPERATIVE. REPINNED WIRES FOR 22H SEAT MOUNTED EMERGENCY LIGHT.
Part: WIRE — DEFECTIVE (CABIN) · airframe 99,177 hrs · 18,958 cycles
SEAT MOUNTED EMERGENCY LIGHT AT 29H INOPERATIVE. RE-PINNED WIRES FOR SEAT MOUNTED EMERGENCY LIGHTS AT 29H. OPS CHECK NORMAL.
Part: FSEU — INOPERATIVE (LE SLAT) · airframe 98,314 hrs · 18,782 cycles
JFK - CREW REPORTED LEADING EDGE ASYMMETRY DURING APPROACH. EMERGENCY DECLARED FLIGHT LANDED JFK WITHOUT INCIDENT. REPLACED FLAP SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: PITOT HEAD — FAULTY (LEFT) · airframe 93,058 hrs · 17,704 cycles
LAX - CREW REPORTED ALTIMETERS DISAGREED BY TWO HUNDRED FEET ON CLIMBOUT. RETURNED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT UPPER PITOT PROBE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2009
Part: BATTERY PACK — WEAK (CABIN) · airframe 92,612 hrs · 17,612 cycles
EMERGENCY LIGHTS ON RIGHT SIDE OF COACH DIM. REPLACED BATTERY PACK M9030.
Part: LIGHT — WEAK (CABIN) · airframe 92,612 hrs · 17,612 cycles
PORTABLE EMERGENCY LIGHT IN COCKPIT DIM. REPLACED PORTABLE LIGHT ASSEMBLY.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 90,545 hrs
JFK - LEFT NUMBER 4 DOOR FUSELAGE EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CONTACT AND REPLACED LAMP FOR LEFT NUMBER 4 DOOR FUSELAGE EXTERIOR EMERGENCY EXIT LIGHT.
2008
Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · 83,305 cycles
JFK SEAT MOUNTED EMERGENCY LIGHT AT SEAT 33H INOPERATIVE. REPAIRED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 33H. SYSTEM GROUND CHECKED NORMAL OPS.
Part: CONTROLLER — FAILED (WINDOW HEAT) · 87,980 cycles
JFK INFLIGHT T4/31AUG. CAPTAINS WINDSHIELD INNER WINDOW PANE CRACKED FOLLOWED BY ELECTRICAL ARCING IN LOWER LT CORNER. CREW INITIATED EMERGENCY DEPRESSURIZATION PROCEDURES. PRESSURIZATION NEVER GOT ABOVE FL100. LANDED JFK WITHOUT INCIDENT. REPLACED WINDOW HEAT CONTROL UNIT, WINDOW HEAT CONNECTOR AND LT NR 1 WINDOW. SYSTEM GROUND CHECKED NORMAL OPS.
2007
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
LAX - EMERGENCY LIGHTS AT RIGHT FORWARD DOOR AND OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK M731 FOR EMERGENCY LIGHTS AT RIGHT FORWARD DOOR AND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)
LAX - EMERGENCY LIGHTS IN FORWARD RIGHT AISLE INOPERATIVE. REPLACED BATTERY PACK CONNECTOR D2746 FOR EMERGENCY LIGHTS IN FORWARD RIGHT AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
AFW - EMERGENCY ESCAPE PATH LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT 25HJ FOR EMERGENCY ESCAPE PATH LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: PSEU — DEFECTIVE (COCKPIT)
JFK T003/27DEC03 EN ROUTE JFK-LAX AFTER TAKEOFF, LANDING GEAR MONITOR MESSAGE WITH AURAL WARNING. UNABLE TO SILENCE. AIRCRAFT RETURNED JFK LANDING WITHOUT INCIDENT. REPLACED GROUND PROXIMITY ELECTRONIC UNIT. SYSTEM GROUND CHECKED OPERATION NORMAL.
