N172AJ
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
119 reports on file, 2002-05-11 – 2020-04-04.
Part: SHIM — MIGRATED (LT PYLON) · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT WING FRONT SPAR PYLON UPPER INBOARD LINK DRAG FITTING SHIM "C" MIGRATING OUTBOARD. REMOVED DRAG LINK FITTING REPLACED SHIM AND RE-INSTALLED DRAG FITTING PER EA 303618.
Part: GOVERNOR — DEFECTIVE (RT ENGINE) · airframe 57,415 hrs · 16,352 cycles
AIRCRAFT IN BASE MAINTENANCE - EMERGENCY DECLARED - DURING FUNCTIONAL CHECK FLIGHT, #2 ENGINE INFLIGHT SHUTDOWN AND RELIGHT TEST, FAILED TO RESTART. NO FUEL FLOW OBSERVED, ALL OTHER ENGINE INDICATIONS NORMAL. NO ENGINE VALVE LIGHT OBSERVED WHEN FUEL CONTROL SWITCH MOVED TO RUN. REMOVED AND REPLACED RIGHT ENGINE FUEL FLOW GOVERNOR PER AMM 73-94-01, OPERATIONAL CHECK GOOD. [SEE ASSOCIATED REPORT AALA2020029005]
Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT WAS NOT GROUNDED: SEAT 33 D, E, F EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE RELAMPED EPL ON SEAT 33 D, E, F PER AMM 33-51-11.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT WAS NOT GROUNDED: SEAT 19 D, E, F EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE RELAMPED EPL ON SEAT 19 D, E, F PER AMM 33-51-11.
Part: SKIN — WORN (TE FLAP) · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE INBOARD FLAP LOWER SURFACE LEADING EDGE SKIN WORN 9 INCHES INBOARD OF AFT FLAP BELL CRACK BRACKET. REPAIRED FLAP SRM 57-53-01-2R.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR RIGHT HAND AFT GALLEY MOUNT AT BS 1718 AND RBL 40. REPLACED MOUNT PER SRM 51-10-02.
Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 1310 AND BS 1380 AT S24R. REPLACED TRANSITION PANEL PER SRM 51-10-02.
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON APU INLET BOX LANDING STRAP AT BS 1787 AND S3R. REPLACED STRAP PER SRM 51-10-02.
Part: MOUNT — CORRODED (FUSELAGE) · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN LAVATORY "K" AFT INBOARD MOUNT AT BS 1640 AND LBL 30. REPLACED MOUNT PER SRM 51-40-02.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN DECK HAT CHANNEL BETWEEN BS 1680 AND BS 1720 AT BL 0. REPLACED CHANNEL PER AARD 51-00-05-1.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN CREASE ANGLE BETWEEN BS 780 AND BS 800 AT S17R. REPAIRED CREASE ANGLE PER AARD 53-30-13-1.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN "Z" ANGLE AT BS 1715 AND RBL 50. REPLACED "Z" ANGLE PER AARD 51-00-05-1.
Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN DECK PLATE AT BS 1715 AND LBL 23. REPAIRED DECK PLATE PER SRM 53-60-51-2R.
Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN DECK PLATE AT BS 1715 AND RBL 48. REPAIRED DECK PLATE PER SRM 53-60-51-2R.
Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN DECK PLATE AT BS 1715 AND RBL 36. REPAIRED DECK PLATE PER SRM 53-60-51-2R.
Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN DECK PLATE AT BS 1715 AND RBL 5. REPAIRED DECK PLATE PER SRM 53-60-51-2R.
Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN DECK PLATE AT BS 1715 AND RBL 12. REPAIRED DECK PLATE PER SRM 53-60-51-2R.
Part: WEDGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING INBOARD FLAP TRAILING EDGE WEDGE UPPER SURFACE BETWEEN 11 INCHES AND 12 INCHES OUT BOARD OF THE AFT FLAP CUT OUT OUTBOARD EDGE. REPAIRED FLAP WEDGE PER EA 303430.
Part: WEDGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 57,412 hrs · 16,350 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING INBOARD FLAP TRAILING EDGE WEDGE UPPER SURFACE BETWEEN 4 INCHES AND 7 INCHES OUT BOARD OF THE AFT FLAP CUT OUT OUTBOARD EDGE. REPAIRED FLAP WEDGE PER EA 303430.
Earlier reports · 2002–2019 · 100 reports
2019
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,155 hrs · 16,267 cycles
AIRCRAFT WAS NOT GROUNDED: L4 EXTERIOR SLIDE LIGHT INOPERABLE. MAINTENANCE RELAMPED SLIDE LIGHT PER MM 33-51-06.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 57,008 hrs · 16,215 cycles
AIRCRAFT WAS NOT GROUNDED: SEAT 34DEF EMERGENCY LIGHT IN SEAT WAS INOPERABLE. MAINTENANCE RECONNNECTED CONNECTOR UNDER SEAT 34DEF PER AMM 33-51-11 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,700 hrs · 16,115 cycles
AIRCRAFT WAS NOT GROUNDED: L4 EXTERIOR SLIDE LIGHT INOPERABLE. MAINTENANCE RELAMPED SLIDE LIGHT PER AMM 33-51-06.
Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 56,700 hrs · 16,115 cycles
AIRCRAFT IN BASE VISIT: SEAT MOUNTED EMERGENCY LIGHTS 26D-36D ARE VERY DIM. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-07.
Part: TRANSMITTER — UNRELIABLE (TE FLAP) · airframe 56,220 hrs · 15,970 cycles
AIRCRAFT WAS GROUNDED: PILOT REPORTS WHEN FLAPS 25 SELECTED, TRAILING EDGE FLAP SPLIT LEFT FLAP INDICATED 25, RIGHT FLAP INDICATED 20. EMERGENCY DECLARED. MAINTENANCE REPLACED RT TE FLAP TRANSMITTER IAW 27-58-03. OPS CHECKS NORMAL.
Part: LIGHT — INOPERATIVE (SEAT 2E) · airframe 56,038 hrs · 15,913 cycles
AIRCRAFT WAS NOT GROUNDED: SEAT 2E EMERGENCY LIGHT AFT INOPERABLE, MISSING LENS AND BULBS. MAINTENANCE REPLACED LIGHT PER AMM 33-51-05.
Part: UNKNOWN — MALFUNCTIONED (RT ENGINE) · airframe 55,938 hrs · 15,885 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS RIGHT ENGINE CONTINUES TO RUN AFTER FUEL CONTROL SWITCH MOVES TO CUTOFF, HAD TO RECYCLE SWITCH. MAINTENANCE ACCOMPLISHED 3 SUCCESSFUL ENGINE START AND SHUTDOWN CYCLES IAW AMM 71-00-00. UNABLE TO DUPLICATE MALFUNCTION.
Part: GOVERNOR — UNRELIABLE (ENGINE) · airframe 55,938 hrs · 15,885 cycles
AIRCRAFT WAS GROUNDED: PILOT HAD TO PULL FIRE SWITCH TO SHUT ENGINE DOWN. AFTER PULLING FIRE HANDLE ENG. VALVE LIGHT STAYED ON. MAINTENANCE REMOVED AND REPLACED FUEL FLOW GOVERNOR IAW JOB CARD 73-94-01. OPS CHECK GOOD.
Part: GOVERNOR — UNRELIABLE (NR 2 ENGINE) · airframe 55,828 hrs · 15,853 cycles
AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS NR 2 ENG RUNS AFTER FUEL CTL. SWITCH OFF FOR 30 SEC. MAINTENANCEREMOVED AND REPLACED #2 ENGINE FUEL FLOW GOVERNOR IAW CARD 19L40073001, OPS AND LEAK CHECK GOOD. RT ENGING SHUT DOWN ON COMMAND.
Part: CONNECTOR — DIRTY (RT ENGINE) · airframe 55,740 hrs · 15,833 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS RIGHT ENGINE FAILED TO SHUTDOWN NORMALLY. AFTER SELECTING CUTOFF SLOW TO STOP RUNNING 30 TO 45 SECONDS. MAINTENANCE PERFORMED TROUBLESHOOTING IAW FIM 73-21-00-815-807-R00. CHECKED 28V AT D41050P PIN 3, FOUND GOOD. CLEANED AND REINSTALLED CONNECTOR. PERFORMED ENGINE RUN IAW AMM 71-00-00. ENGINE SHUTDOWN IMMEDIATELY AFTER FUEL CONTROL SWITCH MOVED TO CUTOFF.
Part: COMPUTER — FAILED (AUTOPILOT) · airframe 55,576 hrs · 15,790 cycles
AIRCRAFT WAS GROUNDED: PILOT REPORTS CENTER AUTOPILOT KICKED OFF 2 HOURS AT CRUISE. RESET 50 MINUTES LATER AND CLEARED NO LAND 3 ANNUNCIATOR. CENTER AUTOPILOT RESET OK. IN DESCENT CENTER AUTOPILOT UNCOMMANDED TURN TO RIGHT AND DISENGAGED. NO LAND 3 ILLUMINATED. USED LEFT AUTPILOT NO PROBLEM. MAINTENANCE ACCOMPLISHED FIM 22-02-00-810-801. CTR FCC FAILED. REMOVED & REPLACED CTR FCC IAW AMM 22-11-01. PERFORMED GROUND TEST LAND 40 IAW AMM 22-00-02. ALL OPS CHECK OK.
