ATL90LA063
1990-02-10 · OCEAN ISLAND BE, North Carolina, United States · None · 1 aircraft · Status: Completed
Aircraft involved
Probable cause & findings
LOSS OF ENGINE POWER DUE TO FUEL STARVATION AND THE PILOT IN COMMANDS FAILURE TO TURN ON THE ELECTRIC BOOST PUMP DURING ATTEMPTED ENGINE RESTART RESULTING IN A FORCED LANDING.
Factual narrative
THE PILOT HAD RETURNED FROM A 3.5 HOUR CROSS COUNTRY FLIGHT THE PREVIOUS WEEK. THIS FLIGHT WAS TO FUEL THE AIRPLANE AT A NEARBY AIRPORT. AFTER TAKEOFF THE PILOT SAW A RAIN SHOWER AT THE DESTINATION & RETURNED TO HIS DEPARTURE AIRPORT. ON BASE LEG THE ENGINE QUIT. THE FUEL SELECTOR WAS CHANGED FROM THE RIGHT TANK TO THE LEFT BUT, THE AUXILIARY FUEL PUMP WAS LEFT OFF. A FORCED LANDING ENSUED ON A SAND DUNE. EXAMINATION OF THE AIRPLANE REVEALED 1/2 GAL OF FUEL IN THE RIGHT TANK & EIGHT PLUS GALS IN THE LEFT TANK. A WX BRIEF WAS NOT OBTAINED. FLIGHT MANUAL LIST AUXILIARY FUEL PUMP-ON IN ENGINE FAILURE EMERGENCY PROCEDURE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1990_ATL90LA063.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 starvation, 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…