NTSB CAROL · Event
Event MIA94LA129
Aircraft involved
Probable cause & findings
THE FAILURE OF THE PILOT IN COMMAND TO USE THE CHECKLIST BEFORE TAKEOFF. THE ENGINE FAILED DUE TO THE FUEL SELECTOR BEING IN THE OFF POSITION. CONTRIBUTING TO THE ACCIDENT WAS THE UNSUITABLE TERRAIN FOR A FORCED LANDING.
Factual narrative
On May 1, 1994, about 1535 eastern daylight time, N323ET, a homebuilt Osprey airplane crashed at Sanford Airport, Sanford, Florida, while on a 14 CFR Part 91 local flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The airplane was substantially damaged and the pilot received serious injuries. The flight had originated about 30 minutes earlier. The pilot experienced an engine failure on takeoff and turned to return to the airport. The airplane crashed into a ditch, and broke in half. Examination of the cockpit after the accident by FAA personnel revealed the fuel selector was in the off position. THE PILOT STATED THE ENGINE LOST POWER ON TAKEOFF AND HE TURNED BACK TO THE AIRPORT BUT COULD NOT MAKE IT. HE CRASHED INTO A DITCH. EXAMINATION OF THE COCKPIT REVEALED THE FUEL SELECTOR WAS IN THE OFF POSITION. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_MIA94LA129.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 (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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…
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