DEN90FA166
1990-07-27 · RUIDOSO, New Mexico, United States · None · 1 aircraft · Status: Completed
N105YV has since been reassigned. It is now registered to a different aircraft (CAMERON BALLOONS US A-105, built 2022), which was not involved in this event.
Aircraft involved
Probable cause & findings
ENGINE FAILURE DUE TO FAILURE OF THE GAS PRODUCER AND POWER TURBINE ASSEMBLIES. A FACTOR IN THE ACCIDENT WAS THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING.
Factual narrative
WHEN POWER WAS REDUCED TO BEGIN INITIAL DESCENT FOR APPROACH AND LANDING THE ENGINE LOST POWER AND THE PILOT PERFORMED A FORCED LANDING ON A ROAD. THE ROAD HAD A 4% UPGRADE AND CURVED TO THE RIGHT. DURING THE ROLLOUT THE OUTBOARD END OF THE RIGHT WING STRUCK A TREE DAMAGING THE WING CARRY THROUGH SPAR. METALLURGICAL TESTING REVEALED THE CAUSE OF THE POWER LOSS TO BE FAILURE OF THE GAS PRODUCER TURBINE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1990_DEN90FA166.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 (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…