BFO92LA033
1992-03-07 · QIOQUINTON, Virginia, United States · None · 1 aircraft · Status: Completed
Airport W96
N27613 has since been reassigned. It is now registered to a different aircraft (BOEING 737-10), which was not involved in this event.
Aircraft involved
Probable cause & findings
ENGINE FAILURE DUE TO FUEL EXHAUSTION BECAUSE OF AN OPEN CROSSFEED FUEL LINE DRAIN VALVE.
Factual narrative
THE AIRLINE TRANSPORT PILOT WAS DIVERTING TO HIS NEW DESTINATION WHEN BOTH ENGINES LOST POWER. A GEAR UP LANDING WAS MADE IN A FIELD 3 MILES NE OF THE AIRPORT. WHILE EN ROUTE THE PILOT OBSERVED THERE WAS AN EXCESSIVE FUEL CONSUMPTION FROM THE LEFT TANK, SO HE RECALCULATED THE FUEL HE HAD REMAINING ON BOARD WHICH HE DETERMINED TO BE TWO HOURS. HE PROCEEDED TO HIS DESTINATION AS IT WAS ONLY 50 MINUTES AWAY FROM HIS PRESENT POSITION. EXAMINATION OF THE AIRCRAFT AND THE FUEL SYSTEM BY THE FAA REVEALED THE CROSSFEED FUEL LINE DRAIN VALVE WAS OPEN. THERE WERE NO OTHER ABNORMALITIES FOUND IN THE SYSTEM. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1992_BFO92LA033.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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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…