NTSB CAROL · Event
Event LAX90LA338
Registry · N9161D
FAA Aircraft Registry record.
Make / Model
MOONEY M20M
Year of manufacture
1990 · 0 years old at event
Engine
LYCOMING TI0-540 SER (310 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19900917
ADS-B equipped
Yes — Mode-S ACAF74
Registrant of record
SCHLESINGER WARREN
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
ENGINE FAILURE DUE TO A RUPTURED FUEL PUMP DIAPHRAGM. A FACTOR IN THE ACCIDENT WAS THE UNSUITABLE NATURE OF THE TERRAIN TO MAKE A FORCED LANDING.
Factual narrative
THE PILOT OF A MOONEY M-20-M EXPERIENCED ENGINE FAILURE WHILE APPROACHING THE AIRPORT FOR LANDING. THE PILOT STATED HE HAD JUST SWITCHED TO THE FULLEST TANK AND ACTIVATED THE BOOST PUMP. AT THAT POINT THE ENGINE QUIT. EXAMINATION OF THE 18 HOURS SINCE NEW AIRCRAFT FUEL SYSTEM, DISCOVERED A RUPTURED FUEL PUMP DIAPHRAGM. AIRWORTHINESS DIRECTIVE 91-08-07 AND SEVERAL TEXTRON/LYCOMING SERVICE BULLETINS ADDRESS THIS EVENTUALITY. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1990_LAX90LA338.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 ↗