NTSB CAROL · Event
Event CHI02LA153
Aircraft involved
Probable cause & findings
The pilot's improper flare resulting in the hard landing.
Factual narrative
On June 6, 2002, at 1400 central daylight time, a Cessna 150C, piloted by a private pilot, was destroyed during a post accident fire following an in-flight collision with runway 18 (4,855 feet by 100 feet, asphalt) during landing at the Anoka Country - Blaine Airport (ANE), Minneapolis, Minnesota. Visual meteorological conditions prevailed at the time of the accident. The personal flight was conducted under the provisions of 14 CFR Part 91 and was not operating on a flight plan. The pilot and passenger were uninjured. The flight originated from the Litchfield Municipal Airport (LJF), Litchfield, Minnesota, at 1315, and was en route to ANE. The pilot stated in her written statement, "...I was able to maintain centerline with some effort... Once over the pavement, it was a little tougher to maintain my descent. I drifted east a little but was able to correct and regained centerline. I was keeping my indicated airspeed up a bit because of the wind, about 70 [knots] on final and 65 [knots] on short final. After I regained centerline I remember wanting to add power to give myself a little time to reestablish my situation since I still had plenty of runway to get down and stop, there was still no doubt I had the landing. I don't remember if I ever got to add any power or not, instantly we just hit the ground. ...We landed near centerline and we landed straight ahead, just somehow nose first. The stall warning horn never went off, I think it happened too fast for it, if we did stall." A witness stated that the airplane flared at approximately 10 feet above the runway. The nose gear broke off the airplane following the impact with the runway. The pilot stated that her legs felt hot shortly after the airplane hit. The pilot and passenger exited the aircraft and the airplane was completely consumed in the post accident fire. The winds reported on the ANE ATIS [automated terminal information service] at the time of the accident were: 190 degrees at 17 knots. No anomalies with respect to the engine, airframe, or systems were determined to have existed prior to the accident. The airplane was destroyed during a post accident fire following an in-flight collision with terrain while landing. The pilot stated, "I don't remember if I ever got to add any power or not, instantly we just hit the ground. ...We landed near centerline and we landed straight ahead, just somehow nose first. The stall warning horn never went off, I think it happened too fast for it, if we did stall." A witness reported seeing the airplane flare at 10 feet above the runway. The airplane's nose gear broke off during the impact and the airplane was completely consumed by the post accident fire. No anomalies with respect to the engine, airframe, or systems were determined to have existed prior to the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_CHI02LA153.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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