NTSB CAROL · Event
Event CHI96LA022
Aircraft involved
Probable cause & findings
failure of the pilot to maintain adequate airspeed after takeoff, which resulted in a stall. A factor relating to the accident was: the gusty wind condition.
Factual narrative
On October 29, 1995, at 1130 eastern standard time (est), a Piper J-3C, NC88037, piloted by a private pilot, was substantially damaged during a collision with terrain, shortly after takeoff. Visual conditions prevailed at the time of the accident. The personal 14 CFR part 91 flight was not operating on a flight plan. The pilot sustained serious injuries. The flight departed Rochester, Indiana, at 1129 est. In the pilot's written statement he wrote that after departing runway 29 he initiated a right turn at 200 feet above ground level (AGL). The pilot wrote that "a wind gust blew the aircraft almost inverted." The pilot reported that the airplane then stalled, with insufficient altitude to recover. The pilot estimated the wind speed at 15 knots with gusts to 25 knots. No mechanical malfunction was reported by the pilot. Four witnesses were interviewed by the investigator in charge and the Federal Aviation Administration. The witnesses estimated that the airplane began the right turn between 50 and 200 feet AGL. Two witnesses reported that the airplane appeared to do a maneuver similar to a wing over, before impacting the ground. The airplane's right wing was crushed. The propeller, fuselage and engine mount were bent. The landing gear collapsed during impact. THE PILOT REPORTED THAT AFTER TAKING OFF FROM RUNWAY 29, A WIND GUST AT ABOUT 200 FEET ABOVE GROUND LEVEL (AGL) CAUSED THE AIRPLANE TO GO TO A NEAR INVERTED ATTITUDE AND STALL. HE ALSO REPORTED THAT THERE WAS INSUFFICIENT ALTITUDE TO RECOVER. THE PILOT ESTIMATED THE WIND SPEED AT 15 KNOTS WITH GUSTS TO 25 KNOTS. WITNESS'S ESTIMATED THAT THE AIRPLANE BEGAN THE RIGHT TURN BETWEEN 50 AND 200 FEET AGL. TWO WITNESS'S REPORTED THAT THE AIRPLANE APPEARED TO GO INTO A WINGOVER BEFORE IMPACTING THE GROUND. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_CHI96LA022.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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 …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
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…
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