SEA06LA012
2005-10-20 · Gleneden Beach, Oregon, United States · None · 1 aircraft · Status: Completed
Airport S45
Current FAA registration · N6000A
- Make / Model
- CESSNA 172
- Year of manufacture
- 1956 · 49 years old at event
- Engine
- CONT MOTOR 0-300 SER (145 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19560326
- ADS-B equipped
- Yes — Mode-S A7C998
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain clearance from objects while maneuvering over the airport environment. Dark night conditions, trees, and ground fog were factors.
Factual narrative
On October 20, about 2000 Pacific daylight time, a Cessna 172, N6000A, registered to and operated by the pilot as a 14 CFR Part 91 personal flight, collided with a tree while maneuvering near the Siletz Bay State Airport, Gleneden Beach, Oregon. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft was substantially damaged and the private pilot and passenger were not injured. The flight departed from Hillsboro, Oregon, about 30 minutes prior to the accident with the intended destination of Siletz Bay State. During a telephone interview, the pilot reported that he was maneuvering around the airstrip to determine runway conditions. There was ground fog present and the lighting conditions were "very dark." The pilot circled the airstrip three or four times and he had the rotating beacon and runway lights in sight, however, he lost sight of the runway lights and when he passed by the rotating beacon he pulled up and heard something hit the right wing. The pilot believed that he was near the southwest end of the airport environment when this happened. The pilot stated that he was unsure if he hit a tree or a bird, but decided not to land and diverted to McMinnville, Oregon, a distance of 42 nautical miles to the northeast, where a landing was made without further incident. Inspection of the aircraft revealed that the right wing tip, to include the outboard rib and about half of the right side aileron had been torn away. The pilot reported that he was in-flight maneuvering over the airstrip to determine runway conditions. There was ground fog present and the lighting conditions were "very dark." The pilot circled the airstrip three or four times and he had the rotating beacon and runway lights in sight, however, he lost sight of the runway lights and when he passed by the rotating beacon he pulled up and heard something hit the right wing. The pilot believed that he was near the southwest end of the airport environment when this happened. The pilot stated that he was unsure if he hit a tree or a bird, but decided not to land and diverted to another airport 42 nautical miles to the northeast, where a landing was made without further incident. Inspection of the aircraft revealed that the right wing tip, to include the outboard rib and about half of the right side aileron had been torn away. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_SEA06LA012.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.