NTSB CAROL · Event
Event CHI96LA244
Aircraft involved
Probable cause & findings
the student pilot's failure to maintain airplane control during a go-around.
Factual narrative
On July 16, 1996, at 1530 central daylight time (cdt), a Cessna 150L, N11303, piloted by a student pilot, was substantially damaged when it cartwheeled after its left wingtip collided with the ground during a go-around on runway 25 (2,805' X 39' dry asphalt) at the Roy Otten Memorial Airfield, Versailles, Missouri. The 14 CFR Part 91 solo instructional flight was operating on a VFR flight plan. Visual meteorological conditions prevailed at the time of the accident. The pilot reported minor injuries. The flight departed Lee's Summitt, Missouri, at 1430 cdt. The pilot's said his airplane was on final approach when he extended 15 degrees of flaps. His written statement said his airplane "...was still fast and running out of runway" when he did an aborted landing. The pilot said he "...applied full throttle, and pull[ed] back on [the] yoke. Plane went down and to left." During an interview with the pilot on July 17, 1996, he said his final approach was too low and fast. He said the airplane banked left after he added full power. He said a gusty crosswind existed at the time he was landing. The pilot said he did not see a wind sock and had no idea where the wind was coming from. When asked how he would judge his final approach path the pilot responded by saying he would use the visual approach slope indicator (VASI) light system. He added that the runway did not have a VASI system. When asked how he would judge his final approach path without the VASI aid, he responded, "By feel, I guess." A witness to the accident said he saw N11303 on a high final approach for runway 25. This witness said the winds were from the southwest at between 5 and 8 miles per hour. He said the airplane had full flaps extended and was about 100 to 200 feet above the runway threshold as it passed over it. He said the airplane's pitch attitude was less than a level flight attitude and that he heard no engine noise. The witness said the airplane was about 2/3 to 3/4 the way down the runway before it attempted to go around. He then heard the engine power increase and saw the airplane pitch up, stall, and roll to the left. N11303's wingtip struck the ground followed by a cartwheel maneuver according to this witness. The on-scene investigation revealed no mechanical anomalies that would have prevented normal flight. The airport has a wind sock and wind tetrahedron at runway 25's midfield location. A witness reported that the airplane had full flaps and was high on final approach. About 2/3 down the runway the pilot applied full power to reject the landing. The witness reported that the airplane pitched up and rolled left after the power was applied. The airplane's left wingtip struck the ground followed by the airplane doing a cartwheel maneuver. The pilot said the airplane was influenced by a gusty crosswind. The witness said the wind was from the southwest at 5 to 8 mph. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_CHI96LA244.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, go-around). 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 …
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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…
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