N1436A
Registered owner: WHITNEY RICHARD T TRUSTEE, CO (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.
16 reports on file, 1996-01-09 – 2006-03-03.
Part: ARM — CRACKED (SEAT)
CENTER ARMREST CRACKED AT ATTACH BRACKET TO SEAT FRAME, HAVE SEEN OTHER SEATS WITH SAME CONDITION, FLIGHTLINE IN TULSA IS WORKING WITH FSDO IN CALIFORNIA AND FLIGHTLINE ENGINEERING. AMERICAN AIRLINES HAS A REPAIR PROCEDURE FOR THIS PART.
Earlier reports · 1996–2003 · 15 reports
2003
Part: LIGHT — MISSING (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AFT ROW 11D MISSING. INSTALLED EMERGENCY EXIT PATH LIGHTING AFT ROW 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: O-RING — TORN (HYD SYSTEM)
CVG - FLT 1712 - EN ROUTE DFW-CVG, LEFT HYDRAULIC SYSTEM QUANTITY ALERT. MANUALLY LOWERED GEARS AND FLAPS. LANDED CVG WITHOUT INCIDENT. REPLACED NR 1 HYDRAULIC SYSTEM O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
FLOORBEAM CAP CORRODED BLO, STA 4610-4710. CUTOUT CORROSION, INSTALLED STRAP AND DOUBLER IAW AARD.
Part: FLOORBEAM — CORRODED (FUSELAGE)
FLOORBEAM CAP CORRODED. BL1127L, STA 3845-4850. REMOVED AND REPLACED TEE-CAP, STA 4175-4575.
Part: FITTING — CORRODED (GIRT BAR)
FORWARD GIRT BAR BLOCK FITTING CORRODED AT FORWARD ENTRY. STA3850 FLOORBEAM 1420L. REMOVED AND REPLACED GIRT BAR BLOCK FITTING IAW SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE)
FLOORBEAM CAP CORRODED. (PL600L, STA 3845-4850). CUTOUT CORROSION, INSTALLED FLOORBEAM CAP STA 4175-4575 PER AARD.
Part: FLOORBEAM — CORRODED (FUSELAGE)
FLOORBEAM, BL600R, CAP CORRODED, STA 3845-4850. CUTOUT CORROSION, INSTALLED FLOORBEAM CAP 3845-4850 PER SRM.
Part: CONNECTOR — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT FROM FORWARD GALLEY TO SEAT 11D INOPERATIVE. TIGHTENED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR FORWARD OF SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: ACM — MALFUNCTIONED (A/C BAY)
MSP - FLT 1482 - EN ROUTE MSP-ORD, SHORTLY BEFORE TAKEOFF DETECTED SMOKE IN COCKPIT. RETURNED MSP GATE WITHOUT FURTHER INCIDENT. REPLACED AIR CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: FAN — FAILED (ACM BAY)
DFW - FLT 0697 - DURING DESCENT, DETECTED A BURNING SMELL IN COCKPIT AND CABIN. LANDED DFW WITHOUT INCIDENT. REPLACED LT PACK RECIRCULTION FAN. ACCOMPLISHED PACK BURN-OUT. SYSTEM GROUND CHECK, NORMAL OPERATION. (X)
1999
Part: BRAKE — DEFECTIVE (RT MLG)
DFW - FLT 2087 - UPON LANDING AT DFW FROM OMA, NR 3 AND 4 MLG BRAKES LOCKED. NR 3 AND 4 BRAKES SMOKED WHICH REQUIRED APPLICATION OF FIRE SUPRESSION FOAM. PASSENGERS WERE DEPLANED ON TAXI WAY. REPLACED NR 3 AND 4 BRAKES AND WHEEL/TIRE ASSEMBLIES. RIGHT WING, FUSELAGE AND RIGHT MAIN LANDING GEAR CLEANED OF FIRE SUPPRESSION FOAM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: WIRE — BROKEN (EMERG EXIT DOOR)
ORD - DURING OVERNIGHT CHECK, LEFT EMERGENCY EXIT DOOR COVER MISSING BREAK AWAY SAFETY WIRE. INSTALLED SAFETY WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: PUMP — DEFECTIVE (NR 1 HYD SYSTEM)
ORD - FLT 1508 - EN ROUTE OKC/ORD DURING CRUISE, HYD SYSTEM 1 EXPERIENCED LOW QTY. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT PROCEEDED TO ORD. ACCOMPLISHED ALTERNATE GEAR AND FLAP EXTENSION AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED NR 2 ENGINE SYSTEM 1 ENGINE DRIVEN HYD PUMP. SERVICED HYD SYSTEM AND ACCOMPLISHED LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: VALVE — DEFECTIVE (NLG DOOR)
DFW - FLT 1139 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR CONTINUED TO INDICATE AMBER. RECYCLED LANDING GEAR WITH SAME RESULTS. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO DFW, LANDING OVERWEIGHT WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOOR SELECTOR VALVE. ACCOMPLISHED LEAK CHECK AND LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. (M)
Part: PUMP — DEFECTIVE (NR 1 ENGINE)
JFK - FLT NR 1072 - EN ROUTE YYZ/JFK - DURING CRUISE, LOST SYSTEM 1 HYDRAULIC QUANTITY WITH PRESSURE DROPPING TO 500 PSI AND QUANTITY AT 35. SYSTEM 2 PRESSURE AND QUANTITY NORMAL. ACCOMPLISHED QRH PROCEDURES FOR NR 1 HYDRAULIC SYSTEM AND AIRCRAFT PROCEEDED TO JFK. ACCOMPLISHED ALTERNATE LANDING GEAR EXTENSION AND ALTERNATE FLAP EXTENSION AND AIRCRAFT LANDED JFK WITHOUT INCIDENT. REPLACED NR 1 ENGINE HYDRAULIC PUMP AND SERVICED SYSTEM. ACCOMPLISHED LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)