N294AA
Registered owner: AMERICAN SAMOA COMMUNITY COLLEGE, AS (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.
37 reports on file, 1996-04-09 – 2009-07-23.
Part: FITTING — CRACKED (DOOR) · airframe 62,368 hrs · 32,853 cycles
TUL - AFT CABIN BULKHEAD DOOR LOWER DOOR BEAM LEFT SIDE BAYONET LATCH FITTING CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW LOWER BAYONET LATCH FITTING IN DOOR UNDER ESO-80186 E58-6375157 MRT-021974.
Part: BRACKET — CRACKED (RT MLG ACTUATOR) · airframe 62,367 hrs · 32,851 cycles
RT WHEEL WELL MLG DOOR ACTUATOR BRACKET CRACKET. REMOVED AND REPLACED BRACKET PER AARD 51-00-00-012 AND SRM 51-30-05.
Part: SKIN — CRACKED (VERTICAL STAB) · airframe 62,366 hrs · 32,851 cycles
VERTICAL STAB L/E SKIN CRACKED AFT OF RAM AIR INTAKE LEFT SIDE. INSTALLED DOUBLER PER SRM 55-01-00 FIGURE 2 SHEET 2.
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 62,366 hrs · 32,851 cycles
CRACK IN RIGHT WHEEL WELL PRESSURE DECK ADJACENT TO FUEL SHROUD SUPPORT ANGLE. INSTALLED DOUBLER PER SRM 53-01 FIGURE 2 SHEET 3.
Part: BRACKET — CORRODED (CARGO BAY) · airframe 62,367 hrs · 32,851 cycles
CORNER BRACKET IN MID CARGO CORRODED. REPLACED CORNER BRACKET PER AARD 51-00-00-012.
Part: BRACKET — DAMAGED (CARGO BAY) · corrosion level 2 · airframe 62,366 hrs · 32,851 cycles
MID CARGO AFT CORNER BRACKET HAS CORROSION. REMOVED AND REPLACED CORNER BRACKET PER AARD 51-00-00-012.
Part: FITTING — CORRODED (FUSELAGE) · airframe 62,367 hrs · 32,851 cycles
CORROSION ON DOOR JAMB LOWER FWD FITTING IN MID CARGO. REPLACED BRACKET PER AARD 51-00-00-012.
Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,367 hrs · 32,851 cycles
TOP FORWARD STOP PAD FITTING CRACKED ON AFT CARGO DOOR. REMOVED AND REPLACED FITTING PER ESO 80174.
Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 62,366 hrs · 32,851 cycles
CABIN FORWARD ENTRY AREA HAS CORROSION ON INBOARD G1 GALLEY SUB FLOOR MOUNT BRACKET. INSTALLED NEW G1 GALLEY MOUNT BRACKET PER SRM 51-30-15.
Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 62,367 hrs · 32,851 cycles
CRACK IN VERTICAL STABILIZER SKATE ANGLE DOUBLER. REMOVED AND REPLACED WITH NEW SKATE ANGLE DOUBLER PER AARD 53-10-00-2
Part: STOP FITTING — CRACKED (DOOR) · airframe 62,369 hrs · 32,854 cycles
DOOR STOP FITTING AT FORWARD END OF NUMBER 5 BEAM IS CRACKED. REMOVED AND INSTALLED A SERVICEABLE DOOR STOP FITTING.
Part: STOP FITTING — CRACKED (DOOR) · airframe 62,369 hrs · 32,854 cycles
DOOR STOP FITTING AT FORWARD END OF NUMBER 1 BEAM IS CRACKED. REMOVED AND INSTALLED A SERVICEABLE DOOR STOP FITTING.
Part: STOP FITTING — CRACKED (DOOR) · airframe 62,369 hrs · 32,854 cycles
DOOR STOP FITTING AT FORWARD END OF NUMBER 3 BEAM IS CRACKED. REMOVED AND INSTALLED A SERVICEABLE DOOR STOP FITTING.
Earlier reports · 1996–2003 · 24 reports
2003
Part: BATTERY — DISCHARGED (COCKPIT)
DTW COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR COCKPIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED
Part: FLASHLIGHT — INOPERATIVE (CABIN)
SEA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: CONNECTOR — NOT SEATED (CABIN)
DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT CEILING LIGHT FROM ROW 19-21, INOPERATIVE. RESET OVER EMERGENCY EXIT LIGHT BATTERIES CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2001
Part: BATTERY — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN SEAT MOUNTED EMERGENCY EXIT ESCAPE PATH LIGHTS DIM. REPLACED AFT CABIN EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, AFT RIGHT OVERHEAD EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK FOR AFT RIGHT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY LIGHTS ABOVE ROWS 29, 30, AND 31 REPORTED INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS ABOVE ROWS 29, 30 AND 31. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY LIGHTS ABOVE ROWS 8, 9, AND 10 REPORTED DIM. REPAIRED BATTERY PACK FOR CEILING EMERGENCY LIGHTS ABOVE ROWS 8, 9, AND 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — INOPERATIVE (CABIN)