Part: LIGHT — SMOKE (CABIN) · airframe 55,576 hrs · 15,790 cycles
AIRCRAFT WAS GROUNDED: READING LAMP AT 25E SMOKES WHEN TURNED ON AND SMELLS OF BURNING PLASTIC. LENS COVER ALSO MISSING. MAINTENANCE ACCOMPLISHED MCM CARD 05-96-70 AND REPLACED LIGHT ASSEMBLY AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-23-00.
Part: LIGHT — SMOKE (ZONE 200 - FUSE) · airframe 55,576 hrs · 15,790 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS READING LAMP AT 25E SMOKES WHEN TURNED ON. SMELLS OF BURNING PLASTIC AND LENS COVER MISSING. MAINTENANCE REMOVED AND REPLACED LIGHT ASSY AT 25E. PERFORMED OPS CHECK ALL CHECKS OK , NO FAULTS NOTED IAW AMM 33-23-00.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 54,982 hrs · 15,628 cycles
PILOT REPORTS THE RIGHT FLAP FAILED BETWEEN 20 AND 25 LEFT FLAP CONTINUED TO 30. WHILE ACCOMPLISHING QRH PROCEDURE, RIGHT FLAP RESUMED TRAVEL TO 30. CONTROL INPUTS CONFIRMED FLAP INDICATION WAS CORRECT. FLAPS RETRACTED NORMAL. MAINTENANCE PERFORMED BITE ON BOTH FSEUS, NO FAULTS FOUND. ALSO RAN FLAPS TO 30. NO FAULTS FOUND, BITE FSAM, NO FAULTS FOUND. A/C OK FOR SERVICE ALL WORK ACCOMPLISHED IAW AMM 27-51-00-715-001, REVIEWED HISTORY, NO FAULTS FOUND.
Part: AUTOPILOT SYS — MALFUNCTIONED (LEFT) · airframe 54,937 hrs · 15,614 cycles
HAD AN UNCOMMANDED AUTOPILOT DISCONNECT, LT AUTOPILOT, 4 HOURS INTO FLIGHT. TURNED BACK ON DURING THE DESCENT AND WORKED REMAINDER OF FLIGHT. MAINTENANCE ACCOMPLISHED MCDP GROUND TEST 01 , L FCC IAW FIM 22-03-00-805-827, NO FAULTS FOUND . PERFORMED MCDP GROUND TEST 40, AUTOLAND IAW FIM 22-03-00-990-843. NO FAULTS NOTED ALL NORMAL .
2018
Part: FSEU — FAULTY (TE FLAPS) · airframe 54,021 hrs · 15,330 cycles
DURING APPROACH, WHILE SELECTING FLAPS 15 TO FLAPS 20, ONE OF THE FLAP INDICATORS STAYED AT 15 FOR ABOUT 3 MINUTES AND THEN SNAPPED TO 20, NO ASSYMETRY FELT IN FLIGHT CONTROLS. DECLARED AN EMERGENCY AND DID A GO-AROUND. FLAP INDICATOR WORKED NORMALLY WHEN FINAL FLAPS 25 WAS SELECTED. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED FSEU-1 M10331 OPS CHECKED NORMAL, IAW FIM 27-51-00-815-812 TASK 22, AND AMM 27-51-01, OK FOR SERVICE.
Part: FLOOR SUPPORT — CRACKED (BS 480-500) · airframe 53,920 hrs · 15,298 cycles
CRACKED FLOOR SUPPORT TOP FLANGE ANGLE BETWEEN BS 480 AND 500, RBL 10. REPLACED THE FLOOR SUPPORT ANGLE IAW 51-00-05.
Part: DOOR — OUT OF ADJUST (L1) · airframe 52,883 hrs · 15,046 cycles
L1 DOOR STRIKING FUSELAGE DOOR FRAME DURING OPENING AND BENDING OUTER DOOR SKIN AT UPPER LEFT CORNER APPROXIMATELY 30 DEGREES UP ON FORWARD EDGE. AIRCRAFT WAS GROUNDED. REPAIRED PER B757 SRM 52-10-01-2R-7 REPAIR 7.
Part: SUPPORT BRACKET — OUT OF ADJUST (L1 DOOR) · airframe 52,879 hrs · 15,045 cycles
AIRCRAFT WAS GROUNDED. UNABLE TO CLOSE L1 DOOR. ADJUSTED L1 DOOR GUIDE ARM SUPPORT BRACKET. PRESSURIZED AIRCRAFT. DOOR OPERATIONS AND LEAK CHECK GOOD.
Part: CAM FOLLOWER — DEFECTIVE (L1 DOOR) · airframe 52,752 hrs · 15,014 cycles
DURING DEPARTURE, THE L1 DOOR EXTREMELY DIFFICULT TO CLOSE. 22 FLIGHT ATTENDANTS AND PILOT COULDNT CLOSE IT. REMOVED AND REPLACED THE UPPER AND LOWER CAM FOLLOWERS IAW MM 52-11-02. REMOVED AND REPLACED L1 DOOR AFT UPPER AND LOWER LATCH FITTINGS IAW MM 52-11-37. DOOR OPS CHECKED OK. THE AIRCRAFT WAS GROUNDED.
