- Registered owner
- Airborne Support Inc
- Location
- Houma, LA
- Owner type
- Corporation
- Serial number
- 34368
- Year built
- 1945
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Experimental, research and development
- Airworthiness date
- February 15, 2010
- Certificate issued
- July 22, 2009
- Expires
- October 31, 2027
- Mode S code
- ACEDC6
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 2
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1997 | 1 |
|---|---|
| 2024 | 1 |
Engine · Pratt & Whitney Canada PT6A-67R
AD 2024-04-51Turbine SectionEmergency ADAD 97-04-12Compressor Bleed-off ValveInformation bulletins that may apply · 1
Advisory, not mandatory.
Engine · Pratt & Whitney Canada PT6A-67R
SAIB CE-03-24NTSB investigations
No NTSB investigations matched to N932HMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Douglas DC3C aircraft
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20201026015469ITakeoff: Departure Roll · Houma, LAAt approximately 1417 z on 26 oct 2020, aircraft lined up for departure on runway 18 at khum. Winds were reported to be 110 at 10 immediately before aircraft took the runway. As the aircraft rolled along the runway, the aircraft weathervaned and moved to the…Incident 20000608018169INormal Cruise · Erie, PA(-23)On June 8, 2000, at 0935, a DC-3, registered to miami valley avaition (vlla) as N932H, landed at Erie International Airport (eri) with the number 2 engine shut down due to the loss of engine oil pressure. Trouble shooting by maintenance revealed metal…
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 092703Engine · failedAT CRUISE POWER FOR 3 HOURS ENROUTE FROM LRD-GMU, RT ENGINE STARTED RUNNING ROUGH AND BLOWING OIL OUT OF THE CRANKCASE BREATHER. AIRCRAFT DIVERTED TO LFT. SUSPECT CYLINDER AND SCAVENGE PUMP FAILURE.SDR 20010423CW002Oil Cooler · failedSHORTLY AFTER DEPARTURE, STARTED TO LOOSE OIL PRESSURE ON RIGHT ENGINE. SHUT DOWN ENGINE AND RETURNED TO AIRPORT. SUSPECT HIGH PRESSURE, COLD OIL MAY HAVE CAUSED FAILURE OF THE COOLER.SDR 20010208CW002Engine · leakingIN ROUTE FROM RYV TO RDV, RT ENGINE STARTED LEAKING OIL OUT OF THE CRANKCASE BREATHER. DIVERTED TO FWA. SUSPECT SCAVAGE PUMP NOT OPERATED CORRECTLY.SDR 20000717SH020Engine · failedAIRCRAFT WAS IN CRUISE. RIGHT ENGINE STARTED RUNNING ROUGH AND HAD A MINOR LOSS IN POWER. POWER WAS DECREASED AND OIL PRESSURE DROPPED TO MINIMUM REDLINE. METAL WAS FOUND IN OIL SCREEN. POSSIBLE CAM RING FAILURE. (X)SDR 99ZZZX4686Engine · malfunctionedEN ROUTE FROM MWO/BAK - RIGHT ENGINE OIL TEMP AND OIL PRESSURE WENT TO RED LINE. RETURNED TO GWO. SUSPECT MASTER ROD HEAVILY FAILURE.SDR 99ZZZX3612Bearing · failedAFTER TAKEOFF ON DEPARTURE FROM OMA, LEFT OIL TEMPERATURE INCREASED TO RED LINE AND OIL PRESSURE DROPPED TO RED LINE. AIRCRAFT RETURNED TO OMA. METAL WAS FOUND IN OIL SCREEN. SUSPECT MASTER ROD BEARING FAILURE.SDR 98ZZZX196Cylinder · crackedENGINE STARTED RUNNING ROUGH. FOUND NR 7 CYLINDER EXHAUST PORT CRACKED ON CYLINDER HEAD.SDR 97ZZZX3832Castle Nut · failedAIRCRAFT WAS AT CRUISE POWER. LEFT ENGINE WENT TO IDLE POWER. FEATHERED LEFT ENGINE AND LANDED. FOUND THROTTLE CONTROL ARM OFF OF CARBURETOR. FOUND PARTS OF THE CRACKED AN 310-4 CASTLE NUT.SDR 97ZZZX1844Engine · failedAIRCRAFT HAD JUST LEVELED OFF AND WAS AT CRUISE POWER. ENGINE STARTED TO LOSE OIL PRESSURE. ENGINE WAS SHUT DOWN AND LANDED AT JHW. FOUND METAL IN OIL AND IN OIL SCREEN. SUSPECT INTERNAL FAILURE.SDR 97ZZZX1846Rocker Shaft · failedON APPROACH, AIRCRAFT'S RIGHT ENGINE STARTED RUNNING ROUGH. FOUND NR 6 CYLINDER EXHAUST ROCKER SHAFT HAD CRACKED IN HALF CAUSING SHAFT TO FALL OUT OF THE CYLINDER. THIS CAUSED THE EXHAUST VALVE NOT TO OPEN.
STCs that may be installed · 3
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.