NYC91LA219
1991-08-24 · MEADVILLE, Pennsylvania, United States · Serious · 1 aircraft · Status: Completed
Airport 2G6
Aircraft involved
Probable cause & findings
ENGINE FAILURE RESULTING FROM THE FATIGUE FAILURE OF THE NUMBER 2 CYLINDER EXHAUST VALVE AND THE SUBSEQUENT FORCED LANDING AT NIGHT. A FACTOR RELATED TO THE ACCIDENT WAS THE RESTRICTED VISIBILITY.
Factual narrative
THE AIRPLANE WAS CRUISING AT NIGHT AT 8000 FEET. THE PILOT SAID '[THERE WAS A] SUDDEN VIOLENT VIBRATION...[I] CHANGED MIXTURE, GAS TANKS, ADJUSTED PROP SETTING...NO CHANGES. PULLED POWER BACK TO REDUCE VIBRATION.' THE PILOT WAS VECTORED TOWARDS THE NEAREST AIRPORT. HE WAS ABLE TO LOCATE THE RUNWAY, BUT BECAUSE OF FOG AND LACK OF ADEQUATE VISIBILITY, HE WAS UNABLE TO DISSIPATE THE EXCESS ALTITUDE AND OVERSHOT THE RUNWAY. THE EXAMINATION OF THE ENGINE REVEALED THE NUMBER 2 CYLINDER EXHAUST VALVE FAILED BECAUSE OF FATIGUE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_NYC91LA219.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
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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…