TULSAIR BEECHCRAFT, INC.
Also recorded as: TULSAIR BEECHCRAFT, INC.
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
No NTSB accidents or incidents linked to this operator.
FAA enforcement actions
FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal.
7 reports on file.
CREW REPORTED OILY SMOKE ODOR IN CABIN. ISOLATED SOURCE TO RT ENGINE BLEED AIR. RT ENGINE "SHUDDERED" AND BEGAN INCREASING ITT. CREW SHUTDOWN NR 2 ENGINE AND DIVERTED.
PRIOR TO LIFTOFF, THE OUTER RIM OF THE RIGHT INBD MAIN WHEEL SEPARATED FROM THE WHEEL ASSEMBLY. THE FLIGHT CREW WAS NOTIFIED BY RADIO THAT A "TIRE BLEW" DURING TAKEOFF. THE ACFT RETURNED TO BASE AND MADE AN UNEVENTFUL LANDING. BOTH RT MAIN WHEEL ASSEMBLIES WERE REPLACED WITH NEW UNITS.
APU FIRE DETECT CIRCUIT BREAKER POPPED ON RT COCKPIT CIRCUIT BREAKER PANEL DURING POWER UP OF AIRCRAFT. TROUBLESHOT SYSTEM FOUND WIRING CHAFED AT FUSELAGE STATION 614.210 AFT EQUIPMENT BAY UPPER AVIONICS SHELF SUPPORT ANGLE PN 4525708307. THE ANGLE DOES NOT HAVE ANY PROTECTION TO PREVENT CHAFING OF WIRING FROM THE FACTORY AND IT APPEARS THAT CLEARANCE IS NOT GREAT ENOUGH TO KEEP THE WIRING FROM CHAFING. HAVE NOTIFIED MFG TECH SUPPORT. (K)
DURING ANNUAL INSPECTION, CRACKS WERE FOUND IN BULKHEAD FS 257.6.
LT INBOARD NACELLE DOOR DEPARTED AIRCRAFT IN FLIGHT AND PUNCTURED THE FUSELAGE.
THE AIRCRAFT WAS PARKED OUTSIDE IN A HEAVY ALLOWING WATER TO ENTER CONNECTORS AFT OF THE PILOTS CIRCUIT BREAKER PANEL. APPROX. FIFTEEN MINUTES AFTER TAKEOFF, THE LEFT AND RIGHT ESSENTIAL (A) CIRCUIT BREAKERS OPENED. THE RIGHT ESSENTIAL (A) BREAKER WAS RESET, ALLOWING THE CREW TO DECLARE AN EMERGENCY. RIGHT ESS. (A) BREAKER OPENED AGAIN ON FINAL APPROACH, AND ASSOCIATED WIRING WERE INSPECTED BY MFG MAINTENANCE, NO DEFECTS NOTED. ALL SYSTEM CHECKS SATISFACTORY. PILOTS SIDE WINDOW SEAL REPLACED.
UPON SELECTING GEAR DOWN FOR LANDING, THE PILOT COULD NOT GET A NOSE DOWN AND LOCK INDICATION. AIRCRAFT WAS LANDED AND NOSE WHEEL COLLAPSED. INVESTIGATION REVEALED THE NOSE GEAR ACTUATOR DOWNLOCK PINS WERE BROKEN WHICH ALLOWED ONE OR BOTH PINS TO VIBRATE INBOARD WHICH PREVENTED ACTUATOR SHAFT FROM RETRACTING COMPLETELY, THEREFORE, NOT ALLOWING DOWNLOCK MECHANISM TO LATCH OVER PINS. IT APPEARS PINS HAD BEEN BROKEN FOR SOME TIME AND HAD FAILED AT THE MACHINED GROOVE WHICH WAS CUT FOR ROLL PIN PROTRUSION. CESSNA SEB 9520 DATED 12-29-95 COVERS THIS SUBJECT. SUBMITTER RECOMMENDS THE INITIAL INSPECTION SHOULD BE REVISED TO 'BEFORE FURTHER FLIGHT'.