Part: WINDOW SHADE — JAMMED (CABIN) · airframe 52,490 hrs · 14,948 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT 15F WINDOW SHADE STUCK IN OPEN POSITION. UNJAMMED WINDOW SHADE AS REQUIRED PER AMM 25-21-12 OPERATIONS CHECK GOOD.
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 51,894 hrs · 14,780 cycles
EXIT SIGN LENS OVER L2 DOOR CAME OFF. MAINTENANCE REPLACED THE SIGN LENS IAW AMM 33-50-00, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: BEARING — DEFECTIVE (L1 DOOR) · airframe 51,610 hrs · 14,707 cycles
AIRCRAFT WAS NOT GROUNDED. 1L DOOR REQUIRES EXCESSIVE FORCE TO CLOSE. REPLACED 1L DOOR LOWER FORWARD BEARING PER 52-10-01. OKAY FOR SERVICE.
2017
Part: FLASHLIGHT — INOPERATIVE (MID CABIN) · airframe 51,353 hrs · 14,637 cycles
AIRCRAFT NOT GROUNDED. MID FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED MID FLIGHT ATTENDANT FLASHLIGHT PER AMM 25-64-00. OPERATIONS CHECK GOOD.
Part: HYDRAULIC LINE — LOOSE (ZONE 500) · airframe 50,625 hrs · 14,419 cycles
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. MIA-UVF FLIGHT RETURNED TO MIA ACCOUNT RIGHT HYDRAULIC QUANTITY INDICATION. OVERWEIGHT LANDING UNEVENTFUL. MAINTENANCE DETERMINED HYDRAULIC LEAK AT SPOILER NR 2. TIGHTENED LINE AT SPOILER NR 2 POWER CONTROL UNIT PER AMM 20-11-00. SERVICED HYDRAULIC SYSTEM PER AMM 12-12-01. LEAK AND OPERATIONAL CHECK GOOD.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 50,263 hrs · 14,326 cycles
EMERGENCY LIGHT AT SEAT 34D IS INOPERATIVE. RESEATED CONNECTOR AT THE WALL. OPS CHECKED GOOD IAW AMM 33-51-00.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 50,263 hrs · 14,326 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS IN THE FIRST CLASS ARE DIM. REMOVED AND REPLACED BATTERY PACK AND CHARGING MODULE (AALA201708149010) AT M10798 PER AMM 33-51-07. OPERATIONAL CHECK GOOD.
Part: MODULE — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 50,263 hrs · 14,326 cycles
SEAT MOUNTED EMERGENCY LIGHTS IN THE FIRST CLASS ARE DIM. REMOVED AND REPLACED BATTERY PACK AND CHARGING MODULE AT M10798 IAW AMM 33-51-07. OPS CHECKED GOOD.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 50,263 hrs · 14,326 cycles
EMERGENCY LIGHT AT SEAT 23D IS INOPERATIVE. RESEATED CONNECTOR AT THE WALL. OPS CHECKED GOOD IAW AMM 33-51-11.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 50,263 hrs · 14,326 cycles
EMERGENCY LIGHT AT SEAT 10D IS INOPERATIVE. RESEATED THE CONNECTOR. OPS CHECKED GOOD IAW AMM 33-51-11.
Part: TRACK — DIRTY (L4 DOOR) · airframe 50,199 hrs · 14,306 cycles
AIRCRAFT WAS GROUNDED. IT TOOK OVER 4 ATTEMPTS TO DISARM 4L DOOR. CLEANED AND LUBRICATED SLIDE TRACKS PER AMM 25-66-01 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: FITTING — OUT OF POSITION (ZONE 800) · airframe 50,191 hrs · 14,303 cycles
AIRCRAFT WAS NOT GROUNDED. L4 DOOR SLIDE PACK FLAP HAS A CLIP STICKING OUT. REPOSITIONED FLAP BACK IN PLACE ON DOOR 4L IAW AMM 52-11-00. SYSTEM CHECKS NORMAL
Part: LANYARD — LOOSE (L4 DOOR) · airframe 50,071 hrs · 14,273 cycles
AIRCRAFT WAS NOT GROUNDED. L4 DOOR EMERGENCY EVACUATION SLIDE COVER LANYARD IS LOOSE. RESECURED LANYARD PER AMM 52-11-02. OPERATIONAL CHECK GOOD.
Part: GIRT BAR — UNSECURE (L2 DOOR) · airframe 50,046 hrs · 14,267 cycles
L2 DOOR ESCAPE SLIDE GIRT BAR ANGLE IS EXPOSED. SECURED THE ANGLE IAW AMM 25-66-01. OPERATIONAL CHECKED GOOD.
Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHT) · airframe 49,933 hrs · 14,237 cycles
SEAT MOUNTED EMERGENCY LIGHT AT SEAT 10D IS INOPERATIVE. RESEATED THE CONNECTOR IAW AMM 33-51-11. OPS CHECKED GOOD.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,557 hrs · 14,138 cycles
FORWARD EMERGENCY EXIT SIGN AFT OF COCKPIT DOOR AND R1 DOOR IS INOPERATIVE. REMOVED AND REPLACED CHARGER ASSEMBLY AND EMERGENCY BATTERY IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LGIHTS) · airframe 49,563 hrs · 14,139 cycles
FORWARD EMERGENCY EXIT SIGN AFT OF COCKPIT DOOR AND R1 DOOR IS INOPERATIVE. REMOVED AND REPLACED CHARGER ASSEMBLY AND EMERGENCY BATTERY IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.
Part: DECK PLATE — CORRODED (BS 1716) · airframe 49,484 hrs · 14,116 cycles
CORROSION ON AFT DECK PLATE 146N5318-3, BS 1716, LBL 51. REPAIRED IAW SRM 53-60-51-2R-14, AND EA 269964.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,274 hrs · 14,072 cycles
AIRCRAFT WAS NOT GROUNDED. EXTERIOR EMERGENCY EXIT LIGHT BY L4 DOOR IS INOPERATIVE. REMOVED AND REPLACED LIGHT IAW AMM 33-51-11. OPERATIONAL CHECK GOOD.
Part: LIGHT — BROKEN (CABIN) · airframe 48,651 hrs · 13,898 cycles
AIRCRAFT NOT GROUNDED. EMERGENCY EXIT LIGHT AT L1 DOOR IS BROKEN. REPLACED LIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 48,614 hrs · 13,890 cycles
SEAT MOUNTED EMERGENCY LIGHT AT SEAT 2E IS INOPERATIVE. SECURED THE CONNECTOR ON THE LIGHT ASSEMBLY IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.
2016
Part: FILTER — DIRTY (ZONE 200) · airframe 48,196 hrs · 13,773 cycles
AIRCRAFT GROUNDED. FOUL ODOR DETECTED FROM DIRTY RECIRCULATION AIR FILTER. REPLACED LEFT FILTER IAW AMM 21-25-02. OPERATIONAL CHECK GOOD.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,022 hrs · 13,729 cycles
AIRCRAFT NOT GROUNDED. R2 DOOR EXTERIOR GROUND ILLUMINATION EMERGENCY SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-06 AND SWPM 20-30-00. OPERATIONAL CHECK GOOD.
Part: LIGHT — BROKEN (CABIN) · airframe 45,814 hrs · 13,140 cycles
L1 DOOR EMER EXIT LIGHT ASSEMBLY BROKEN. REPLACED L1 DOOR EMER LIGHT ASSEMBLY IAW MM 33-51-10. ALL CHECKED NORMAL. THE ACFT WAS GNDED.
Part: CONTROL PANEL — FAULTY (WEATHER RADAR) · airframe 45,556 hrs · 13,075 cycles
WEATHER RADAR FAILED SHORTLY AFTER TAKEOFF. DUE TO DESTINATION WEATHER, FLIGHT DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. FOUND DUST BUILD UP ON T/R UNIT RACK CONNECTOR PINS. CLEANED CONNECTOR, R & R WEATHER RADAR CONTROL PANEL IAW MM 34-43-02. INSPECTED RADAR ANTENNA ASSEMBLY & ACCOMPLISHED WIRING CHECKS. THE ACFT WAS GNDED.
Part: CONNECTOR — DIRTY (WEATHER RADAR) · airframe 45,556 hrs · 13,075 cycles
WEATHER RADAR FAILED SHORTLY AFTER TAKEOFF. DUE TO DESTINATION WEATHER, FLIGHT DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. FOUND DUST BUILD UP ON T/R UNIT RACK CONNECTOR PINS. CLEANED CONNECTOR, R & R T/R WEATHER UNIT IAW MM 34-43-01. INSPECTED RADAR ANTENNA ASSEMBLY & ACCOMPLISHED WIRING CHECKS. THE ACFT WAS GNDED.
