N288AA
Registered owner: ANDURIL INDUSTIRES INC, CA (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.
33 reports on file, 1995-07-11 – 2006-01-09.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DTW - EMERGENCY EXIT LIGHTS AT FORWARD ENTRY DOORS AND SEAT ROWS 3 TO 15 INOPERATIVE. REPLACED FORWARD CONTROL AND BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.
Earlier reports · 1995–2005 · 32 reports
2005
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
EMERGENCY LIGHTS IN FORWARD ENTRY AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD ENTRY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
LAX - EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. SECURED LOOSE CONNECTOR UNDER SEAT 5E FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SLIDE — DISCHARGED (GALLEY DOOR)
MSP - AFT GALLEY DOOR SLIDE PRESSURE OUT OF LIMITS. REPLACED SLIDE AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CIRCUIT BREAKER — POPPED (EMERGENCY LIGHT)
PHX - INFLIGHT T1418 AIRCRAFT BATTERY CHARGER CIRCUIT BREAKER POPPED. REPLACED BATTERY CHARGER AND CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY — DISCHARGED (CABIN)
DFW - EMERGENCY EXIT SIGN AT RIGHT AND LEFT HAND OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY FOR EMERGENCY EXIT SIGN AT RIGHT AND LEFT HAND OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY — DISCHARGED (CABIN)
DFW - EMERGENCY EXIT SIGN AT AFT GALLEY EXIT DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY EXIT SIGN AT AFT GALLEY EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY — DISCHARGED (CABIN)
DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 12 AND 16 INOPERATIVE. REPLACED BATTERY FOR THE OVERHEAD EMERGENCY LIGHT AT ROWS 12 AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY — DISCHARGED (CABIN)
DFW - TAIL SECTION OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY FOR TAIL SECTION OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE AFT SERVICE DOOR LOCATION. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT THE AFT SERVICE DOOR EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY — NOT SEATED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: BATTERY — DISCHARGED (CABIN)
AUS - DURING OVERNIGHT MAINTENANCE, FORWARD CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: LIGHT — DEFECTIVE (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT OVERWING EXIT TOO BRIGHT. REPLACED EMERGENCY EXIT LIGHT AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: APU — LEAKING (APU BAY)
ORD - FLT 1836 - EN ROUTE TUS-ORD, SHORTLY AFTER TAKEOFF, DETECTED LIGHT HAZE AND SMELL IN CABIN. BOTH PACKS TAKEN OT OF FULL COLD. SMELL AND HAZE DISSIPATED AND DID NOT RETURN FOR THE REMAINDER OF THE FLIGHT. LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED APU. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: APU — LEAKING (APU BAY)
DFW - FLT 1806 - AFTER TAKEOFF, CABIN FILLED WITH SMOKE. LANDED DFW WITHOUT INCIDENT. REPLACED AUXILIARY POWER UNIT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: FLOORBEAM — WORN (BS 845)
TUL - INBOARD OF NR 3 SEAT TRACK FLOORBEAM WORN AT FS 845. BLENDED OUT WEAR DYE CHECKED FOR WEAR. INSTALLED DOUBLER PER ESO 80559 REV 118. (M)
Part: FLOORBEAM — WORN (BS 864)
TUL - INBOARD OF NR 3 SEAT TRACK FLOORBEAM WORN AT FS 864. BLENDED OUT AREA DYE CHECKED. INSTALLED ODUBLER PER ESO 80559. (M)
