DCA83IA003
1982-10-28 · WILMINGTON, Delaware, United States · None · 1 aircraft · Status: Completed
Airport ILG
N213DS has since been reassigned. It is now registered to a different aircraft (DIAMOND AIRCRAFT DA 40, built 2004), which was not involved in this event.
Aircraft involved
Factual narrative
THE AIRCRAFT CRASHED SHORTLY AFTER TAKING OFF FROM THE GREATER WILMINGTON AIRPORT, WILMINGTON, DE. THE PILOT STATED THAT THE LEFT ENGINE LOST POWER AT ABOUT 100 FT AGL, JUST AS THE LANDING GEAR WAS BEING RETRACTED. HE SAID THE AUTOFEATHER WAS ARMED, BUT THE LEFT PROPELLER DID NOT AUTOMATICALLY FEATHER. HE MANUALLY FEATHERED THE LEFT PROPELLER AND CHECKED THAT THE GEAR WAS RETRACTING. THE AIRSPEED DECREASED TO ABOUT 100 KTS. HE STATED THAT HE BEGAN A DESCENT TO ACHIEVE THE BEST SINGLE ENGINE SPEED, BUT LEVEL FLIGHT COULD NOT BE SUSTAINED. REALIZING HE WAS COMMITTED TO A FORCED LANDING, HE CLIMBED TO CROSS OVER A POWER LINE, LOWERED THE GEAR AND FLAPS, THEN LANDED IN AN OPEN FIELD. DURING TOUCHDOWN, THE LEFT GEAR HIT A MOUND OF DIRT AND SEPARATED. WHILE SKIDDING TO A STOP, THE RIGHTMAIN GEAR ALSO FAILED. AN EXTENSIVE INVESTIGATION REVEALED NO REASON FOR THE ENGINE FAILURE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1982_DCA83IA003.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (engine failure). All research papers
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- NASA NTRS 2019 · Technical Memorandum (TM) A simulator investigation of engine failure compensation for powered-lift STOL aircraft
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- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum) Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
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