FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N54332 and the event date: after January 26, 1949, when the previous aircraft’s registration ended, through this one’s cancellation.
Incident 19871207076069IInitial Approach-IFR · St Louis, MOStrong vibration felt on NR3 engine. Landed with engine at idle. Engine had internal turbine damage.Incident 19820106006049IGround Taxi, Other Airplane · Phoenix, AZZo taxiing to takeoff, passenger spoke to others of bombs and exploding aircraft. Returned to gate. No bomb found.Incident 19790428200619INormal Cruise · Wichita, KSUnidentified caller reported bomb on board. Made emergency landing. Total search found no bomb.
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TWAA9819901Door · not latchedON LIFT OFF GOT AN EQUIPMENT ACCESS DOOR ANNUNCIATOR LIGHT. THE PLANE WOULD NOT PRESSURIZE, OPERATIONAL CHECK OF THE DOOR WAS MADE. CC-01 01-24-98 MCI.SDR TWAA9711705Skin · corrodedMCI - REMOVED CORROSION FROM SKIN AROUND ANTENNA MOUNT PLATE RING INSIDE CARGO BIN RADIO ALTIMETER NR 1. (M)SDR 96ZZZM213Frame · crackedMCI - DURING C-CHECK, FOUND CRACK IN LEFT FUSELAGE FRAME AT 5TH HOLE FROME BOTTOM OF FUSELAGE FRAME. REPAIRED PER DWG NR 65C36280, SHEET 1.SDR TWAA9572Gaskets · failedSTL - DURING CLIMB SHUT DOWN NR 1 ENGINE, S/N 1537, DUE TO STRUT OVERHEAT. FOUND 13TH STAGE AIR LEAK AT WING ANTI-ICE VALVE. REPLACED GASKETS, MFG P/N 60023-1, AT 13TH STAGE VALVE. PERFORMED HIGH POWER RUNUP LEAK CHECK AND OPERATION WAS NORMAL. (M)SDR 95ZZZX3183Nr 3 Bearing · failedONT - FLT 54 - RETURNED FROM FLIGHT ACCOUNT NR 3 ENGINE OIL BYPASS LIGHT CAME ON AND OIL TEMPERATURE ROSE. FOUND METAL IN MAIN OIL SCREEN. REPLACED ENGINE SN 1543. ENGINE TOTAL TIME: 34,195 HOURS; 22,195 CYCLES. CHECK C-2 - 1-4-95 - MCI. INVESTIGATION INSDR 95ZZZX712Casting · crackedMCI - DURING CHECK C-2D, FOUND .75 INCH CRACK IN TOP INBOARD CORNER OF NR 1 ENGINE AFT ENGINE MOUNT CASTING. REPAIRED BY INSTALLING DOUBLERS PER BOEING DWG 65C34994. AIRCRAFT TOTAL TIME: 61,014 HOURS; 40,930 CYCLES.SDR 95ZZZX546Bulkhead · crackedDURING CHECK C-2D, FOUND CRACK APPROXIMATELY TWO INCHES IN BULKHEAD BELOW APU FLOW CONTROL VALVE, IN RT MLG WHEELWELL. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TWA DWG C03242 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 61,014 HOURS; 40,930 CYCLES.
Other aircraft with N54332 · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N54332 now.