NTSB CAROL · Event
Event NYC99LA145
Aircraft involved
Probable cause & findings
Loss of engine power for undetermined reasons.
Factual narrative
On June 16, 1999, about 1640 eastern daylight time, a homebuilt Myers 145, N42240, was substantially damage after a partial loss of power, and a forced landing to a grassy field near the Armstrong Airport, Wapakoneta, Ohio. The certificated private pilot received serious injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight conducted under 14 CFR Part 91. According to the pilot, he left his home about 1500, and traveled to the airport were the airplane was kept outside, and tied down. Before preflighting, he added 5 gallons of fuel, then did a fuel check. The check was "normal", and the pilot identified no anomalies during the preflight. The pilot boarded the airplane, and started the engine on the first attempt. He then taxied short of runway 8, and completed the run-up checks. During the run-up checks, engine rpm did not drop when individual magnetos were selected. In addition, the pilot scanned both engine and flight instruments, and noticed no discrepancies. The pilot announced his intentions on UNICOM, taxied onto the runway, advanced the throttle, and departed using 10 degree of flaps. He estimated that the airplane became airborne approximately 1/4 of the way down the 5,002 foot long runway. The pilot remained in left closed traffic, and turned crosswind, downwind, base, and final. While on final and 800 feet agl, the pilot noticed a partial loss in power. He moved the throttle, but engine rpm did not change. With insufficient power to make the runway, the pilot executed a forced landing to what he thought was a level grassy field. The airplane touched down "smoothly", and started to rollout. Before the airplane came to a stop, it encountered a creek bed approximately 5 feet deep, and 30 feet wide. The airplane entered the creek bed, and "immediately" came to a stop. The pilot secured the ignition system, removed the key, and disconnected the battery. He then egressed the creek bed via the airplane's wing, and was assisted by witnesses. In addition, the pilot stated that both the airframe, and engine had about 50 hours of operation. He added that on a previous flight, the engine experience a high oil temperature. He changed the oil from 50 weight to 30 weight, and installed a clean set of spark plugs. The purpose of the accident flight was to evaluate the effects of these changes. A review of field notes taken by the Federal Aviation Administration Inspector that was on scene, revealed no pre-impact failures for either the engine or the airframe. The following excerpts are from the Advisory Circular 20-27D, Certification and Operation of Amateur-Built Aircraft: "The amateur-built program was designed to permit person(s) to build an aircraft solely for educational or recreational purposes. The FAA has always permitted amateur builders freedom to select their own designs. The FAA does not formally approve these designs since it is not practicable to develop design standards for the multitude of unique design configurations generated by kit manufacturers and amateur builders.... Since 1983, FAA inspections of amateur-built aircraft have been limited to ensuring the use of acceptable workmanship methods, techniques, practices, and issuing operating limitations necessary to protect persons and property not involved in this activity." Before preflighting, the pilot added 5 gallons of fuel, then did a fuel check. The check was 'normal', and the pilot identified no anomalies during the preflight. The pilot boarded the airplane, and started the engine on the first attempt. He then taxied short of the runway, and completed the run-up checks. No anomalies were identified. The pilot taxied onto the runway, advanced the throttle, and departed using 10 degree of flaps. He estimated that the airplane became airborne approximately 1/4 of the way down the 5,002 foot long runway. The pilot remained in left closed traffic, and turned crosswind, downwind, base, and final. While on final and 800 feet agl, the pilot noticed a partial loss in power. He moved the throttle, but engine rpm did not change. With insufficient power to make the runway, the pilot executed a forced landing to what he thought was a level grassy field. The airplane touched down, and started to rollout, but encountered a creek bed before coming to a stop. Post accident examination of the engine revealed no pre-impact failures. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_NYC99LA145.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…
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