NYC06LA139
2006-06-05 · Du Bois, Pennsylvania, United States · Serious · 1 aircraft · Status: Completed
Airport DUJ
Aircraft involved
Probable cause & findings
The pilot's inadequate compensation for wind conditions, which resulted in a stall and subsequent impact with the ground. A factor was the wind gust as reported by the pilot.
Factual narrative
On June 5, 2006, at 1615 eastern daylight time, a Piper PA-28-180, N1654B, was substantially damaged during landing at Du Bois-Jefferson County Airport (DUJ), Du Bois, Pennsylvania. The certificated private pilot received serious injuries and the pilot-rated passenger received minor injuries. Visual meteorological conditions prevailed for the flight that originated at the Zelienople Municipal Airport (8G7), Zelienople, Pennsylvania. No flight plan was filed for the personal flight conducted under 14 CFR Part 91. According to the pilot-rated passenger, as the pilot flared for landing, a gust of wind lifted the airplane at "an extremely high angle to the runway, and then quit." The airplane "stalled," nosed over, and impacted the ground. A postcrash fire ensued; however, both occupants were able to egress prior to the airplane being consumed. The pilot reported the same sequence of events, and additionally reported there were no mechanical anomalies with the airplane. A witness who was also a commercial airline pilot, observed the airplane flying at an altitude of approximately 10 feet over the approach end of runway 07. The airplane appeared to be performing a "normal landing" until the airplane "was lifted in a vertical motion" to an altitude of approximately 30 feet. The airplane then nosed over and impacted the runway. Examination of the airplane by a Federal Aviation Administration inspector revealed no preimpact mechanical deficiencies with the airplane. The propeller displayed rotational damage, and flight control continuity was confirmed to the flight controls. According to the pilot, at the time of the accident, he had accumulated 528 hours of total flight experience. The weather recorded at DUJ, at 1556, included variable winds at 3 knots, 10 miles visibility, few clouds at 10,000 feet, temperature 75 degrees Fahrenheit, dew point 45 degrees Fahrenheit, and an altimeter setting of 29.95 inches Mercury. As the pilot flared for landing a gust of wind lifted the airplane at "an extremely high angle to the runway, and then quit." The airplane then "stalled," impacted the ground, and caught fire. The pilot reported he had accumulated 528 hours of total flight experience at the time of the accident. He additionally reported experiencing no mechanical anomalies with the airplane. Examination of the airplane by an FAA inspector also revealed no mechanical deficiencies. The winds reported at the airport, at the time of the accident were variable at 3 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_NYC06LA139.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 (stall). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
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Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…