FAA incident reports · 4
FAA accident and incident reports matched to this aircraft by N54335 and the event date: after February 16, 1949, when the previous aircraft’s registration ended, through this one’s cancellation.
Incident 19880715043789IFinal Approach · St Louis, MOShut down NR3 engine on approach due to a fire warning. Found engine detector sensor loop defective.Incident 19860412018689INormal Cruise · St Louis, MOEmergency descent after cabin pressure surge. Climbed again without problem. Replaced outflow and isolation valve.Incident 19800610054419IFinal Approach-IFR · St Louis, MOLeft main gear warning light on. Aircraft landed safely, problem was indication.Incident 19791012052399IClimb · Tulsa, OKBomb threat recieved ten minutes after departure. Continued to nearby destination, searched, results negative.
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TWAA9909101Wire · brokenTHE RIGHT WING AFT OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. FOUND BROKEN WIRES IN A FLEXIBLE CONDUIT. REPLACED 2 WIRES FROM SPLICE POINT SP5 TO CONNECTOR D5024P, PINS 5 AND 6. CHECK-C 7-31-98.SDR TWAA9812212Skin · wornDURING CHECK C, FOUND RT WING RT O/B FOREFLAP WITH ROUND DEPRESSION WORN IN I/B LEADING EDGE. INSTALLED 2024-T42 DOUBLER PER SRM 57-50-4, PG 2B.SDR TWAA9812211Skin · corrodedDURING CHECK-C, FOUND 14 IN BY 2 IN BY .375 IN HOLE IN LT WING L/E ABOVE LANDING LIGHT. ACCOMP FLUSH REPAIR PER SRM 57-30-4, PAGES 2B, 3, AND 4, FIG 2.SDR TWAA9812209Rib · crackedDURING CHECK-C, FOUND CRACK 17 IN LONG AT BOTTOM OF RT WING RIB WEB ANGLE, 27 IN O/B OF WING BODY FAIRING, FWD. REMOVED AND REPLACED WEB ANGLE AT O/B END OF WING BODY FAIRING, PER SRM 51-10-1, AND 51-40-3.SDR TWAA9812210Stringer · corrodedDURING CHECK-C, FOUND FS 720, S28L WITH CORROSION. HEAVY CORROSION ON STRINGER, LIGHT SKIN CORROSION. REMOVED SKIN CORROSION PER SRM 51-10-6, AND FABRICATED NEW STRINGER AND INSTALLED PER SRM 51-10-1.SDR TWAA9812208Stringer · corrodedDURING CHECK-C, FOUND FUSELAGE STRINGERS CORRODED AT FS 660 TO 680, S27L TO S27R. REMOVED 3 T ANGLE STIFFENERS, REMOVED CORROSION BY ABRASIVE SANDING AND RE-INSTALLED PER SRM 51-10-6, PG 5.SDR TWAA9711601Actuator · malfunctionedSTL - FLT 173 - DURING GEAR RETRACTION THE LEFT MAN GEAR FAILED TO RETRACT ON THE FIRST ATTEMPT, SECOND ATTEMPT WAS SUCCESSFUL. REMOVED AND REPLACD THE LEFT MAIN GEAR ACTUATOR, MFG P/N 65-17830-13, MANUFACTURED BY BOEING. OPERATIONAL CHECK NORMAL. (M)SDR TWAA9613701Connector · looseSTL - FLT 375 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 1541, DUE TO START VALVE LIGHT ILLUMINATION. FOUND DISCONNECT PLUG D374J, MFG PN CA3100KR28-11S727A, CONTAMINATED WITH MOISTURE. REPLACED THE D374J DISCONNECT PLUG. ENGINE START VALVE AND ENGINE OPERASDR TWAA9613601Switch · malfunctionedSTL - FLT 422 - DURING CLIMB, SHUT DOWN NR 1 ENGINE, SN 1541, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND OIL FILTER BYPASS LIGHT SWITCH MALFUNCTIONING. REPLACED BYPASS LIGHT SWITCH, MFG PN A00803-2. ENGINE OPERATION AND INDICATION OK. ENGINE TOTAL TSDR 95ZZZM636Fuel Pump · defectiveSTL - DURING TAKEOFF NR 3 ENGINE, S/N 4018, SPUN DOWN. SHUT DOWN ENGINE PER FLIGHT HANDBOOK PROCEDURES. FOUND DEFECTIVE FUEL PUMP, MFG P/N 378201-7. REPLACED ENGINE DRIVEN FUEL PUMP. ENGINE OPERATION THEN CHECKED NORMAL.
Other aircraft with N54335 · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N54335 now.