N901TA

No registry detail on file · not in current registry

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.

4 reports on file, 1995-12-20 – 2006-05-07.

SMOKE/FUMES/ODORS/SPARKS · 2006-05-07 Matched by certificate designator
ATA 2120

Part: ODOR — DETECTED (CABIN) · airframe 8,662 hrs · 4,996 cycles

KAGS - FOLLOWING TAKEOFF THE CABIN FILLED WITH A BURNING SMELL. THE AIRCRAFT WAS RETURNED TO KAGS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT LOCATE ANY BURNING OR BURNING SMELL IN THE CABIN AREA WHEN INVESTIGATING THE DISCREPANCY. THE BURINING SMELL WAS REPORTED TO HAVE DISSIPATED DURING DESCENT INTO KAGS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR DJFA2006242
OTHER · 2006-03-25 Matched by certificate designator
ATA 2131

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 8,571 hrs · 4,936 cycles

DURING CLIMBOUT THE CREW NOTICED THAT THE CABIN ALTITUDE WAS APPROXIMATELY 10,000 FT. THE AIRCRAFT WAS LEVELED OFF AT 16,000 FT AND THE CREW DONNED THEIR OXYGEN MASKS. PASSENGER OXYGEN MASKS RELEASED WHILE ATTEMPTS WERE MADE TO ISOLATE THE PROBLEM. MANUAL PRESSURIZATION CONTROL WAS USED TO MAINTAIN CABIN PRESSURIZATION WHILE THE AIRCRAFT WAS DIVERTED TO KAPA. MAINTENANCE REPLACED THE PRESSURIZATION CONTROLLER. GROUND OPERATIONAL CHECKS OF THE PRESSURIZATION SYSTEM WERE SATISFACTORY, AND A SUCCESSFUL CHECK FLIGHT WAS PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR DJFA2006223
VIBRATION/BUFFET; PARTIAL RPM/PWR LOSS · 1995-12-23 Matched by certificate designator
ATA 7314

Part: PUMP — FAILED (AFT ENGINE)

DURING SCHEDULED FLIGHT AFTER TAKEOFF CLIMB AT 700 MSL, THE REAR ENGINE STARTED DECREASING RPM'S, AND INCREASING MANIFOLD ON REAR ENGINE. VIBRATION FELT ON AIRCRAFT RETURN AND LANDING WITHOUT ANY FURTHER INCIDENT. REAR ENGINE RUN-UP AND FOUND DEFECTIVE MECHANICAL FUEL PUMP. REPLACED BY NEW ONE. ENGINE RUN-UP AND FOUND AIRWORTHY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR 96ZZZX1101
PARTIAL RPM/PWR LOSS · 1995-12-20 Matched by certificate designator
ATA 6122

Part: GOVERNOR — SHAFT FAILED (AFT ENGINE PROP)

DURING TAKEOFF, REAR ENGINE LOST POWER AND PROPELLER FEATHER. REAR GOVERNOR REMOVED AND FOUND BROKEN SHAFT. GOVERNOR REPLACED AND AIRCRAFT RETURNED TO SERVICE.

Source: SDR 96ZZZX1102