NYC92FA050
1991-12-25 · WILMINGTON, Ohio, United States · Fatal · 1 aircraft · Status: Completed
Airport OH77
Current FAA registration · N236JS
- Make / Model
- BEECH F90
- Year of manufacture
- 1980 · 11 years old at event
- Engine
- P&W CANADA PT6A-60A (1050 hp)
- Seats / Engines
- 10 seats · 2 engines
- Last airworthiness date
- 19801103
- ADS-B equipped
- Yes — Mode-S A21FA3
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE FAILURE OF THE PILOTS TO MAINTAIN ADEQUATE TERRAIN CLEARANCE. FACTORS WHICH CONTRIBUTED TO THE ACCIDENT WERE: THE NIGHT CONDITIONS, REDUCED VISIBILITY DUE TO FOG, AND THE LIKELIHOOD THAT THE PILOTS DIVERTED THEIR ATTENTION TO THE OPERATION OF THE LORAN EQUIPMENT.
Factual narrative
THE ACFT WAS ON A LOCAL NIGHT FLIGHT TO SEE THE XMAS LIGHTS OF DAYTON FROM THE AIR. A PAX STATED THAT WHEN SHE THOUGHT THEY WERE GOING TO LAND THE ACFT HIT TREES. THERE WAS NO UNUSUAL ENGINE SOUND, OR ANYTHING DIFFERENT FROM OTHER FLIGHTS. THE ACCIDENT OCCURED ABOUT 1 MI FROM THE AIRPORT. THE LEFT SEAT PILOT WAS NOT INSTRUMENT-RATED. THE RIGHT SEAT PILOT WAS THE ACFT OWNER, AND WAS INSTRUMENT RATED. THE PILOT OPERATING THE CONTROLS AT THE TIME OF THE ACCIDENT WAS NOT DETERMINED. THERE ARE NO FAA-APPROVED APPROACHES FOR THE ARPT; HOWEVER, THE OWNER HAD DESIGNED A LORAN-C APPROACH AND TWO R-NAV APPROACHES FOR PERSONAL USE. THE ACTIVE WAYPOINT FOUND IN THE ACFT'S LORAN UNIT COINCIDED WITH THE ARPT. THE OWNER WAS DESCRIBED AS A PERSON WHO ' WAS PROUD OF, AND WOULD BE EAGER TO SHOW OTHER PILOTS FLYING THE AIRPLANE, THE PROCEDURES FOR USE OF THE EQUIPMENT INSTALLED.' Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_NYC92FA050.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 (stall). All research papers
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- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
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- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…