# N932H: 1945 Douglas DC3C - Status: Valid registration - Airframe: [Douglas DC3C](https://openairdocs.org/model/douglas-dc3c) (registry code 3021457, 32 seats) - Engine: [Pratt & Whitney Canada PT6A-67R](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67r) (registry code 52208) - Data sheets: [TCDS E26NE](https://openairdocs.org/tcds/E26NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: 34368 - Year built: 1945 - Type: Fixed wing multi engine - Engine type: 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 - Registered owner: [Airborne Support Inc](https://openairdocs.org/faa-owner/AIRBORNE%20SUPPORT%20INC) - Location: [Houma, LA](https://openairdocs.org/faa-place/LA/Houma) - Owner type: Corporation - Owner's area on the map: 29.5067° N, 90.7008° W: Placed by OpenAirDocs at the center of ZIP code 70363, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=932H - Page: https://openairdocs.org/aircraft/N932H From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 2 in force ### Matched by airframe (Douglas DC3C) None in force. ### Matched by engine (Pratt & Whitney Canada PT6A-67R) - [AD 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024 - [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997 ## Information bulletins (advisory) (1 in force) - [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003 ## NTSB investigations None matched to N932H. ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20201026015469I](https://openairdocs.org/incident/20201026015469I), Oct 26, 2020: Douglas DC3C (N932H), Houma, LA, No damage. At 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… - [Incident 20000608018169I](https://openairdocs.org/incident/20000608018169I), Jun 8, 2000: Doug DC3C (N932H), 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… ## Service difficulty reports (10) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 092703](https://openairdocs.org/sdr/092703), Sep 29, 2003: ENGINE. FAILED. AT 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. SUSPE - [SDR 20010423CW002](https://openairdocs.org/sdr/20010423CW002), Mar 29, 2001: OIL COOLER. FAILED. SHORTLY AFTER DEPARTURE, STARTED TO LOOSE OIL PRESSURE ON RIGHT ENGINE. SHUT DOWN ENGINE AND RETURNED TO AIRPORT. SUSPECT HIGH PRESSURE, COLD OIL MAY HAVE CAUSE - [SDR 20010208CW002](https://openairdocs.org/sdr/20010208CW002), Dec 8, 2000: ENGINE. LEAKING. IN 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 20000717SH020](https://openairdocs.org/sdr/20000717SH020), Jun 9, 2000: ENGINE. FAILED. AIRCRAFT 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 - [SDR 99ZZZX4686](https://openairdocs.org/sdr/99ZZZX4686), Nov 26, 1999: ENGINE. MALFUNCTIONED. EN ROUTE FROM MWO/BAK - RIGHT ENGINE OIL TEMP AND OIL PRESSURE WENT TO RED LINE. RETURNED TO GWO. SUSPECT MASTER ROD HEAVILY FAILURE. - [SDR 99ZZZX3612](https://openairdocs.org/sdr/99ZZZX3612), Jul 17, 1999: BEARING. FAILED. AFTER 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 - [SDR 98ZZZX196](https://openairdocs.org/sdr/98ZZZX196), Jan 7, 1998: CYLINDER. CRACKED. ENGINE STARTED RUNNING ROUGH. FOUND NR 7 CYLINDER EXHAUST PORT CRACKED ON CYLINDER HEAD. - [SDR 97ZZZX3832](https://openairdocs.org/sdr/97ZZZX3832), Aug 19, 1997: CASTLE NUT. FAILED. AIRCRAFT 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 - [SDR 97ZZZX1844](https://openairdocs.org/sdr/97ZZZX1844), Apr 10, 1997: ENGINE. FAILED. AIRCRAFT 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 OI - [SDR 97ZZZX1846](https://openairdocs.org/sdr/97ZZZX1846), Apr 2, 1997: ROCKER SHAFT. FAILED. ON 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 CYLIND ## STCs that may be installed (OpenAirDocs) (3) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the engine (Pratt & Whitney Canada PT6A-67R) - [STC SE8652SW](https://openairdocs.org/stc/SE8652SW): Installation of a flexible hose from the Propeller Primary Governor to the Fuel Control Unit. Air Tractor Inc - [STC SE00022EN](https://openairdocs.org/stc/SE00022EN): Installation of Oil Tank Filler Neck Check Valve. Helicopter Support Inc Services Div - [STC SE659NE](https://openairdocs.org/stc/SE659NE): Installation of oil tank filler neck check valve, P/N TSA-76A. Aviation Components Support ## Related - Other Douglas DC3C aircraft: https://openairdocs.org/model/douglas-dc3c/aircraft.md - The Pratt & Whitney Canada PT6A-67R engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67r.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.