SEA05CA088
2005-04-27 · Eureka, Montana, United States · None · 1 aircraft · Status: Completed
Airport 88M
Current FAA registration · N1387Q
- Make / Model
- CESSNA 150L
- Year of manufacture
- 1971 · 34 years old at event
- Engine
- CONT MOTOR 0-200 SERIES (100 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19710811
- ADS-B equipped
- Yes — Mode-S A09C45
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to adequately compensate for the wind conditions during the landing roll. Factors include a 10 knot crosswind, with gusts up to 15 knots, and a taxiway sign near the point where the aircraft exited the runway.
Factual narrative
On April 27, 2005, about 1300 mountain daylight time, a Cessna 150L, N1387Q, registered to and flown by the pilot as a 14 CFR Part 91 personal flight, collided with a taxiway sign during landing at Eureka Airport, Eureka, Montana. Visual meteorological conditions prevailed at the time, and no flight plan was filed. The aircraft was substantially damaged and the private pilot and his pilot-rated passenger were not injured. The flight originated from Eureka at 1200 as a local flight. During a telephone interview, the pilot reported that during the landing roll on runway 36, the aircraft encountered a gust of wind. The pilot was unable to maintain directional control, and the aircraft traveled to the side of the runway where the horizontal stabilizer collided with a taxiway sign. The taxiway sign was knocked over and the horizontal stabilizer sustained substantial damage. The pilot reported no mechanical failures or malfunctions with the aircraft at the time. The pilot reported the winds to be from 080 degrees at 10 knots with gusts to 15 knots. During the landing roll, the aircraft encountered a gust of wind, and the pilot was unable to maintain directional control. The aircraft therefore exited the side of the runway, where the horizontal stabilizer collided with a taxiway sign. The taxiway sign was knocked over and the horizontal stabilizer sustained substantial damage. There were no mechanical failures or malfunctions with the aircraft. At the time of the accident, there was a crosswind of 10 knots with gusts to 15 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_SEA05CA088.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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