- Manufacturer (registry)
- HONEYWELL
- Model
- TPE331-2-201A
- Registry code
- 01652
- Installed in
- 4 registered aircraft
- Type
- Turbo-prop
- Power
- 715 hp
Model codes come from the FAA registry’s reference file.
On this page
Airworthiness directives that may apply · 0
ADs whose products match this engine model. Each AD’s applicability may narrow it by serial number, part number or configuration.
No ADs matched this model
Registered aircraft · 4
N193WWWin Win Aviation Inc · Wake Forest, NCN194WWWin Win Aviation Inc · Wake Forest, NCN196WWWin Win Aviation Inc · Wake Forest, NCN197WWWin Win Aviation Inc · Wake Forest, NC
Query with SQL
duckdb -csv -c "SELECT n_number, serial_number, year_manufactured, status, registrant_name, registrant_city, registrant_state
FROM 'https://openairdocs.org/data/latest/faa_aircraft_registration.parquet'
WHERE engine_model_code IN ('01652')
ORDER BY n_number"Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT n_number, serial_number, year_manufactured, status, registrant_name, registrant_city, registrant_state
FROM 'https://openairdocs.org/data/latest/faa_aircraft_registration.parquet'
WHERE engine_model_code IN ('01652')
ORDER BY n_numberRun it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
NTSB investigations
No NTSB investigations matched to aircraft with this engine modelMatched through the registry by N-number, so foreign aircraft and some older cases aren’t counted.
FAA incident reports
No reports matched to aircraft with this engine modelMatched through the registry by N-number, so foreign aircraft and some older reports aren’t counted.
Service difficulty reports · 13
SDR CA100804026Engine · flamed out(CAN) ENGINE FLAMED OUT, ACFT RETURNED TO DEPARTURE.SDR 2013FA0000081Gear · failedTORQUE SENSOR GEAR TEETH SHEARED ON CAM SET AND ALSO SHEARING OFF THE OPPOSITE GEAR ON THE HIGH SPEED PINION GEAR SHAFT.SDR CA080916008Motor · 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, CREW AND PASSENGER WERE CHECKED AT LOCAL NURSING STATION AND RELEASED. FURTHER INVESTIGATING PROBLEM,SDR CA050722005Radio · 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 MOISTURE HAD MADE ITS WAY FROM AN UNKNOWN LOCATION ABOVE THE RADIOS AND WORKED ITS WAY DOWN DURING FLIGHSDR CA030905008Wheel · 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 AIRCRAFT WAS STOPPED ON THE RUNWAY. IB WHEEL HALF PN/AH 42883, S/N 994 AND CALIPER SUSTAINED DAMAGSDR 2003FA0000648Bearing · disintegratedENGINE SHUT DOWN IN FLIGHT, AIRCRAFT LANDED IN A FIELD SUFFERED SUBSTANTIAL DAMAGE. AN ENGINE TEARDOWN WAS CONDUCTED, THE TORQUE SENSOR GEAR BEARING HAD FAILED, THE BEARING HAD COME APART BITS AND PIECES OF THE CAGE AND BALLS WERE FOUND IN THE BOTTOM OF THE GESDR AUS20010559Gasket · failed(AUS) LH ENGINE IGNITER PLUG BLANK GASKET FAILED.SDR AUS20010558Valve · faulty(AUS) START PRESSURE REGULATOR INTERNAL FAULT. EGT OVERTEMP ON START. OVERTEMP INSPECTION FOUND NO DEFECTS WITH THE ENGINE.SDR AU000558Shaft · failed(AUS) RT ENGINE TURBINE SHAFT FAILED. SECOND STAGE AND THIRD STAGETURBINE WHEELS, REAR BEARING SUPPORT AND SCAVENGE PUMP MISSING.SDR AU000130Engine · failed(AUS) ENGINE FAILED IN-FLIGHT.SDR AU990910Impeller · damaged(AUS) COMPRESSOR SECOND STAGE IMPELLER VANES (2 OFF) FRACTURED AND SEPARATED. CAUSED BY EROSION OF VANES. DAMAGE TO INTERNAL COMPONENTS.SDR 97ZZZX2003Pump · leakageINVESIGATION 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 GEARBOX. ALLIED SIGNAL SB TPE 331-72-0104 IS THE WET SPLINE MOD.SDR 97ZZZX1358Transfer Tube · fracturedPILOT 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 A 3 INCH PIECE OF THE TUBE WAS FOUND IN THE GEARBOX NEXT TO THE OIL SCAVENGE PUMP PICK-UP TUBE. T
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'TPE3312201A' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'TPE3312201A' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.