N145GT

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
CONQUEST AIR, INC. (Q9UA)Operator2019-02-08 – 2019-02-08Operator named in NTSB report

Accident & incident history

Acc · 2019-02-08 Operator named in NTSB report
Convair C131 Fatal injury Part 135CONQUEST AIR, INC.
Source: NTSB case ERA19LA096

Maintenance disclosures

O · 2019-03-08 Matched by certificate designator
ATA 6122

FLIGHT CREW INABILITY TO ADJUST RPM INFLIGHT VIA PROPELLER SPEED CONTROL. PROPELLER SPEED CONTROL COULD BE ADJUSTED ON THE GROUND DURING RUN UP.

Source: SDR Q9UA2019FA0000058 · FAA SDRS
F · 2016-06-20 Matched by certificate designator
ATA 6122

NR 1 PROPELLER GOVERNOR WAS SLOW TO RESPOND WITH TOGGLE SWITCH, AFTER TAKEOFF.

Source: SDR Q9UA2016062303 · FAA SDRS
K R · 2014-12-19 Matched by certificate designator
ATA 8530

DURING CLIMB THE NUMBER 2 ENGINE BEGAN MAKING A POPPING NOISE AND THE MANIFOLD AND BMEP READINGS WERE WIDLY FLUCTUATING. THE CREW NOTICED A SLIGHT DROP IN THE ENGINE OIL LEVEL ON THE NUMBER TWO ENGINE. THE CREW ELECTED TO PREFORM A PRECAUTIONARY ENGINE SHUT DOWN ON THE NUMBER TWO ENGINE. UPON INSPECTION OF THE ENGINE, THE MAINTENANCE CREW DICOVERED THE NUMBER ONE CYLINDER WAS CRACKED. THIS CAUSED A SLIGHT LOSS OF POWER AND SLIGHT LOSS OF ENGINE OIL.

Source: SDR Q9UA2014122300002 · FAA SDRS
O · 2014-10-03 Matched by certificate designator
ATA 6122

PROPELLER GOVERNOR WOULD NOT DECREASE BELOW 2500 RPM. AFTER REACHING CRUISE ALTITUDE, CREW WAS UNABLE TO DECREASE THE ENGINE RPM BELOW 2500. SHORTLY THEREAFTER THE RPM BEGAN TO GRADUALLY INCREASE ON ITS OWN. ENGINE WAS FEATHERED TO PREVENT PROPELLER OVERSPEED. THE NR 1 PROPELLER GOVERNOR FAILED TO CONTROL. WE WILL SEND THE PROPELLER GOVERNOR TO O/H AND REVIEW THE TEARDOWN REPORT. IF ANY ABNORMALLY IS REPORTED WE WILL FORWARD THIS INFORMATION TO FAA.

Source: SDR Q9U201410170001 · FAA SDRS
F · 2014-10-02 Matched by certificate designator
ATA 6122

PROPELLER GOVERNOR WOULD NOT DECREASE BELOW 2500 RPM. AFTER REACHING CRUISE ALTITUDE, THE CREW WAS UNABLE TO DECREASE THE ENGINE RPM BELOW 2500 RPM. SHORTLY THEREAFTER THE RPM BEGAN TO INCREASE ON ITS OWN. ENGINE WAS FEATHERED TO PREVENT PROPELLER OVERSPEED. THE NR 1 PROPELLER GOVERNOR FAILED TO CONTROL, WE WILL SEND THE PROPELLER GOVERNOR TO O/H AND REVIEW THE TEAR DOWN REPORT. IF ANY ABNORMALITY IS REPORTED WE WILL FORWARD THIS INFORMATION TO THE FAA.

Source: SDR Q9UA20141002001 · FAA SDRS
O · 2001-01-22 Unresolved
ATA 8520

AFTER TAKEOFF, CLIMBING THROUGH 2,200 FT CREW NOTICED OIL TEMPERATURE RISING AND OIL PRESSURE DECREASING. ENGINE SHUTDOWN/FEATHERED, RETURNED TO AIRPORT. INSPECTION REVEALED BEARING MATERIAL IN OIL SCREENS. ENGINE REMOVED FROM SERVICE FOR REPAIRS.

Source: SDR 20010305CW003 · FAA SDRS