# Honeywell TPE331-2-201A

- Type: Engine model (FAA registry)
- Registry code: 01652
- Manufacturer (registry): HONEYWELL
- Model: TPE331-2-201A
- Engine type: Turbo-prop
- Power: 715 hp
- Installed in: 4 registered aircraft
- Page: https://openairdocs.org/engine/honeywell-tpe331-2-201a

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft (4)

- [N193WW](https://openairdocs.org/aircraft/N193WW): [Win Win Aviation Inc](https://openairdocs.org/faa-owner/WIN%20WIN%20AVIATION%20INC), [Wake Forest, NC](https://openairdocs.org/faa-place/NC/Wake%20Forest), built 1978, S/N SH1957
- [N194WW](https://openairdocs.org/aircraft/N194WW): [Win Win Aviation Inc](https://openairdocs.org/faa-owner/WIN%20WIN%20AVIATION%20INC), [Wake Forest, NC](https://openairdocs.org/faa-place/NC/Wake%20Forest), built 1969, S/N SH1969
- [N196WW](https://openairdocs.org/aircraft/N196WW): [Win Win Aviation Inc](https://openairdocs.org/faa-owner/WIN%20WIN%20AVIATION%20INC), [Wake Forest, NC](https://openairdocs.org/faa-place/NC/Wake%20Forest), built 1977, S/N SH1965
- [N197WW](https://openairdocs.org/aircraft/N197WW): [Win Win Aviation Inc](https://openairdocs.org/faa-owner/WIN%20WIN%20AVIATION%20INC), [Wake Forest, NC](https://openairdocs.org/faa-place/NC/Wake%20Forest), built 1973, S/N SH1908

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (13)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA100804026](https://openairdocs.org/sdr/CA100804026), Aug 1, 2010: ENGINE. FLAMED OUT. (CAN) ENGINE FLAMED OUT, ACFT RETURNED TO DEPARTURE.
- [SDR 2013FA0000081](https://openairdocs.org/sdr/2013FA0000081), Jun 12, 2009: GEAR. FAILED. TORQUE SENSOR GEAR TEETH SHEARED ON CAM SET AND ALSO SHEARING OFF THE OPPOSITE GEAR ON THE HIGH SPEED PINION GEAR SHAFT.
- [SDR CA080916008](https://openairdocs.org/sdr/CA080916008), Sep 13, 2008: MOTOR. MALFUNCTIONED. (CAN) SKYVAN EN ROUTE WITH 2 CREW ,1 PASSENGER ON BOARD ADVISED ARCTIC RADIO THEY HAD SMOKE IN COCKPIT, CREW REQUESTED EMERGENCY VEHICLES, ACFT LANDED SAFELY, C
- [SDR CA050722005](https://openairdocs.org/sdr/CA050722005), Jul 19, 2005: RADIO. INOPERATIVE. (CAN) RETURNED TO BASE WITH NO WORKING RADIOS. IT WAS RETURNING FROM WERE IT HAD BEEN RAINING HEAVILY WHILE THEY WERE ON THE GROUND. IT WAS FOUND THAT SOME MOIS
- [SDR CA030905008](https://openairdocs.org/sdr/CA030905008), Sep 2, 2003: WHEEL. DAMAGED. (CAN) ON TAKEOFF THE CREW HEARD A LOUD NOISE UPON SETTING MAX POWER. AN IMMEDIATE REJECTED TAKEOFF WAS CARRIED OUT, DIRECTIONAL CONTROL WAS MAINTAINED, AND THE 
- [SDR 2003FA0000648](https://openairdocs.org/sdr/2003FA0000648), Jun 13, 2003: BEARING. DISINTEGRATED. ENGINE SHUT DOWN IN FLIGHT, AIRCRAFT LANDED IN A FIELD SUFFERED SUBSTANTIAL DAMAGE. AN ENGINE TEARDOWN WAS CONDUCTED, THE TORQUE SENSOR GEAR BEARING HAD FAILED,
- [SDR AUS20010559](https://openairdocs.org/sdr/AUS20010559), May 24, 2001: GASKET. FAILED. (AUS) LH ENGINE IGNITER PLUG BLANK GASKET FAILED.
- [SDR AUS20010558](https://openairdocs.org/sdr/AUS20010558), May 19, 2001: VALVE. FAULTY. (AUS) START PRESSURE REGULATOR INTERNAL FAULT. EGT OVERTEMP ON START. OVERTEMP INSPECTION FOUND NO DEFECTS WITH THE ENGINE.
- [SDR AU000558](https://openairdocs.org/sdr/AU000558), Jul 1, 2000: SHAFT. FAILED. (AUS) RT ENGINE TURBINE SHAFT FAILED. SECOND STAGE AND THIRD STAGETURBINE WHEELS, REAR BEARING SUPPORT AND SCAVENGE PUMP MISSING.
- [SDR AU000130](https://openairdocs.org/sdr/AU000130), Jan 9, 2000: ENGINE. FAILED. (AUS) ENGINE FAILED IN-FLIGHT.
- [SDR AU990910](https://openairdocs.org/sdr/AU990910), Sep 6, 1999: IMPELLER. DAMAGED. (AUS) COMPRESSOR SECOND STAGE IMPELLER VANES (2 OFF) FRACTURED AND SEPARATED. CAUSED BY EROSION OF VANES. DAMAGE TO INTERNAL COMPONENTS.
- [SDR 97ZZZX2003](https://openairdocs.org/sdr/97ZZZX2003), Apr 9, 1997: PUMP. LEAKAGE. INVESIGATION FOR EXCESS OIL USAGE, FOUND THE OIL WAS ENTERING THE FUEL SYS VIA THE OIL WET SPLINE MOD TO THE DRIVESHAFT THAT DRIVES THE FUEL PUMP ON THE ENG GEA
- [SDR 97ZZZX1358](https://openairdocs.org/sdr/97ZZZX1358), Mar 10, 1997: TRANSFER TUBE. FRACTURED. PILOT REPORTED A LOSS OF POWER AND GEARBOX NOISE AND SHUT THE ENGINE DOWN. AFTER DISASSEMBLY OF THE GEARBOX, DISCOVERED THE OIL TUBE 3101605-1 HAD FRACTURED AND

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