NYC91LA201
1991-08-06 · WESTERLY, Rhode Island, United States · None · 1 aircraft · Status: Completed
Airport WST
Current FAA registration · N30837
- Make / Model
- PIPER J3C-65
- Year of manufacture
- 1940 · 51 years old at event
- Engine
- CONT MOTOR A&C65 SERIES (65 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19560303
- ADS-B equipped
- Yes — Mode-S A33FEB
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
ENGINE FAILURE FOR AN UNDETERMINED REASON. A FACTOR WAS THE PILOT MISJUDGING THE CLEARANCE OVER A FENCE DURING AN ATTEMPTED FORCED LANDING.
Factual narrative
THE PILOT STATED THAT SHE EXPERIENCED A PARTIAL POWER LOSS AFTER TAKEOFF WHILE CLIMBING THROUGH 300 FEET AGL. SHE SUBSEQUENTLY ATTEMPTED TO TURN BACK TO THE AIRPORT, HOWEVER, DURING THE TURN THE AIRPLANE DEVELOPED A DESCENT RATE AND THE PILOT CHANGED HER INTENDED FORCED LANDING AREA TO A STREET RATHER THAN IN FRONT OF THE AIRPORT TERMINAL. ON SHORT FINAL, THE AIRPLANE STRUCK A CHAIN LINK FENCE AND CONTROL WAS LOST. THE AIRPLANE CAME TO REST IN FRONT OF THE TERMINAL. THE REASON FOR THE POWER LOSS WAS NOT DETERMINED DURING THE INVESTIGATION. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_NYC91LA201.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…