LAX88LA123
1988-03-10 · ORACLE, Arizona, United States · None · 1 aircraft · Status: Completed
Aircraft involved
Probable cause & findings
ENGINE FAILURE FOR UNDETERMINED REASONS.
Factual narrative
THE PILOT SAID THAT HE HAD COMPLETED A CATTLE SURVEY AND WAS RETURNING TO THE RANCH AIRSTRIP WHEN HE ADDED POWER TO CLIMB BACK TO PATTERN ALTITUDE. THE PILOT STATED THAT AS HE ADDED THROTTLE HE HEARD A LOUD POP AND THE ENGINE BEGAN TO LOSE POWER. THE PILOT SAID THAT HE TURNED ON THE BOOST PUMP BUT IT HAD NO EFFECT ON THE ENGINE POWER OUTPUT. THE PILOT NOTED THAT HE PUMPED THE THROTTLE AND WAS ABLE TO RESTORE LIMITED POWER; HOWEVER, THE POWER LEVEL WAS NOT ENOUGH TO MAINTAIN FLIGHT. THE AIRCRAFT SETTLED ONTO THE GROUND, TRAVELING UPSLOPE ON A HILL, AND HIT SEVERAL SMALL TREES WHICH SHEARED OFF THE LEFT LANDING GEAR. A POST CRASH FIRE CONSUMED THE AIRCRAFT. EXAMINATION OF THE AIRCRAFT REVEALED THAT ALL ENGINE ACCESSORIES WERE DESTROYED AND COULD NOT BE FUNCTIONALLY TESTED. NO INTERNAL ABNORMALITY WAS NOTED ON THE ENGINE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1988_LAX88LA123.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…