NTSB CAROL · Event
Event CHI03LA190
Registry · N30CM
FAA Aircraft Registry record.
Make / Model
CESSNA A185F
Year of manufacture
1974 · 29 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19740621
ADS-B equipped
Yes — Mode-S A31D37
Registrant of record
BOARDMAN AIR SERVICE LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's misjudgment of speed and distance resulting in an overrun. Factors were the ditch embankment, and the tailwind component.
Factual narrative
On July 1, 2003, at 1430 central daylight time, a Cessna A185F, N30CM, piloted by a private pilot, sustained substantial damage when it overran runway 36 (1,800 feet by 100 feet, grass/turf) and went into a ditch at the Sky Harbor Seaplane Base, Eveleth, Minnesota. The 14 CFR Part 91 personal flight was operating in visual meteorological conditions without a flight plan. The pilot and passenger were not injured. The flight originated from the Manitowish Waters Airport, Manitowish Waters, Wisconsin, at 1310. The runway is adjacent to the seaplane base and is used by aircraft coming to the base to have floats installed. In a written report, the pilot stated that on his first landing approach, he noticed a mower on the runway and aborted the landing. He contacted the airport to have the mower exit the runway. The pilot stated that he circled the airstrip 2 to 3 times before making another landing attempt. On the second landing attempt, the mower had moved to the right side of the runway about 1/4 of the way down the length of the runway. The pilot stated that he landed past the location of the mower, touching down past the halfway point on the runway. He reported that the airplane was too fast to stop on the grass runway, subsequently impacting the ditch embankment. The pilot reported no mechanical difficulties with the airplane. A weather reporting station about 2 nautical miles and 200 degrees from the accident site recorded the wind at 1436 as 230 degrees at 8 knots. The tailwind component was calculated to be 5 knots. The airplane was substantially damaged when it overran the grass runway and hit a ditch embankment. The pilot reported that on the final landing attempt he landed past a mower that had cleared the runway about 1/4 of the way down the length of the runway. He stated that he touched down past the halfway point on the runway and was too fast to stop on the grass runway, subsequently impacting the ditch embankment. The pilot reported no mechanical difficulties with the airplane. The tailwind component was calculated to be 5 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_CHI03LA190.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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