BFO94LA127
1994-08-06 · EDGEWATER, Maryland, United States · Serious · 1 aircraft · Status: Completed
Airport ANP
Aircraft involved
Probable cause & findings
The pilot's inadequate preflight inspection which failed to detect water contaminated fuel which resulted in fuel starvation.
Factual narrative
On August 6, 1994, at 1640 hours, a Piper PA-28R-200, N5242T, a local personal flight, had a loss of engine power and was forced landed shortly after takeoff from Lee Airport, Edgewater, Maryland. Visual meteorological conditions existed. The pilot and passenger were seriously injured. The airplane was destroyed. The flight was conducted under 14 CFR Part 91. The pilot reported: "About 15 seconds after takeoff, it felt like engine powered back to idle. I don't remember hearing engine noises, like bangs or pops. Just after engine failure, leveled aircaft, to maintain airspeed of 90 knots. Switched from left to right fuel tank, propeller still turning. I put my hand on electric fuel pump switch to check position, while trying to find a place to land. "Unable to restart engine, I made emergency landing in trees. Just prior to hitting trees, tried to bank left to avoid tree trunks, and pushed hard left rudder. Plane went nose down in small group of trees." According to the pilot, the airplane crashed 1000 feet off end of runway. The FAA examination of the airplane disclosed evidence of water at the fuel servo finger screen and that the right magneto was firing on two of its four contacts. Shortly after takeoff, the engine lost power and the pilot forced landed into trees about 1000 feet beyond the runway. The pilot stated that about 15 seconds after lift off, the engine powered back to idle. He reported the loss of power was not preceded with a 'bang' or 'pop' sound. The examination of the engine revealed evidence of water contaminated fuel. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_BFO94LA127.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 (fuel starvation, engine failure). All research papers
- arXiv 2022 · arXiv preprint Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM) A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum) Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…