FAA incident reports · 7
FAA accident and incident reports matched to this aircraft by N997Z and the event date: up to this one’s cancellation.
Incident 19951229045759IFcd/Prec Ldg From Cruise · Tulsa, OKNarrative: first officer notified ATC that the captain had become incapacitated enroute from sat to stl, and requested a deviation to tul. The DC-9 landed safely at tul without further incident and the captain was transported to a local hospital. This…Incident 19871115073309INormal Cruise · Springfield, MOLost cabin pressure at 33M. Made emergency descent. Manual mask drop but all did not deploy. Replaced controller.Incident 19860706041259ITakeoff Ground Roll · St Louis, MOAborted takeoff when tail compartment high temperature light came on. Replaced clamp on right augmentation valve.Incident 19860111003109INormal Cruise · Kansas City, MOEngine vibration at FL350. Shut down and diverted. Found first stage fan blade failure.Incident 19790308019669IDescent · St Louis, MOCrew felt bump on descent, inspection revealed upper cowling and forward lower cowling missing.Incident 19790110000359IOther Ground Ops · Sioux City, IACatering truck struck and damaged the inboard slat, right side.Incident 19780913017209IGround Taxi, Other Airplane · Rockford, ILAircraft slid off wet taxiway that had just been sealed.
Service difficulty reports · 52
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TWAA0000502Actuator · wornCREW WAS UNABLE TO EXTEND THE NOSE LANDING GEAR DURING APPROACH TO MLI WAS NECESSARY TO USE MANUAL NOSE GEAR EXTENSION. FOUND PROBLEM WAS THE NOSE LANDING GEAR BUNGEE CYLINDER. MAINTENANCE FERRIED THE AIRCRAFT TO STL FOR REPLACEMENT. CHECK-C 8-28-99 STL.SDR TWAA9911803Longeron · crackedDURING CHECK-C MAINT, LONGERON 2R WAS FOUND CRACKED AT END CAP STA 1076, A ONE INCH CRACK. REPAIRED PER SRM 53-02, FIG 8 AND 18.SDR TWAA9911802Longeron · crackedDURING CHECK-C MAINT, LONGERON 2L WAS FOUND CRACKED AT THE END CAP STA 1076, ONE INCH LONG. REPAIRED PER SRM 53-02, FIG 8 AND 18.
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