N1432A
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.
13 reports on file, 1997-07-12 – 2002-03-22.
Part: BULKHEAD — GOUGED (FUSELAGE)
TUL - FOUND SCREW GOUGE ON FORWARD SIDE OF PERSSURE BULKHEAD (AFT) UNDER NR 3 RIGHT AFT LAVATORY BENCH ASSEMBLY MOUNT BRACKET. REPAIRED PER ESO 51000, DATED 26 OCT 01 AARD 53-65-00. (M)
Part: BULKHEAD — GOUGED (FUSELAGE)
TUL - FOUND SCREW GOUGE ON FORWARD SIDE OF AFT PRESSURE BULKHEAD UNDER NR 4 RIGHT AFT LAVATORY BENCH MOUNT BRACKET. REPAIRED PER AARD 53-65-00 ESO 51000 DATED 28 OCT 01. (M)
Part: DOOR FRAME — CORRODED (FUSELAGE)
TUL - FOUND MID CARGO AFT DOOR FRAME CORRODED. FABRICATED DOUBLER AND INSTALLED PER ESO 51000 DATED 14 MAR 02. (M)
Part: DOOR FRAME — CORRODED (FUSELAGE)
TUL - FOUND CORROSION AROUND FASTENER HOLES ON FORWARD SIDE OF FRAME 22236 AT CARGO DOOR OPENING. INSTALLED DOUBLER PER ESO 51000 DATED 3/5/02. (M)
Part: DOOR FRAME — CORRODED (FUSELAGE)
TUL - FOUND CORROSION AROUND FASTENER HOLE ON AFT SIDE OF FRAME 20778 AT CARGO DOOR OPENING. INSTALLED DOUBLER PER ESO51000 DATED 3-5-02. (M)
Part: BULKHEAD — DAMAGED (FUSELAGE)
TUL - FOUND DAMAGE TO AFT PRESSURE BULKHEAD DUE TO IMPROPER FASTENER INSTALLATION. INSTALLED DOUBLER LEFT SIDE OF AFT PRESSURE BULKHEAD PER ESO 51000, CHAPTER 53-65-00. (M)
Earlier reports · 1997–2001 · 7 reports
2001
Part: WIRE — INOPERATIVE (L1 DOOR)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT FLOOR CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20H THROUGH 29H DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AT SEATS 24H AND 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1999
Part: SYNCHRONIZER — FAILED (LT TE FLAP)
DSM - FLT 1091 - EN ROUTE DFW/DSM DURING CRUISE, HAD FLAP ASEMBLY ON LEFT AND RIGHT MFDU. FLAPS WOULD NOT EXTEND. TRIED PULLING AND RESETTING 7H, 7J, 40K, 14K CIRCUIT BREAKERS FOR MFDU. WARNINGS EXTINGUISHED, BUT WHEN FLAPS WERE CALLED FOR ON APPROACH NOTHING HAPPENED. MADE ZERO FLAP APPROACH LANDING AT DFW. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LEFT INBOARD FLAP ASSMELBY TRNASMIEMBLY TRANSMITTER. ACCOMPLISHED ALL REQUIRED CHECKS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1998
Part: LIGHT — DEFECTIVE (EMERGENCY EXIT)
DFW - DURING OVERNIGHT MAINTENANCE, RIGHT AFT FAIRING EXTERIOR EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. REPLACED RIGHT AFT FAIRING EXTERIOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DAMAGED (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EMERGENCY EXIT LIGHT DAMAGED. REPLACED LEFT AFT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WARNING — MALFUNCTIONED (COCKPIT)
COS - FLT 659 - AFTER TAKEOFF, EIGHT DEGREES FLAPS WAS SELECTED AND A FLAP ASYMMETRY MESSAGE APPEARED ON MFDU. FLIGHT CREW DECLARED AN EMERGENCY AND LANDED COS WITHOUT FURTHER INCIDENT. MAINTENANCE RESET ASYMMETRY FAULT BALL ON MAINTENANCE TEST PANEL AND CYCLED FLAPS SEVERAL TIMES UNABLE TO DUPLICATE FAULT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: PACKING — FAILED (LT ENGINE)
ORD - FLT 0892 - DURING DESCENT INTO ORD, LOST HYDRAULIC SYSTEM 1. ACCOMPLISHED ABNORMAL PROCEDURES FOR LOSS OF HYDRAULIC SYSTEM 1 AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED PACKING ON LEFT ENGINE NR 1 HYDRAULIC PUMP PRESSURE FITTING AT PUMP. SYSTEM LEAK AND GROUND CHECK NORMAL OPERATION. (X)