Part: SKIN — DENTED (BS 245-249)
TUL - A 4 INCH DENT BETWEEN STATION 245 AND 249, 1 INCH BELOW LONGERON 17 LEFT AND 1 INCH DENT AT STRINGER 244, 3 INCHES ABOVE LONGERON 18 LEFT. (M)
Part: FRAME — CRACKED (BS 1212)
TUL - AFT CARGO FRAME WEB CRACKED FROM LIGHTNING HOLE STATION 1212, LONGERON 27R. REMOVED OLD WEB. INSTALLED NEW WEB AND FASTENERS PER AARD 53-10-00-24. (M)
Part: FLOORBOARD — CORRODED (BS 148)
TUL - FOUND CORROSION ON COCKPIT FLOORBOARD, STATION 148 BETWEEN SEAT TRACKS, RIGHT SIDE RBL 23-27. INSTALLED NEW FLOORBOARD PER SRM 51-01. (M)
Part: SEAT TRACK — CORRODED (BS 1174-1278)
TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 1174, 1231, 1250, 1265 AND 1278. REPLACED CORRODED SEAT TRACK WITH NEW ONE PER SRM 51-01. (M)
Part: SEAT TRACK — CORRODED (BS 824-828)
TUL - NR 6 SEAT TRACK CORRODED STATION 824-828. REMOVED OUT OF LIMITS AREA AND INSTALLED PLUG PER AARD 53-20-00-10. (M)
Part: FRAME — MISDRILLED (BS 1287)
TUL - FOUND DOUBLE DRILLED HOLE ON FUSELAGE FRAME BELOW LONGERON 7L, AFT SIDE OF FS 1287. INSTALLED DOUBLER AT FS 1287, STRINGER 7L TO 8L PER SRM 53-03, PAGE 129. (M)
Part: SEAT TRACK — CORRODED (BS 670-674)
TUL - NR 6 SEAT TRACK CORRODED STATION 670-674. REMOVED CORROSION CUTOUT DAMAGED AREA AND INSTALLED PLUG PER AARD 53-20-00-10 PAGES 1-3. (M)
Part: SEAT TRACK — CORRODED (BS 234-237)
TUL - NR 4 SEAT TRACK TANG CORRODED. REPAIRED SEAT TRACK PER SRM 53-05 PART 1 FIG 4A. (M)
Part: SEAT TRACK — CORRODED (BS 824-828)
TUL - NR 6 SEAT TRACK CORRODED STATION 824-828. SEAT TRACK PLUG PER AARD 53-20-00-10. (M)
Part: SEAT TRACK — CORRODED (BS 576-582)
TUL - NR 6 SEAT TRACK CORRODED STATION 576-582. REPAIRED SEAT TRACK PER AARD 53-20-00-10 SEAT TRACK PLUG. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT CEILING FORWARD OF VENTRAL AIRSTAIR DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT AFT CEILING FORWARD OF VENTRAL AIRSTAIR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOORPATH LIGHT STRIP CLOSE TO FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: GEAR HANDLE — STUCK (COCKPIT)
DFW - FLT 2347 - AFTER TAKEOFF DFW, GEAR HANDLE WOULD TRAVEL MIDWAY AND STOP. CREW RAN CHECKLIST AND GEAR HANDLE RELEASE BUTTON WAS PUSHED WITH HANDLE TRAVELING MIDWAY AND STOPPING. AIRCRAFT RETURNED TO DFW AND WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED LANDING GEAR MECHANISM AND FOUND DEBRIS. DEBRIS WAS REMOVED. ACCOMPLISHED GEAR RETRACTION WITH NO FURTHER DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: LAV SERVICE PNL — CORRODED (BS 1287-1308)
TUL - FOUND HEAVY CORROSION ON INSIDE OF AFT LAV SERVICE PAN. INSTALLED DOUBLER PER ESO80559 DATED 5-3-96. (M)
1995
Part: WIRE — BROKEN (E/E COMPT)
ORD - FLT 1155 - AFTER T/O, JUST AFTER SLAT RETRACTION, A/C LOST YAW DAMPER OPERATION AND SIMULTANEOUS COMPUTER FAILURE WITH ALTITUDE IND STUCK AT FL 130, AIRSPEED IND STUCK AT 250 KTS AND FLT GUIDANCE COMPUTER C/B TRIPPED. A/C RETURNED AND LANDED W/O INCIDENT. GRD CHK OF FLT GUIDANCE SYS WAS UNABLE TO DUPLICATE PROBLEM. CHK'D WIRING IN AFT TAIL COMPART WITH NO DEFECTS NOTED. PRECAUTIONARY REPLACED NR 1 AND NR 2 DFGC'S NR 1 AND NR 2 AUTOPILOTS GRD CHK'D NORM OPERATION AND NR 1 AND NR 2 DFGC'S GROUND CHK'D NORM OPERATION. SUBSEQUENTLY, ON FLT 0578 DURING DESCENT IN DCA, PROB REPEATED. A/C LANDED DCA W/O INCIDENT. REPAIRED WIRE 2C610U2ORD BTWN P10-1206 AND S30-5 POST NR 10, WDM REF 22-16-11. OPS CHK OK.(M)