CHI96LA297
1996-08-14 · COLUMBIA, Missouri, United States · None · 1 aircraft · Status: Completed
Airport COU
Current FAA registration · N10645
- Make / Model
- CESSNA 150L
- Engine
- CONT MOTOR 0-200 SERIES (100 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19730721
- ADS-B equipped
- Yes — Mode-S A01E00
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the improper recovery from a bounced landing by the pilot in command. Factors were the gusty wind conditions, and the failure of the pilot to maintain aircraft control.
Factual narrative
On August 14, 1996, at 1400 central daylight time (cdt), a Cessna 150, N10645, sustained substantial damage during a hard landing on runway 31, at the Columbia Regional Airport, Columbia, Missouri. The student pilot was returning from a solo cross country flight, at the time of the accident. The pilot was uninjured in the accident. The 14 CFR Part 91 flight was operating in visual meteorological conditions, and a VFR flight plan had been filed for the flight. The pilot reported on NTSB Form 6120.1/2 that she had aborted the first landing, and this was the second approach for landing. She reported that the airplane was on short final, with 20 degrees of flaps, at 80 knots. She reported the airspeed was excessive, and as the airplane came over the runway full flaps were extended. The pilot reported that after full flaps were extended the airplane stalled, and bounced on the runway. After the bounced landing she put the nose of the airplane down causing the airplane to hit nose wheel first on the runway. The pilot did not report any mechanical malfunctions with the airplane or the engine. The airplane's nose gear, engine mount, firewall and propeller were all bent in the accident. The student pilot reported that this was the second approach for landing. The pilot reported the airspeed was excessive on final approach, and extended full flaps. After full flaps were extended the airplane stalled, and bounced on the runway. The pilot reported that after the bounced landing she put the nose of the airplane down, causing the airplane to hit nose wheel first on the runway. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_CHI96LA297.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.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
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 …
- 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…
- arXiv 2021 · arXiv preprint Investigation of flow field of clap & fling motion using immersed boundary coupled lattice Boltzmann method
This paper deals with the investigation of flow field due to clap and fling mechanism using immersed boundary coupled with lattice Boltzmann method.