NTSB CAROL · Event
Event SEA03LA193
Registry · N8351M
FAA Aircraft Registry record.
Make / Model
CESSNA A150K
Engine
CONT MOTOR 0-200 SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19690927
ADS-B equipped
Yes — Mode-S AB6D74
Registrant of record
WHEATON ERIC J
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's failure to maintain directional control of the aircraft during the landing roll.
Factual narrative
On September 18, 2003, at 1130 Pacific daylight time, a Cessna A150K, N8351M, registered to and operated by the CAP Aero Club, as a 14 CFR Part 91 instructional flight, was substantially damaged during the landing roll at the Rogue Valley International Airport, Medford, Oregon. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The aircraft was substantially damaged and the student pilot, the sole occupant, was not injured. In a written statement, the student pilot reported that she was practicing touch-and-go landings on runway 32. Six touch-and-goes were accomplished successfully. The student pilot stated that during the landing for the seventh, the approach was stable. As soon as the aircraft touched down, "the plane took a hard right turning on its right wheel and hit the right wing tip, causing my prop to also be ruined." The student was also thrown to the right side, but was able to pull herself back into position and gain control of the aircraft. The student pilot reduced the throttle as the aircraft veered back to the left, eventually coming to a stop. The right wing outboard section was damaged as well as the propeller. Additional damage included the engine mount and wrinkles to the fuselage aft of the main landing gear. The Medford surface observation taken at 1053, was reporting a variable wind at four knots. The 1153 observation was reporting a calm wind. The student pilot reported that she was practicing touch-and-go landings. During the seventh landing, the approach was stable. As soon as the aircraft touched down, it took a hard right turn on the right main landing gear. The right wing and propeller contacted the surface. The student was thrown to the right side, but was able to pull herself back into position and gain control of the aircraft. The student reduced power as the aircraft veered back to the left, eventually coming to a stop. At the time of the accident, the wind was variable at four knots to calm. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_SEA03LA193.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). 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 · Contractor Report (CR)
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 · 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…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