2015
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 45,049 hrs · 12,957 cycles
EMERGENCY AISLE PROXIMITY LIGHTS INOPERATIVE, FROM SEATS 10 - 16. R & R EQUIP 10952 POWER SUPPLY & BATTERY IAW AMM 33-51-07. EMER AISLE LIGHTS, BETWEEN SEATS 10 - 16, OPERATIONALLY CHECKED OK. THE ACFT WAS NOT GNDED.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 45,049 hrs · 12,957 cycles
EMERGENCY LIGHTS INOPERATIVE, BETWEEN SEATS 26 - 36 & WEAK BETWEEN SEATS 16 - 26. R & R POWER SUPPLY & BATTERY EQUIPMENT M10953. EMERGENCY AISLE PROXIMITY LIGHTS, BETWEEN SEATS 16 - 36 OPERATIONALLY CHECKED OK IAW AMM 33-51-07. THE ACFT WAS NOT GNDED.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,215 hrs · 12,307 cycles
R2 DOOR EMER LIGHT INOPERATIVE. REPLACED EMER LIGHT BATTERY PACK M10952 IAW AMM 33-51-07. SYS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,215 hrs · 12,307 cycles
EMERGENCY LIGHTS FROM ROWS 9 - 15 & ROWS 19 - 23 VERY DIM. REPLACED EMER LIGHT BATTERY PACKS M10952 & M10953 IAW AMM 33-51-07. SYS CHECKED NORMAL.
2014
Part: FRAME — DENTED (FUSELAGE) · airframe 40,020 hrs · 11,798 cycles
AFT CARGO COMPARTMENT, FUSELAGE FRAME IS DENTED AT STATION 1360 & STRINGER 26 RT. ACCOMPLISHED REPAIR FOR FRAME IAW EA B757-53-034980 & REO-G17458 REV B.
Part: SKIN — DAMAGED (CARGO DOOR) · airframe 40,020 hrs · 11,798 cycles
FORWARD CARGO DOOR HAS SEVERAL BLEND OUTS OF LIGHTNING STRIKES THAT EXCEED SRM LIMITS. ACCOMPLISHED REPAIRED FWD CARGO DOOR SKIN AT STATIONS 577, 590 & STATIONS 612 TO 618.
Part: FRAME — DENTED (FUSELAGE) · airframe 40,020 hrs · 11,798 cycles
AFT CARGO COMPARTMENT, FUSELAGE FRAME IS DENTED AT STATION 1420 & STRINGER 26 LT. REPAIRED FUSELAGE FRAME AT STATION 1420 & STRINGER 26 LT IAW SRM 53-00-07-2R-5, FIGURE 201, DETAIL I.
Part: THRUST REVERSER — CORRODED (NR 1 ENGINE) · corrosion level 2 · airframe 40,020 hrs · 11,798 cycles
NUMBER 1 ENG OTBD THRUST REVERSER INNER UPPER AFT AREA HAS CORROSION. INSTALLED NEW SERVICEABLE NR 1 OTBD THRUST REVERSER IAW CARD 78-94-01.
Part: FRAME — DENTED (FUSELAGE) · airframe 40,020 hrs · 11,798 cycles
AFT CARGO COMPARTMENT, FUSELAGE FRAME IS DENTED AT STATION 1380 & STRINGER 26 LT. ACCOMPLISHED NESTED ANGLE REPAIR IAW 53-00-07-2R-5 FIGURE 201, DETAIL I.
Part: SKIN — DENTED (FUSELAGE) · airframe 40,020 hrs · 11,798 cycles
FUSELAGE SKIN DENTED AT STATION 1687 BETWEEN STRINGERS 23 & 24 RT. INSTALLED REPAIR DOUBLER IAW SRM 53-00-01-2R-3 FIG 201 SHEETS 1 OF 8 & IAW SRM 51-40-02.
Part: TRANSITION PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 40,020 hrs · 11,798 cycles
AFT CARGO RT HAND TRANSITION PANEL HAS CORROSION FROM FRAME STATIONS 1530 TO 1640. R & R TRANSITION PANEL IAW SRM 51-40-02.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,020 hrs · 11,798 cycles
FORWARD CABIN FLOOR AREA, STATION 361 & RBL 64, FLOOR ATTACH STRUCTURE HAS CORROSION AROUND NUT PLATES. REMOVED CORROSION & REPLACED ANGLE IAW AARD 51-00-05-1.
Part: SKIN — DAMAGED (CARGO DOOR) · airframe 40,020 hrs · 11,798 cycles
FORWARD CARGO DOOR HAS SEVERAL BLEND OUTS OF LIGHTNING STRIKES THAT EXCEED SRM LIMITS. REPAIRED FWD CARGO DOOR SKIN AT STATIONS 517, 590 & 612 TO 618 IAW SRM 52-30-01-2R-4.
Part: SUPPORT BRACKET — CRACKED (ZONE 700) · airframe 40,020 hrs · 11,798 cycles
RIGHT MAIN WW LG SELECTOR VLV SUPPORT BRACKET IS CRACKED. REMOVED DAMAGE & INSTALLED DOUBLER IAW SRM 51-70-11-0G.
Part: STRAP — CRACKED (FUSELAGE) · airframe 40,020 hrs · 11,798 cycles
CABIN FLOOR STABILIZATION STRAP IS CRACKED AT BS 1380 & RBL 45.5. REPAIRED STABILIZATION STRAP IAW EA B757-53-034558.
