CHI91LA202
1991-06-26 · VERMILLION, South Dakota, United States · Minor · 1 aircraft · Status: Completed
Airport VMR
N541FL has since been reassigned. It is now registered to a different aircraft (DASSAULT-BREGUET FALCON 20, built 1966), which was not involved in this event.
Aircraft involved
Probable cause & findings
THE PILOT'S DECISION TO OPERATE THE AIRPLANE WITH KNOWN DEFICIENCIES AND AN IMPROPER LANDING FLARE. RELATED FACTORS ARE THE USE OF AUTOMOBILE FUEL, EXTREME TEMPERATURES AND OVERSHOOTING THE PLANNED LANDING APPROACH.
Factual narrative
AFTER A BRIEF LOCAL FLIGHT, THE PILOT TURNED BACK TOWARD THE AIRPORT TO REENTER THE TRAFFIC PATTERN. HE REPORTED THAT AS HE NEARED THE AIRPORT THERE WAS A COMPLETE LOSS OF ENGINE POWER. BECAUSE OF HIS POSITION AND ALTITUDE THE PILOT ELECTED TO MAKE A DOWNWIND LANDING ON RUNWAY 30 (HE ESTIMATED THE WINDS AS OUT OF 140 DEGREES AT 10 TO 12 KNOTS). THE PILOT REPORTED THAT HE OVERSHOT THE RUNWAY AND MADE A HARD LANDING IN A BEAN FIELD. A POST ACCIDENT ENGINE RUN UP REVEALED THAT THE ENGINE WAS CAPABLE OF NORMAL OPERATION. THE PILOT REPORTED THAT HE AND HIS INSTRUCTOR HAD ABORTED A FLIGHT EARLIER IN THE DAY OF THE ACCIDENT BECAUSE THE ENGINE FAILED DURING THE TAKEOFF ROLL. THEY ATTRIBUTED THAT ENGINE FAILURE TO VAPOR LACK. THE AIRPLANE WAS FUELED WITH AUTOMOBILE GAS, AND AT THE TIME OF THE ACCIDENT THE TEMPERATURE WAS ESTIMATED TO BE MORE THAN 90 DEGREES FAHRENHEIT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_CHI91LA202.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
- 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…