FTW91LA107
1991-06-22 · SAN ANGELO, Texas, United States · None · 1 aircraft · Status: Completed
Airport SJT
Current FAA registration · N2424J
- Make / Model
- CESSNA 525B
- Seats / Engines
- 8 seats · 2 engines
- ADS-B equipped
- Yes — Mode-S A23A5A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S FAILURE TO REFUEL THE AIRPLANE WHICH RESULTED IN ENGINE FAILURE DUE TO FUEL EXHAUSTION.
Factual narrative
DURING A FLIGHT FROM MIDLAND, TEXAS, TO SAN ANGELO, TEXAS, THE AIRPLANE LOST ENGINE POWER WHILE CRUISING AT 5,500 FEET MEAN SEA LEVEL, DUE TO FUEL EXHAUSTION. THE INSTRUCTOR PILOT ATTEMPTED TO LAND IN THE ONLY AVAILABLE AREA; HOWEVER, THIS PROVED TO BE UNSUITABLE AND RESULTED IN THE AIRPLANE NOSING OVER TO THE INVERTED POSITION AND SUSTAINING SUBSTANTIAL DAMAGE. NEITHER WING FUEL TANK WAS COMPROMISED AND THERE WAS NO EVIDENCE OF FUEL SPILLAGE. APPROXIMATELY 12 OUNCES OF FUEL WAS RECOVERED FROM THE TANKS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_FTW91LA107.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type or causal vocabulary (fuel exhaustion, 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…