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SEA04LA007

2003-10-18 · Trout Lake, Washington, United States · None · 1 aircraft · Status: Completed

Airport 66WA

Current FAA registration · N1841R

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
19741105
ADS-B equipped
Yes — Mode-S A15213

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The failure of the pilot to maintain directional control of the aircraft during the landing roll. A factor was the wet runway.

Factual narrative

On October 18, 2003, approximately 1420 Pacific daylight time, a Cessna 185 single-engine airplane, N1841R, was substantially damaged following a loss of control during landing roll at the Trout Lake Airport (66WA), Trout Lake, Washington. The airplane was registered to and operated by a private individual. The private pilot and his sole passenger were not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 CFR Part 91 personal flight. The local flight departed Trout Lake at 1410. In a telephone interview with the NTSB investigator-in-charge (IIC), and according to the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the pilot reported that after a normal touchdown, the aircraft rollout was slightly to the right. The pilot stated the aircraft did not respond to left rudder or left wheel braking, but that the skid marks, which were 200 feet in length, indicated the left brake was functioning. The pilot further reported that he then applied heavy braking, and subsequently the right wheel plowed into the ground, causing the tail to come up and the aircraft nosing over. The pilot reported the runway surface was "slightly" wet. An FAA inspector, who traveled to the accident site, inspected the aircraft and reported that there was no evidence found to indicate a mechanical failure or malfunction. The inspector also reported the aircraft had sustained substantial damage to the rudder and vertical stabilizer. After touching down on the wet runway, the aircraft veered slightly to the right. During landing rollout the aircraft did not respond to left rudder or left wheel braking, but skid marks measuring 200 feet in length indicated the left brake was functioning. After applying heavy braking, the right wheel plowed into the ground causing the aircraft to nose over. A post-accident inspection of the airplane did not indicate a mechanical failure or malfunction. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2003_SEA04LA007.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (loss of control). All research papers