2013
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,861 hrs · 11,539 cycles
EMERGENCY LIGHTS LOCATED ON OVERHEAD BINS FWD & AFT OF MID LAVATORY ON LT SIDE INOPERATIVE. REPLACED BATTERY PACK & POWER SUPPLY. OPERATIONS CHECKED NORMAL.
Part: RELAY — FAILED (TE FLAP) · airframe 35,820 hrs · 10,844 cycles
BOS - CREW REPORTED WHEN SELECTING FLAPS 25 TRAILING EDGE FLAP DIAGREE MESSAGE APPEARED. EMERGENCY DECLARED FLIGHT LANDED BOS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LOAD RELIEF RELAY K10245 BAD. REPLACED RELAY K10245. SYSTEM GROUND CHECK NORMAL OPERATION.
2012
Part: STOP FITTING — OUT OF ADJUST (L4 DOOR) · airframe 35,147 hrs · 10,703 cycles
JFK - CREW REPORTED LEFT NUMBER 4 DOOR HANDLE MOVED IN FLIGHT AND DOOR INDICATION EICAS MESSAGE INDICATION. FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND SEVERAL DOOR STOPS OUT OF ADJUSTMENT. RE-ADJUSTED DOOR STOPS. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,134 hrs · 10,697 cycles
LIGHTNING STRIKE DAMAGE TO STATION 1442. INSTALLED DOUBLER PER EA B757-53-027479.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,134 hrs · 10,697 cycles
LIGHTNING STRIKES AT STATION 660 STRINGER 21 RIGHT. INSTALLED DOUBLER AT STATION 660 PER EA B757-53-027481.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,134 hrs · 10,697 cycles
LIGHTNING STRIKE TO STATION 1458 BETWEEN STRINGERS 2 AND 3 RIGHT. INSTALLED DOUBLER PER EA B757-53-027450.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 34,845 hrs · 10,636 cycles
EMERGENCY LIGHT AT SEAT 30D INOPERATIVE. SECURED EMERGENCY LIGHT PLUG AT SEAT 30D. OPS CHECK NORMAL.
Part: PUMP — FAILED (LT ENGINE) · airframe 34,070 hrs · 10,457 cycles
DUB - INFLIGHT LHR-BOS. CREW REPORTED LEFT ENGINE DRIVEN PUMP HIGH TEMPERATURE INDICATION. EMERGENCY DECLARED FLIGHT DIVERTED DUB LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE DRIVEN PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,718 hrs · 10,157 cycles
FOUND ALL SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK M10798. OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,718 hrs · 10,157 cycles
FOUND ALL SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK M10953. OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,718 hrs · 10,157 cycles
FOUND ALL SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK M10952. OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,718 hrs · 10,157 cycles
FOUND ALL SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK M10801. OPS CHECK NORMAL.
Part: IDG — INOPERATIVE (RT ENGINE) · airframe 32,695 hrs · 10,153 cycles
JFK - CREW REPORTED RIGHT GENERATOR TRIPPED DURING CRUISE. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE GENERATOR INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,858 hrs · 9,972 cycles
THE 3AB BULLNOSE MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR ESCAPE PATHLIGHT AT 3AB. OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,818 hrs · 9,956 cycles
EMERGENCY LIGHTS FROM ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY LIGHTS FROM ROWS 9 TO 15. OPS CHECK NORMAL.
Part: SIGN — BROKEN (CABIN) · airframe 31,636 hrs · 9,917 cycles
LEFT NUMBER 4 DOOR EMERGENCY EXIT SIGN BROKEN. REPLACED EMERGENCY EXIT SIGN AT LEFT NUMBER 4 DOOR. OPS CHECK NORMAL.
2010
Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 27,849 hrs · 9,149 cycles
EMERGENCY LIGHT AT SEAT 3E IS INOPERATIVE. RECONNECTED AND REROUTED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES HARNESS. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,471 hrs · 9,070 cycles
EMERGENCY LIGHT ABOVE SEATS 25DEF INOPERATIVE. REPLACED LAMP FOR BULLNOSE EMERGENCY LIGHT AT SEATS 25DEF. OPS CHECKED NORMAL.
Part: STOP PIN — OUT OF ADJUST (L4 DOOR) · airframe 27,100 hrs · 9,002 cycles
JFK - CREW REPORTED LEFT NUMBER 4 DOOR OPEN WARNING INDICATION DURING CLIMB OUT. EMERGENCY DECLARED RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ADJUSTED DOOR STOP PINS AND LOWER AND UPPER GATES. PRESSURIZED AIRCRAFT AND CHECK OF DOOR HANDLE SHOWED NO MOVEMENT. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,723 hrs · 8,712 cycles
FROM 26D SEAT TO AFT DOORS EMERGENCY LIGHT TOO DIM. REPLACED BATTERY PACK FOR 26D TO AFT DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.
