LAX87DVA07
1987-04-29 · TULARE, California, United States · None · 1 aircraft · Status: Completed
Airport TLR
Aircraft involved
Factual narrative
DURING A CLIMBING 180 DEGREE TURN TO THE LEFT, THE ENGINE LOST POWER. THE PILOT ATTEMPTED TO LAND IN A NEARBY FIELD THAT HAD JUST BEEN PLOWED. WITH INSUFFICIENT ALTITUDE TO TURN FAR ENOUGH TO LINE THE AIRCRAFT UP WITH THE ROWS, THE PILOT TOUCHED DOWN AT A '20 DEGREE ANGLE' WITH THE ROWS. THE MAIN GEAR STUCK INTO THE GROUND AND THE PLANE FLIPPED OVER ON ITS BACK. THE SOURCE OF THE ENGINE FAILURE WAS NOT DETERMINED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1987_LAX87DVA07.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
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Related research
Matched on aircraft type or causal vocabulary (engine failure). All research papers
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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…