CHI95LA168
1995-05-25 · EVELETH, Minnesota, United States · None · 1 aircraft · Status: Completed
Airport 9Y5
Current FAA registration · N8611X
- Make / Model
- CESSNA 180D
- Year of manufacture
- 1961 · 34 years old at event
- Engine
- CONT MOTOR O-470 SERIES (230 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19610211
- ADS-B equipped
- Yes — Mode-S ABD51F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's improper setting of the flaps to the 30 degree position and an excessive descent rate during the landing.
Factual narrative
On May 25, 1995, at 0804 central daylight time, a Cessna 180D, sustained substantial damage during landing at the Sky Harbor Seaplane Base in Eveleth, Minnesota. The private pilot and two passengers reported no injuries. The personal, 14 CFR Part 91 flight originated in Milwaukee, Wisconsin. Visual meteorological conditions prevailed and an IFR flight plan was filed. In his written statement the pilot reported that he used what he believed was 20 degrees of flaps and turned onto final approach at an airspeed of 80 knots with the power set at 15 inches of manifold pressure. As he flew over the trees prior to the threshold, he heard the stall warning indicator. He applied full power and the airplane impacted the runway. The airplane bounced and the right wing impacted bushes along the side of the runway. The pilot reported that he examined the airplane following the accident and discovered the flaps were in the 30 degree position. He reported that he had never landed the airplane in this configuration before. IN HIS WRITTEN STATEMENT THE PILOT REPORTED THAT HE USED WHAT HE BELIEVED WAS 20 DEGREES OF FLAPS AND TURNED ONTO FINAL APPROACH AT AN AIRSPEED OF 80 KNOTS WITH THE POWER SET AT 15 INCHES OF MANIFOLD PRESSURE. AS HE FLEW OVER THE TREES PRIOR TO THE THRESHOLD, HE HEARD THE STALL WARNING INDICATOR. HE APPLIED FULL POWER AND THE AIRPLANE IMPACTED THE RUNWAY. THE AIRPLANE BOUNCED AND THE RIGHT WING IMPACTED BUSHES ALONG THE SIDE OF THE RUNWAY. THE PILOT REPORTED THAT HE EXAMINED THE AIRPLANE FOLLOWING THE ACCIDENT AND DISCOVERED THE FLAPS WERE IN THE 30 DEGREE POSITION. HE REPORTED THAT HE HAD NEVER LANDED THE AIRPLANE IN THIS CONFIGURATION BEFORE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_CHI95LA168.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.
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
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- 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…