NTSB CAROL · Event
Event SEA07CA265
Aircraft involved
Probable cause & findings
The pilot's failure to attain an adequate airspeed, which resulted in a forced landing off the end of the runway. A contributing factor to the accident was the gusting wind.
Factual narrative
The 33-hour student pilot intended to practice short field takeoffs and landings. This was his first time practicing short field takeoffs and landings as the sole occupant of the airplane. The last time he performed a short field takeoff was with his certified flight instructor about 2 months prior to the accident. His preflight and run up checks were all within limits. He selected two notches of flaps and while holding the brakes, applied full power. The airplane accelerated to 65 knots and the airplane lifted from the runway quickly. As the airplane climbed to 100 feet the pilot noted a decrease in airspeed so he pushed the nose over. He retracted a notch of flaps and descended to 20 feet above the runway. The student pilot then force landed the airplane off the end of the runway and it impacted trees. Post accident examination of the wreckage by the Federal Aviation Administration inspector did not reveal any mechanical anomalies with the engine or airframe. The flaps were fully retracted at the accident site. The winds recorded at the airport approximately 3 minutes prior to the accident were from 240 degrees at 10 knots, with 16-knot wind gusts. The 33-hour student pilot was performing a short field takeoff. He selected two notches of flaps and while holding the brakes, applied full power. The airplane accelerated to 65 knots and lifted from the runway. The airspeed then decreased so the pilot pushed the nose over and retracted the flaps. He continued to descend and the airspeed would not increase. The pilot force landed the airplane off the end of the runway and it impacted trees. According to the Federal Aviation Administration inspector, there were no mechanical malfunctions with the airframe or engine. Winds at the time of the accident were from 240 degrees at 10 knots, with 16-knot wind gusts. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_SEA07CA265.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 ↗