NTSB CAROL · Event
Event SEA05LA051
Registry · N181WC
FAA Aircraft Registry record.
Make / Model
AVIAT AIRCRAFT INC A-1C-200
Year of manufacture
2020
Engine
LYCOMING IO-390-C3B6 (215 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20201014
ADS-B equipped
Yes — Mode-S A1465A
Registrant of record
AVIAT AIRCRAFT INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's improper compensation for the wind condition and the improper rejected landing procedure, which resulted in the collision with terrain. A contributing factor to the accident was the crosswind condition.
Factual narrative
On February 22, 2005, approximately 1500 Pacific standard time, a Piper PA-28-181 single-engine airplane, N181WC sustained substantial damage after impacting terrain following an aborted landing at the Columbia Gorge Regional/The Dalles Municipal Airport (DLS), The Dalles, Oregon. The airplane was registered to a private individual, and the student pilot, sole occupant of the aircraft sustained serious injuries. Visual meteorological conditions prevailed for the instructional flight, which was conducted in accordance with 14 CFR Part 91, and a flight plan was not filed. The local flight departed DLS about 1445. According to the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the student pilot reported that while inbound for landing on Runway 07, "...the Automated Surface Observing System (ASOS) told me the wind was at 9 knots. I started getting nervous thinking of landing with wind. We had no training on crosswinds." The student pilot stated that on final [approach] when she realized the wind was pushing her to the left and the stall warning [horn] was going off, she [added] full throttle to go around. The student pilot related that at this time the [airplane] initially pitched down, but then she became totally confused. "...it felt like I was spinning. In turning to the left the wing caught [the ground] and brought me down." The student pilot also reported that she could not remember whether the nose of the airplane was supposed to be pitched up or down when attempting a go-around. A Federal Aviation Administration aviation safety inspector traveled to the accident site and reported the left wing was broken into three pieces. At 1453, the DLS ASOS weather reporting system indicated wind 060 degrees at 9 knots, visibility 10 statue miles, sky clear, temperature 12 degrees C, dew point -3 degrees C, and the altimeter setting of 30.23 inches of Mercury. On final approach the student pilot became nervous thinking about landing with a crosswind, as she had no previous training in crosswind landings. With the wind pushing the airplane to the left the pilot initiated a go-around, but became confused and could not remember if the nose should be pitched up or down. The airplane initially pitched down, resulting in the left wing impacting the ground and cartwheeling. The aircraft came to rest in an upright position with the left wing separated into three pieces. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_SEA05LA051.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall, go-around). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
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