SEA05CA080
2005-04-09 · Yamhill, Oregon, United States · None · 1 aircraft · Status: Completed
Airport OR05
Current FAA registration · N8400L
- Make / Model
- CESSNA 172I
- Year of manufacture
- 1968 · 37 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19680308
- ADS-B equipped
- Yes — Mode-S AB823C
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain aircraft control while on final approach for landing. A crosswind, a fence post and the pilot's inadequate compensation for the crosswind condition were contributing factors.
Factual narrative
On April 9, 2005, about 0930 Pacific daylight time, a Cessna 172I, N8400L, registered to and flown by the pilot as a 14 CFR Part 91 personal flight, collided with a fence post and subsequently the terrain during landing at Flying M Airport, Yamhill, Oregon. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft was substantially damaged and the private pilot and his passenger were not injured. The flight originated from Salem, Oregon, about 15 minutes prior to the accident. In a written statement, the pilot reported that he was approaching the airstrip from the east for a landing on runway 25. The pilot noted, via the wind sock, that the wind was out of the north at about 5 miles per hour, but variable. The pilot stated that he had just started the flare when the airplane "did a sharp shift to the left, just to the side of the runway." The pilot attempted to correct for the crosswind, however, the airplane continued to move further off to the south side of the runway towards a fence which was located about 25 feet away. The left horizontal stabilizer collided with a fence post about the same time the wheels touched the surface. Due to a vehicle that was on the road that runs parallel to the runway and in close proximity to the airplane, the pilot added full power in an attempt to avoid the car. The airplane traveled up an incline back to the runway surface and toward trees off the north side of the airstrip. The airplane collided with several small trees and eventually traveled into a culvert and tipped over onto its nose, coming to rest in about three feet of water. The pilot reported no mechanical failure or malfunction with the airplane at the time of the accident. In a written statement, the pilot reported that he was approaching the airstrip from the east for a landing on runway 25. The pilot noted, via the wind sock, that the wind was out of the north at about 5 miles per hour, but variable. The pilot stated that he had just started the flare when the airplane "did a sharp shift to the left, just to the side of the runway." The pilot attempted to correct for the crosswind, however, the airplane continued to move further off to the south side of the runway towards a fence which was located about 25 feet away. The left horizontal stabilizer collided with a fence post about the same time the wheels touched the surface. Due to a vehicle that was on the road that runs parallel to the runway and in close proximity to the airplane, the pilot added full power in an attempt to avoid the car. The airplane traveled up an incline back to the runway surface and toward trees off the north side of the airstrip. The airplane collided with several small trees and eventually traveled into a culvert and tipped over onto its nose, coming to rest in about three feet of water. The pilot reported no mechanical failures or malfunctions with the airplane at the time of the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_SEA05CA080.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type. All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (E…
- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- Embry-Riddle Scholarly Commons 2023 · Conference paper Validation of Training Satisfaction Survey
The Training Satisfaction Survey (TSS) was developed as part of a larger project to examine the features of Virtual Reality software and supporting devices as a training program on visual illusions an…
- Semantic Scholar 2021 · Article (Data in Brief) Cockpit voice recorder transcript data: Capturing safety voice and safety listening during historic aviation accidents
Cockpit Voice Recorder (CVR) transcripts capture audio data within cockpit environments. This aids the investigation of causal factors contributing to aviation accidents by revealing communication and…
- Semantic Scholar 2021 · Article (Safety Science) Safety voice and safety listening during aviation accidents: Cockpit voice recordings reveal that speaking-up to power is not enough
Abstract Safety voice is theorised as an important factor for mitigating accidents, but behavioural research during actual hazards has been scant.