ATL87LA055
1987-01-04 · GALLIPOLIS, Ohio, United States · Minor · 1 aircraft · Status: Completed
Airport GAS
N345TR has since been reassigned. It is now registered to a different aircraft (ISRAEL AIRCRAFT INDUSTRIES 1124A, built 1981), which was not involved in this event.
Aircraft involved
Factual narrative
THE FLIGHT WAS ESTABLISHED IN THE TRAFFIC PATTERN WHEN THE PILOT EXPERIENCED A DUAL ENGINE FAILURE. THE PILOT ATTEMPTED TO RESTART THE ENGINES BUT FAILED. THE PILOT ALSO FAILED TO FEATHER THE PROPELLERS WHICH CREATED A AERODYNAMIC CONDITION WHICH ALLOWED THE AIRCRAFT TO DESCEND FASTER THAN NORMAL. THE AIRCRAFT CRASHED SHORT OF THE RUNWAY AFTER PULLING UP TO AVOID A COLLISION WITH AN AUTOMOBILE ON THE ROAD OF INTENDED LNDG. THE WRECKAGE EXAMINATION FAILED TO DISCLOSE ANY AIRCRAFT PROBLEMS. THE EXACT REASON FOR THE DUAL ENGINE FAILURE WAS NOT DETERMINED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1987_ATL87LA055.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 (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…