2009
Part: MODULE — INOPERATIVE (CABIN) · airframe 22,446 hrs
SJU - EMERGENCY EXIT LIGHTS FROM SEAT ROWS 9D TO 16D INOPERATIVE. REPLACED MODULE FOR EMERGENCY EXIT LIGHTS FOR SEAT ROWS 9D TO 16D.
Part: MODULE — INOPERATIVE (CABIN) · airframe 22,446 hrs
SJU EMERGENCY EXIT LIGHTS FROM SEATS 9D TO 16D INOPERATIVE. REPLACED MODULE 5537 FOR EMERGENCY EXIT LIGHTS AT SEATS 9D T 16D.
2008
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,359 hrs · 20,359 cycles
JFK - EXTERIOR EMERGENCY LIGHT AT OVERHEAD SEAT 3EF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 3EF. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,359 hrs · 20,359 cycles
JFK - EXTERIOR EMERGENCY LIGHT AT RT NR 4 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NR 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,359 hrs · 20,359 cycles
JFK - EMERGENCY EXIT SIGN AT RT NR 4 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT RT NR 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,207 hrs
MIA - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: LIGHT — INOPERATIVE (EXTERIOR)
DFW - AFT EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR AFT EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 27C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 27C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (EXTERIOR)
DFW - AFT EXTERIOR EMERGENCY LIGHT AT LEFT AFT ENTRY DOOR INOPERATIVE. REPLACED LAMP FOR AFT EXTERIOR EMERGENCY LIGHT AT LEFT AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SWITCH — LOOSE (EXTERIOR)
DFW - EXTERNAL EMERGENCY LIGHT SWITCH BY NOSE STRUT IS LOOSE. TIGHTENED EXTERNAL EMERGENCY LIGHT SWITCH BY NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: A/C PACK — ODOR (LEFT)
MIA - DURING DESCENT BELOW 8000 FEET, LEFT PACK CREATED OIL SMELLING FUMES VISIBLE IN COCKPIT. TURNING OVER PACK CLEARED AIR AND ODOR. NO ENGINE INDICATING OR CREW ALERTING SYSTEM OR OTHER INDICATIONS. LANDED MIA WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. ACCOMPLISHED INSPECTION OF LEFT PACK. NO FAULTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: PIN — MISSING (BRAKE)
SFO - DURING PUSHBACK FOR TRIP 1684, NUMBER THREE BRAKE ROD DROPPED DOWNWARD. AIRCRAFT OUT OF SERVICE FOR REPAIRS. FOUND BRAKE ROD ATTACH PIN MISSING. REPLACED BRAKE ROD AND ALL ATTACHING PARTS INCLUDING ROD BOLTS, BRAKE LINE, BRAKE ASSEMBLY AND WHEEL/TIRE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: FIRE DETECTOR — OBSTRUCTED (CARGO BAY)
DEN - CARGO DETECTION AIR STATUS MESSAGE IN FLIGHT. LANDED DEN WITHOUT INCIDENT. FOUND BAGS IN AFT COMPARTMENT STACKED TO CEILING IMPEDING AIR FLOW TO DETECTORS. REALIGNED BAGS AND TESTED CARGO FIRE DETECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT FORWARD OF ROW 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT FORWARD OF ROW 26. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BLOWER — INOPERATIVE (SMOKE DETECTOR)
BOS - INFLIGHT CARGO DETECTION AIR STATUS MESSAGE DISPLAYED AFTER TAKEOFF. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. REPLACED PLENUM PRESSURE SWITCH FOR NUMBER 4 SMOKE DETECTION BLOWER. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: TUBE — OBSTRUCTED (CARGO BAY FAN)
MIA - CAPTAIN REPORTED FIRE INDICATION IN AFT CARGO COMPARTMENT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ACCOMPLISHED BITE TEST WITH NO FAULTS NOTED. REMOVED DEBRIS FROM AFT CARGO COMPARTMENT FAN TUBING. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
EMERGENCY EXIT DOOR LIGHTS ON SEATS 16D THROUGH 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT DOOR LIGHTS ON SEATS 16D THROUGH 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: SENSOR — FAILED (CARGO BAY)
LAX - FLT 276 - AIRCRAFT EN ROUTE LAX-MIA WHEN AFT CARGO SMOKE DETECTOR INDICATED A FIRE. RETUNED IMMEDIATELY TO LAX FOR A LANDING WITHOUT INCIDENT. AIRCRAFT WAS OVERWEIGHT. PERFORMED OVERWEIGHT INSPECTION. REPLACED FAILED WARNING SYSTEM SENSOR IN THE AFT CARGO. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: TERMINAL BLOCK — DEFECTIVE (E/E BAY)
BOS - FLT 1044 - ON TAXI-IN, SEVERAL COMPONENTS ON LEFT BUS ARE INOPERATIVE. REPLACED TERMINAL BLOCK AND TERMINAL ENDS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)