BOS - DURING OVERNIGHT INSPECTION, EMERGENCY LIGHT CONNECTOR HAS PIN NOT SEATED. RE-SEATED EMERGENCY EXIT LIGHT CONNECTOR PIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1999
Part: SEAT TRACK — CORRODED (BS 1155-1250)
TUL - NR 1 SEAT TRACK CORROSION STATION 1214 DOME NUT 20 EACH SEAT TRACK LUGS CORROSION. INSTALLED NEW SEAT TRACK FROM STATION 1155-1309 SRM 51-01. (M)
Part: SEAT TRACK — CORRODED (BS 1174-1200)
TUL - FOUND CORROSION ON SEAT TRACK STATION 1174 TO 1200 TRACK NR 3. REMOVED CORROSION AND INSTALLED REPAIR 2 PLACES PER SRM AND 1 PLACE PER ESO 80559. (M)
Part: SEAT TRACK — WORN (BS 826)
TUL - INBOARD LUG ON NR 4 SEAT TRACK WORN STATION 826. CUTOUT DAMAGED AREA AND INSTALLED SEAT TRACK PLUG REPAIR PER AARD 53-20-00-10. (M)
Part: CUSP — CORRODED (BS 1231)
TUL - REF E58 NR 0141593, CORROSION ON LEFT CUSP AT STATION 1231 (UNDER SEAT TRACK). INSTALLED NEW CUSP STATION 1174 TO 1250 PER SRM 51-01. (M)
Part: CUSP — CORRODED (BS 1271)
TUL - FOUND CORROSION ON LEFT CUSP AND EXTENDING UNDER DOUBLER AT STATION 1271 APPROX LBL 48. INSTALLED NEW CUSP FROM STATION 1250-1305 SRM 51-01. (M)
Part: SKIN — DAMAGED (BS 305)
TUL - TOOLING DAMAGE IN SKIN T STATION 305, LONG 3R. ACCOMPLISHED REPAIR PER GUIDELINES OF SRM 53-04 FIG NR 38 ALONG WITH THE FOLLOWING, AT THE AFT END OF DOUBLER OVERLAP EXISTING INTERNAL DOUBLER ONE ROW MINIMUM AND OMIT FINGERS AT THE OVERLAPPED DOUBLER PER ESO80559, DATED 11/3/99. (M)
Part: STRINGER — CRACKED (BS 160)
TUL - STRINGER 4L CRACKED AT STATION 160 LEFT. REPLACED DAMAGED SECTION AND INSTALLED SPLICE PER 53-02. (M)
Part: SHEAR TIE — CRACKED (BS 1307)
TUL - SHEAR TIE CRACKED AT STATION 1307, L16, LEFT. REMOVED CRACKED SHEAR TIE FS 1307 STRINGER 16 LEFT. INSTALLED NEW SERVICEABLE SHEAR TIE PER SRM 51-01. (M)
Part: SEAT TRACK — CORRODED (BS 518)
TUL - FOUND CORROSION ON NR 1 SEAT TRACK AT STATION 518. REMOVED DAMAGED AREA. INSTALLED PLUG IN SEAT TRACK PER AARD 53-20-00-10. (M)
Part: SHEAR TIE — CRACKED (BS 1429)
TUL - SHEAR TIE CRACKED JUST INBOARD OF VERTICAL STABILIZER SPAR FITTING RIGHT, AFT SIDE OF STATION 1429. REPLACED SHEAR TIE JUST INBOARD OF VERTICAL STABILIZER SPAR FITTING RIGHT, AFT SIDE OF STATION 1429 PER SRM 51-01. (M)
1998
Part: CONTROLLER — MALFUNCTIONED (FUSELAGE)
DFW - FLT 689 - EN ROUTE ORD, ELP DURING CRUISE AT 28,000 FT FLOW LIGHT ILLUMINATED. PROCEDURES WERE ACCOMP, NO HELP. CABIN ASCENT COULD NOT BE STOPPED IN MANUAL MODE. PERFORMED EXPLOSIVE REPRESSURIZATION PROCEDURE AND DIVERTED TO DFW. PAX'S O2 MASKS DROPPED CORRECTLY. LANDED DFW WITHOUT INCIDENT. REPLACED BOTH PRESSURE CONTROLLERS AND PERFORMED REQUIRED OPERATION CHECKS. PRESSURIZED A/C USING ENGINES AND APU AND PERFORMED LEAK CHECK FOR A/C. INSPECTED OUTFLOW VALVES AND LINKAGES AND PERFORMED FUNCTIONAL CHECK OF AUTO PACK TRIP SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: CLAMPS — LOOSE (LT PACK)
BNA - FLT 1573 - EN ROUTE BNA-DFW - DURING CRUISE, THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH POWER REDUCTION. AIR INTERRUPTED AND LANDED BNA WITHOUT FURTHER INCIDENT. RESECURRED LEFT PACK WATER SEPARATOR CLAMPS. ACCOMPLISHED DUCT LEAK CHECK DURING ENGINE RUN UP AT HIGH POWER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SPAR — CRACKED (VERT STAB)
TUL - FOUND CRACK IN FWD VERT STAB LEFT SPAR LEG ON AFT SIDE OF STATION 1388 CANT FRAME IN AFT ACCY. STOP DRILLED CRACK MANUFACTURED DOUBLER AND INSTALLED PER ESO 80559, DATED 4-12-96. (M)
Part: ANGLE — CORRODED (BS 200)
TUL - ANGLE HAS CORROSION STATION 200 INBOARD OF BELL FRAME SAME STATION. REPLACED WITH NEW ANGLE PER SRM. (M)
Part: ANGLE — CORRODED (BS 160-200)
TUL - FOUND FLOOR SUPPORT ANGLE HAS CORROSION STATION 160 TO 200 AT NUT PLATE HOLES. REPLACED WITH NEW ANGLE PER SRM. (M)
Part: SEAT TRACK — CORRODED (BS 200-230)
TUL - FOUND NR 2 SEAT TRACK CORRODED, BLENDED BEYOND LIMITS. REMOVED BAD SECTION OF TRACK TO PRODUCTION SPLICE, INSTALLED NEW TRACK SRM 53-05. (M)