NTSB CAROL · Event
Event LAX87LA175
Registry · N271F
FAA Aircraft Registry record.
Make / Model
SCHLEICHER ASW-24
Year of manufacture
1993
Engine
NONE NONE
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19940902
ADS-B equipped
Yes — Mode-S A2AAB0
Registrant of record
MMMDAM LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE PLT STATED HE HAD FLOWN THE ACFT THE DAY PRIOR TO THE ACCIDENT ON THE LEFT FUEL TANK ONLY. NO FUEL HAD BEEN ADDED ON THE DAY OF THE ACCIDENT AND THE PLT STATED THAT THE LEFT TANK WAS THREE QUARTERS FULL AND THE RIGHT TANK WAS FULL. THE PLT POSITIONED THE FUEL SELECTOR TO THE RIGHT FUEL TANK AND JUST AFTER TAKEOFF WHILE CLIMBING THROUGH 200 FT, THE ENGINE QUIT. THE ACFT COLLIDED WITH THE TERRAIN. A FUEL LINE WAS BROKEN ON IMPACT AND THE EXACT AMOUNT OF FUEL ON BOARD IS UNKNOWN. THE CAUSE 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_LAX87LA175.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 ↗