Part: GENERATOR — FAILED (RT ENGINE)
DRIVE LIGHT CAME ON WITH ASSOCIATED EICAS MESSAGE DISCONNECTED AS PER CHECK LIST. EICAS MESSAGE DISTINGUISHED BITE MAINTENANCE PANEL FOR FAULTS. VISUALLY INSPECTED GEN NO FAULTS NOTED ON THE GROUND. RAN ENGINE FOUND IDG TO BE LEAKING. DEFERRED RIGHT IDG INOPERATIVE PER MEL ACCOMPLISHED MPM 24-1 ENT IN MIC SHEET. REMOVED AND REPLACED NR 2 ENGINE IDG. LEAK AND OPS CHECK GOOD. REMOVED PLACARD CLEARED MIC SHEET. (M)
2002
Part: FAIRING — DEPARTED (LT PYLON)
SFO - FLT 1994 - EN ROUTE SFO-DFW - ON TAKEOFF, LEFT PYLON DOGHOUSE FAIRING DEPARTED THE AIRCRAFT. RETURNED TO SFO WITHOUT INCIDENT. INSPECTED AIRCRAFT AND LEFT PYLON FOR OTHER DAMAGES. NO OTHER DAMAGED NOTED, PER SRM 54-5170-01 INTERIM REPAIR WAS PERFORMED. REINSPECT AT EACH B-CHECK FOR PROGRESSION AND PERFORM PERMANENT REPAIR AT NEXT MBV. GROUND CHECKED OPERATION NORMAL. (M)
2001
Part: GCU — FAILED (E/E BAY)
AFTER TAKEOFF, RIGHT GEN OFF PLUS RIGHT GEN DRIVE LIGHT ON STEADY. GEN DISCONNECTED BY CREW. PLACARD RIGHT GEN INOPERATIVE PER MEL ENTERED IN MIC SHEET VERIFIED BOTH IDG'S AND APU OIL FULL IAW MEL 24-1 IDG REMAINS DISCONNECTED. BITE CHECK OF BPCU SHOWS NO FAULT UP TO 10 FLIGHT LOGS, ON RIGHT GCU. MEG CHECK SHOWED NO SHORTS. SHOOK HAR 5272 WIRING. NO OPENS NOTED. REPLACED RIGHT ENGINE GCU. RAN ENGINE. LOADED RIGHT GENERATOR, NO FAULTS. RIGHT GENERATOR OPS CHECK NORMAL. REMOVED DEV 9-221DC-A MEL REP 24-1. CLEARED MIC SHEET. REPLACED IDG HARNESS HAR 5272 RAN RIGHT ENGINE SYSTEM CHECKS NORMAL. (M)
Part: OVEN — DIRTY (F/C GALLEY)
GLA - FLT 52 - EN ROUTE ORD-GLA, DETECTED SMOKE AT FIRST CLASS NR 2 GALLEY OVEN. PULLED CIRCUIT BREAKER. LANDED GLA WITHOUT FURTHER INCIDENT. REMOVED DEBRIS AT NR 2 OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — INOPERATIVE (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 37B INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 39B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 37B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: WARNING LIGHT — ILLUMINATED (TAILCONE)
DFW - FLT 320 - EN ROUTE DFW-BDL - DURING TAKEOFF ROLL, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ABORTED TAKEOFF AT 140 KNOTS. RAN BOTH ENGINES 80 PERCENT WITH BOTH PACKS. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1999
Part: PROCESSOR UNIT — DEFECTIVE (E/E COMPT)
DFW - FLT 947 - AFTER TAKEOFF DFW, LIM RIGHT FUEL QTY INDICATOR INDICATED 2000 TO 2500 LBS GREATER THAN LEFT FUEL QTY INDICATOR. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED FUEL QTY PROCESSOR UNIT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: CSEU — DEFECTIVE (E/E COMPT)
MIA - FLT 973 - EN ROUTE MIA-GIG, AT CRUISE, APPROXIMATELY 2 HOURS INTO FLIGHT, THE EICAS MESSAGE 'SPOILERS' AND 'R YAW DAMPER' ILLUMINATED. AT THE SAME TIME THE EICAS MESSAGE 'AILERON LOCKOUT' WAS FLICKERING AND THEN BECAME A STEADY MESSAGE, MOMENTS LATER THE RUDDER RATION EICAS MESSAGE ILLUMINATED. CIRCUIT BREAKERS WERE NORMAL, AS WELL AS, HYDRAULICS AND ELECTRONICS. RETURNED AND LANDED MIA W/O INCIDENT. REPLACED BOTH RIGHT CSEU UNITS AS A PRECAUTION. LAND 40 TEST PASSES WITH NO FAULTS. NO FAULTS ON GROUND TEST. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: CONNECTOR PIN — LOOSE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING AT SEAT 26B INOPERATIVE. RESECURED PUSHED BACK PIN AT SEAT HARNESS FOR EMERGENCY EXIT LIGHTING AT SEAT 26B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: CONNECTOR — DISCONNECTED (CABIN)
ORD - FLT 42 - DURING FLIGHT, EMERGENCY EXIT LIGHT AT PAX SEAT 26B INOPERATIVE. RECONNECTED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SKIN — CORRODED (BS 956)
