NTSB CAROL · Event
Event MIA03LA049
Aircraft involved
Probable cause & findings
A loss of engine power for undetermined reasons.
Factual narrative
On January 28, 2003, about 1736 eastern standard time, a Mooney M20K, N231NT, operated by a private individual as a Title 14 CFR Part 91 personal flight impacted with the terrain during a forced landing at the Grand Strand Airport, Myrtle Beach, South Carolina. Visual meteorological conditions prevailed. No flight plan was filed. The airplane was substantially damaged. The commercial-rated pilot and one passenger reported minor injuries. The flight was originating at the time of the accident and was en route to Greenville, South Carolina. The flight had departed on runway 23 and the landing gear was retracted. The pilot reported a "loud pop" followed by a loss of engine power. The pilot lowered the landing gear in an attempt to land on the remaining runway. The aircraft came to a stop about 250 feet past the end of the runway and 200 feet left of the centerline. According to the FAA inspector, an examination of the aircraft's engine revealed, that the number 3 cylinder read 3 to 10 psi over 80 psi when a cold compression differential check was performed to the engine. According to the FAA inspector "this was not a cause for the engine failure." In addition, he stated that the fuel, along with the fuel systems, was examined and no abnormalities were found. According to the FAA inspector's statement the pilot stated that part of her preflight was to select the right tank when her husband is on board. The fuel selector was found in the "off" position at the time of the FAA accident investigation. Someone from the fix base operator stated to the FAA, that he assisted the occupants out of the aircraft and turned off all switches. He remembered the auxiliary fuel pump was "on" and the fuel selector was pointing to a position between the left fuel tank and the off position. When asked to put the statement in writing he would not corroborate. The FAA asked the pilot if she attempted to turn the fuel selector to the off position at the time of the accident? The pilot could not remember. The pilot reported a "loud pop" followed by a loss of engine power during takeoff climb and attempted to land on the remaining runway. The airplane came to a stop about 250 feet past the end of the runway and 200 feet left of the centerline. Examination of the airplane's engine revealed no discrepancies except for a low reading in the number 3 cylinder, during a cold compression check. The fuel, along with the fuel systems, was examined and no abnormalities were found. Someone from the fix base operator had assisted the occupants out of the aircraft and turned off all switches. He remembered the auxiliary fuel pump was on and the fuel selector was pointing to a position between the left fuel tank and the off position. The pilot could not remember if she had turned the fuel selector to the off position at the time of the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_MIA03LA049.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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