N283AA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
21 reports on file, 1996-05-15 – 2007-08-14.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
LGA - EMERGENCY LIGHT AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT FORWARD GALLEY CEILING FOR EMERGENCY LIGHT AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: COALESCER BAG — DISCONNECTED (AIR CONDITIONING)
TUL INFLIGHT T2528/21JUL - DURING CLIMB FLIGHT ATTENDANT REPORTED ODOR AND SMOKE IN CABIN. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. FOUND RIGHT COALESCER BAG OFF AND STUCK TO BOTTOM OF DUCT. REPLACED BOTH COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Earlier reports · 1996–2006 · 19 reports
2006
Part: APU — INOPERATIVE (APU BAY)
STL - CREW REPORTED SMOKE IN CABIN. RETURNED TO STL AND LANDED WITHOUT INCIDENT. FOUND APU HAD INGESTED OIL. REPLACED APU ON 16 SEPTEMBER AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: PUMP — INOPERATIVE (ZONE 100)
DFW INFLIGHT T1296/22AUG - AIRCRAFT WOULD NOT TRANSFER FUEL FROM CENTER TANK. FORWARD BOOST PUMP CIRCUIT BREAKER POPPED ON TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED CENTER FORWARD TANK BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.
2002
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMEREGNCY EXIT LIGHTS IN TAIL INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY — INOPERATIVE (GALLEY)
DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT AND FORWARD ENTRANCE AND GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED COCKPIT AND FORWARD ENTRANCE AND GALLEY EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: WIRE — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT GALLEY INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT WIRE AT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SOCKET — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: PANEL — CORRODED (BS 243)
TUL - FORWARD LAV SERVICE PANEL PAN HAS CORROSION ON INBOARD SURFACE FLANGE AROUND DUMP CHUTE AND BETWEEN PAN AND PAN STIFFENER. REPLACED PAN AND PAN STIFFENER PER SRM 51-30. (M)
1999
Part: LIGHT — INOPERATIVE (EMER EXIT)
DFW - DURING MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT OVERWING EXIT INOPERATIVE. REPLACED EMERGENCY PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: ACTUATOR — LEAKING (NLG)
DFW - FLT 2012 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT AND NOSE GEAR UNSAFE LIGHT ILLUMINATED. EXTENDED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR RETRACTION CYLINDER. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)
Part: CUSP — CORRODED (BS 160-200)
TUL - FOUND CORROSION ON RIGHT CUSP AT FORWARD SERVICE DOOR. INSTALLED DOUBLER PER SRM 53-01 PAGE 2, SHEET 3, PER ESO 80554, DATED 5-21-96. (M)
Part: SEAT TRACK — CORRODED (BS 1060-1182)
TUL - FOUND SEAT TRACK CORROSION BLENDED BEYOND MANUAL LIMITS FROM STATION 1060 TO STATION 1182, REF E58-4A 0095459, 0095471, 0095483. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05. (M)
Part: SUPPORT — CORRODED (BS 160-200)
TUL - FOUND CORROSION ALONG FLOOR SUPPORT STATION 160 TO 200 AT CLIP NUT AREAS, CORROSION BEYOND LIMITS. REPLACED ANGLE SUPPORT. (M)
Part: CUSP — CORRODED (BS 160-200)
TUL - FOUND CORROSION ON RIGHT CUSP AT FORWARD SERVICE DOOR AREA STATION 160 TO 200 (CORROSION REMOVED AND BEYOND LIMITS FOR THICKNESS). INSTALLED DOUBLER PER SRM 53-01 PAGE 2 SHEET 3. (M)
Part: CUSP FITTING — CORRODED (BS 200)
TUL - FOUND CORROSION AT CUSP FITTING JUST AFT OF FORWARD SERVICE DOOR CUTOUT, (CORROSION REMOVAL BEYOND LIMITS). INSTALLED DOUBLER PER ESO NR 80559. (M)
Part: SEAT TRACK — CORRODED (BS 1210)
TUL - FOUND GALLEY TIE DOWN IN SEAT TRACK NR 1 HAS INTERGRANULAR CORROSION AT STATION 1210. CUT OUT AREA THAT WAS BEYOND LIMITS AND INSTALLED PLUG PER SRM 53-05 FIG 4A AND TREATED AND PRIMED. (M)
Part: SEAT TRACK — CORRODED (BS 1212-1250)
TUL - FOUND CORROSION ON TOP OF TRACK NR 1 AND GALLEY TIE DOWNS HAS INTERGRANULAR CORROSION IS FROM STATION 1212-1250. CUT OUT AREA THAT WAS BEYOND LIMITS AND INSTALLED PLUG PER SRM 53-05 FIG 4A AND TREATED AND PRIMED. (M)
Part: SEAT TRACK — CORRODED (BS 1195)
TUL - FOUND CORROSION ON SEAT TRACK NR 3 AT STATION 1195. INSTALLED PLUG IN SEAT TRACK AT STATION 1195 PER SRM 53-05 FIG 4A. (M)
Part: JAMB — CORRODED (BS 160-200)
TUL - FOUND CORROSION LEFT CUSP AT FORWARD ENTRY STATION 160 TO 200. INSTALLED DOUBLER PER ESO 80559, DATED 5-17-96. (M)