AFW - FOUND CORROSION ON CENTER WING UPPER SKIN AT AFT DRAIN LOCATION. REMOVED CORROSION, BLENDED AREA, PRIMED, PAINTED AND SEALED PER ENGINEERING MRB 767-1593. (M)
Part: SKIN — LIGHTNING STRIKE (BS 440)
AFW - FOUND AND BLENDED OUT AN ARE OF LIGHTNING STRIKE DAMAGE ON THE EXTERNAL FUSELAGE SKIN. THE BLENDOUT EXCEEDS SRM LIMITS. NDT CHECKED BLENDED AREA. NO CRACKS INDICATED. REFINISHED PER SRM. APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-1589. (M)
Part: SILL — CORRODED (BS 542)
AFW - FOUND AND BLENDED CORROSION ON THE OUER CHORD OF THE FWD CARGO DOOR LOWER SILL. THE BLENDOUT IS ON THE UPPER SURFACE OF THE OUTBOARD LOWER FLANGE OF THE CHORD. THE BLEND OUT EXCEEDS SRM LIMITS. REFINISHED THE BLENDOUT PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB767-1587. (M)
Part: WIRE — CHAFED (CABIN)
SFO - DURING MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROWS 20H THROUGH 30H WOULD NOT ILLUMINATE. REPAIRED EMERGENCY EXIT LIGHT CHAFED WIRE AT SEAT ROW 28H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1996
Part: FAN — DEFECTIVE (FWD EQUIP BAY)
LHR - FLT 0066 - EN ROUTE ORD/LHR DURING CRUISE, ELECTRICAL ODOR NOTED IN COCKPIT FOLLOWED BY EICAS MESSAGE FOR FORWARD EQUIPMENT COOLING SUPPLY FAN. COOLING SUPPLY FAN CIRCUIT BREAKER POPPED AND ODOR DISAPPEARED. AIRCRAFT PROCEEDED LHR AND LANDED WITHOUT INCIDENT. REPLACED NR 1 FORWARD EQUIPMENT COOLING FAN. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ELECTRICAL ODOR NOTED. (M)
1995
Part: FRAME — CRACKED (BS 1219)
AFW - FOUND WEB OF FRAME AT STATION 1219 BL 0 CRACKED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER FROM 0.032 7075-T6 ALUMINUM AND INSTALLED WET WITH BMS5-95 SEALANT, ALODINED, PRIMED AND PAINTED PER ENGINEERING MRB 767-972. (M)
Part: CORNER — CORRODED (CARGO DOOR)
AFW - FOUND CORROSION AROUND A NUT PLATE HOLE IN THE INNER FLANGE OF THE LOWER FORWARD CORNER PIECE OF THE BULK CARGO DOOR. FOUND BEYOND SRM LIMITS AFTER BLENDING. TREATED, PRIMED AND PAINTED AREA. REINSTALLED NUT PLATE, APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-974. (M)
Part: SKIN — WORN (LT PYLON)
AFW - FOUND A GROOVE WORN IN THE LEFT PYLON INBOARD AND OUTBOARD SIDE SKINS. BOTH GROOVES WERE CAUSED BY AN ANGLE ON THE THRUST REVERSER RUBBING ON THE SIDE SKINS. BLENDED AND REFINISHED GROOVES. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-975. (M)
Part: FLOOR BEAM — CORRODED (BS 266)
AFW - FOUND FLOOR BEAM CORROSION, REMOVAL BEYOND SRM LIMITS. ALODINE BLENDED AREA. FILL BLEND OUT WITH BMS-592. FABRICATE A REPAIR STRAP FROM .050 301 HALF HARD STAINLESS AND INSTALL WET PER ENGINEERING MRB 767-970.
Part: EEL WIRE — BROKEN (CABIN)
SFO - DURNG OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 7G INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z)
Part: EEL WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE BETWEEN R1 AND R3 DOORS INOPERATIVE. REPAIRED BROKEN WIRE IN FIRST CLASS SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z)
Part: SENSOR — DEFECTIVE (LT MLG)
MIA-DFW - FLT 457 - AFTER TAKEOFF, GEAR FAILED TO RETRACT. ON FOURTH ATTEMPT, GEAR RETRACTED AND LOCKED. LANDED DFW WITHOUT INCIDENT. REPLACED LT TILT SENSOR AND ADJUSTED BOTH LT MLG SENSORS. ACCOMPLISHED GEAR SWING, SYSTEM GROUND CHECKS NORMAL OPERATION. (W)
Part: EEL WIRE — SHORTED (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LOWER FORWARD AND AFT OPENING OF L2 DOOR FOUND INOPERATIVE. REPLACED SHORTED WIRES FOR LOWER FORWARD AND AFT L2 DOOR EMERGENCY EXIT LIGHTS LOCATED IN CONDUIT L9008. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)
Part: EEL CONNECTOR — DEFECTIVE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LT AISLE FROM PASSENGER SEAT 23B AFT FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)