NTSB CAROL · Event
Event SEA05CA003
Registry · N2849Z
FAA Aircraft Registry record.
Make / Model
PIPER PA-22-160
Year of manufacture
1959 · 45 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19590617
ADS-B equipped
Yes — Mode-S A2E082
Registrant of record
ALEXANDER TRAVIS M
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate compensation for crosswind conditions during landing, resulting in his failure to maintain directional control. Factors include the presence of crosswinds.
Factual narrative
On October 1, 2004, at 1705 Pacific daylight time, a tailwheel equipped Piper PA-22/20, N2849Z, impacted the terrain during an attempted landing at Rogue Valley International Airport, Medford, Oregon. The private pilot, who was the sole occupant of the aircraft, was not injured, but the aircraft, which is owned by another individual, sustained substantial damage. The 14CFR Part 91 personal proficiency flight, which originated at the same airport about 35 minutes earlier, was being conducted in visual meteorological conditions. No flight plan had been filed. There was no report of an ELT activation. According to the pilot, who was practicing touch-and-go landings in crosswind conditions, during his first landing there was a 40 degree crosswind at five knots. As he was cleared for his second landing, the tower advised him that the wind had changed direction and speed, and he was therefore landing in a 60 degree crosswind of seven knots. According to the pilot, during the landing flare, he relaxed his "cross control input" too much, and the aircraft's left wing began to lift. He therefore elected to execute a go-around, but as he added power the aircraft began rotating to the left. He therefore elected to try to put the aircraft back onto the runway, but as it touched down, the aircraft was not aligned with the runway, and it therefore quickly veered to the left. As the aircraft departed the side of the runway, the tip of its right wing came in contact with the terrain resulting in substantial damage to the wing's internal structure. In a telephone interview with the Investigator-In-charge (IIC), the pilot said that there was nothing wrong with the aircraft, and that the accident was simply a result of his failure to adequately control the aircraft in the crosswind conditions. The pilot was practicing touch-and-go landings in crosswind conditions, and during his first landing there was a 40 degree crosswind at five knots. As he was cleared for his second landing, the tower advised him that the wind had changed direction and speed, and he was therefore landing in a 60 degree crosswind of seven knots. During his second landing, he relaxed his "cross control input" too much during the landing flare, and the aircraft's left wing began to lift. He therefore elected to execute a go-around, but as he added power the aircraft began rotating to the left. He therefore elected to try to put the aircraft back onto the runway, but as it touched down, the aircraft was not aligned with the runway, and it therefore quickly veered to the left. As the aircraft departed the side of the runway, the tip of its right wing came in contact with the terrain resulting in substantial damage to the wings internal structure. According to the pilot, there was nothing wrong with the aircraft, and the accident was simply a result of his failure to adequately control the aircraft in the crosswind conditions. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_SEA05CA003.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 (icing, 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.
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Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- 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.
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
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