FTW90LA116
1990-06-07 · PASENDENA, Texas, United States · Minor · 1 aircraft · Status: Completed
Airport EFD
Aircraft involved
Probable cause & findings
ENGINE FAILURE DUE TO AN UNDETERMINED REASON.
Factual narrative
FOLLOWING A RAPID DESCENT FROM 1,500 FEET TO 600 FEET, THE PILOT LEVELED OFF AND APPLIED ENGINE POWER AND RECEIVED NO RESPONSE. HIS EFFORTS TO REMEDY THE SITUATION WERE NOT SUCCESSFUL AND HE DECIDED TO EXECUTE A FORCED LANDING TO A FIELD. ON SHORT FINAL THE AIRPLANE STRUCK BRUSH, NOSED DOWN, AND FLIPPED OVER. EXAMINATION OF THE WRECKAGE REVEALED ADEQUATE FUEL ON BOARD AND FUEL WAS FOUND THROUGHOUT THE SYSTEM AND ENGINE UP TO THE FLOW DIVIDER. FOLLOWING RECOVERY, THE ENGINE WAS TEST RUN WHILE STILL MOUNTED ON THE AIRFRAME, USING EXISTING CONTROLS AND AN IMPROVISED FUEL SUPPLY SYSTEM. THE ENGINE STARTED AND WAS OPERATED UP TO POWER SETTINGS OF 2,000 RPM. THROUGHOUT THE RUNS THE ENGINE RESPONDED TO ALL THROTTLE MOVEMENTS WITHOUT HESITATION. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1990_FTW90LA116.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…