NTSB CAROL · Event
Event LAX92LA309
Aircraft involved
Probable cause & findings
AN ON GROUND COLLISION WITH TERRAIN SUBSEQUENT TO AN ENGINE FAILURE FOR UNDETERMINED REASONS.
Factual narrative
THE PILOT REPORTED THAT WHILE ON THE DOWNWIND LEG THE AIRPLANE SUSTAINED A TOTAL LOSS OF POWER. THE PILOT'S ATTEMPTS TO RESTART THE ENGINE WERE UNSUCCESSFUL AND HE EXECUTED AN EMERGENCY LANDING TO THE RUNWAY. IN ORDER TO NEGOTIATE THE AIRPORT THE PILOT ANGLED TOWARDS THE RUNWAY. AFTER TOUCH DOWN THE PILOT WAS UNABLE TO ALIGN THE AIRPLANE WITH THE RUNWAY AND EXITED THE RUNWAY AND COLLIDED WITH THE VISUAL APPROACH SLOPE INDICATOR LIGHTS BEFORE STOPPING. THE OPERATOR OPERATED THE ENGINE, SHORTLY AFTER THE ACCIDENT BUT COULD NOT RECALL IF THE FUEL SELECTOR VALVE WAS PROPERLY SELECTED TO A FUEL TANK. THE ACCIDENT WAS INITIALLY REPORTED AS AN INCIDENT. FURTHER EXAMINATION OF THE ENGINE DISCLOSED NO EVIDENCE OF ANY PREEXISTING MALFUNCTIONS OR FAILURES AND THE CAUSE OF THE LOSS OF POWER COULD NOT BE DETERMINED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1992_LAX92LA309.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…
Browse the full corpus — academia portal ↗