NYC00LA158
2000-06-12 · WAUSEON, Ohio, United States · None · 1 aircraft · Status: Completed
Airport USE
Current FAA registration · N8197W
- Make / Model
- PIPER PA-32R-301T
- Year of manufacture
- 1980 · 20 years old at event
- Engine
- LYCOMING TI0-540 SER (310 hp)
- Seats / Engines
- 7 seats · 1 engine
- Last airworthiness date
- 19800317
- ADS-B equipped
- Yes — Mode-S AB2E2D
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airspeed, which resulted in an inadvertent stall.
Factual narrative
On June 12, 2000, about 0720 Eastern Daylight Time, a Piper PA-32R-301T, N8197W, was substantially damaged while landing at the Fulton County Airport, Wauseon, Ohio. The certificated private pilot and two passengers were not injured. Instrument meteorological conditions prevailed and an instrument flight rules flight plan was filed for the personal flight conducted under 14 CFR Part 91. According to the pilot, he executed the NDB approach to Runway 27, flew over the centerline of the runway and made a 180-degree turn to land on Runway 09. During the turn, the pilot overshot the extended centerline of Runway 09 and attempted to realign the airplane to the runway centerline. While maneuvering back to the runway centerline, the airplane stalled just above the runway and impacted the ground. The airplane touched down on all three landing gear, slid sideways and came to rest in a water drainage ditch. The pilot estimated that the cloud bases at the time of the accident were about 650 feet above the ground and 1 mile of visibility with heavy rain. After the accident, the pilot stated to an Ohio State Police officer that his airspeed was "about 80 knots but less because stalled about then." When interviewed by a Federal Aviation Administration inspector, the pilot stated that he did not recall hearing the stall warning horn or what his airspeed was while maneuvering. At 0700, the reported weather at an airport located 15 miles to the west of the accident site was: winds from 100 degrees at 8 knots; 1 3/4 miles of visibility with light rain and mist; overcast clouds at 300 feet. While executing a non-precision approach, the pilot flew over the centerline of the runway and made a 180-degree turn to land on the reciprocal runway. During the turn, the pilot overshot the extended centerline. While maneuvering back to the runway centerline, the airplane stalled just above the runway and impacted the ground, before coming rest in a water drainage ditch. After the accident, the pilot stated that his airspeed was 'about 80 knots but less because stalled about then.' Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_NYC00LA158.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 (stall). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
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- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…