NTSB CAROL · Event
Event LAX91LA275
Aircraft involved
Probable cause & findings
FUEL EXHAUSTION DUE TO THE FAILURE OF THE PILOT TO ENSURE THAT AN ADEQUATE FUEL SUPPLY WAS ON BOARD THE AIRCRAFT PRIOR TO DEPARTURE.
Factual narrative
ACCORDING TO REPORTS FROM THE OPERATOR, THE PILOT DEPARTED FROM NORTH LAS VEGAS WITH A FUEL LOAD ABOUT ONE HALF TANK CAPACITY. THE PILOT DID NOT REFUEL THE AIRCRAFT AT BOULDER CITY. WHILE INBOUND TO NORTH LAS VEGAS, THE PILOT CONTACTED THE LAS VEGAS TERMINAL RADAR APPROACH CONTROL FACILITY AND REPORTED AN ENGINE FAILURE. THE AIRCRAFT ATTEMPTED A LANDING ON A CITY STREET IN A REMOTE INDUSTRIAL AREA. THE AIRCRAFT COLLIDED WITH THE CENTER MEDIAN DIVIDER FENCE OF A STREET DURING THE LANDING ROLL. FAA INSPECTORS EXAMINED THE AIRCRAFT ON THE EVENING OF JUNE 21 AND FOUND NO FUEL IN THE FUEL TANKS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_LAX91LA275.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 (fuel exhaustion, 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…
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