NTSB CAROL · Event
Event LAX85FA019
Aircraft involved
Factual narrative
THE ACFT WAS ON A 3.5 MILE FINAL APPROACH TO TORRENCE ARPT WHEN THE PILOT EXPERIENCED AN ENGINE FAILURE. THE PLT LANDED THE ACFT THE LOS ANGELES, WEST BASIN HARBOR. EXAMINATION OF THE ENGINE AND ASSOCIATED FUEL LINES AFTER THE ACCIDENT REVEALED NO EVIDENCE OF A MALFUNCTION OR FAILURE. THE ENG DRIVEN FUEL PUMP WAS TESTED AND FOUND TO BE DEVELOPING LESS THAN THE MANUFACTURER'S SPECIFIED PRESSURE. AN EXAMINATION OF THE FUEL PUMP REVEALED A BRITTLE AND CRACKED RUBBER DIAPHRAM. THE ENGINE HAD A TOTAL TIME OF 2,932 HOURS, 982 HOURS SMOH AND THE ORIGINAL SAFETY WIRES WERE STILL IN USE ON THE FUEL PUMP. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1984_LAX85FA019.txt.
Findings + structured fields enriched from FAA avall.mdb.
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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.
- NASA NTRS 2020 · Technical Memorandum (TM)
Evaluation Issues for a Flight Deck Interface; CAST SE-210 Output 2: Report 4 of 6
This report is part of a series of reports that addresses flight deck design and evaluation, written as a response to loss of control accidents.
- 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.
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