NTSB CAROL · Event
Event ERA11CA096
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during the takeoff roll. Contributing to the accident was the pilot’s attempt to take off with full flaps.
Factual narrative
According to the pilot, he was practicing touch and go landings on runway 5, a 6,404-foot-long, 150-foot-wide runway. During the takeoff roll following his eighth landing, the pilot felt "a gust of wind pushing…the plane to the left." He applied full right aileron, but could not arrest the turn. The pilot then applied the brakes, but the airplane departed the left side of the runway, impacted a ditch, and came to rest inverted, resulting in substantial damage to the firewall, wings, and vertical stabilizer. During a subsequent examination of the wreckage, a Federal Aviation Administration inspector found the flaps in the FULL, 30-degree position. The inspector also reported that there were no preexisting mechanical anomalies with the airplane. Winds, recorded at the airport about the time of the accident, were from 350 degrees true at 7 knots. According to the pilot, he was practicing touch-and-go takeoffs and landings. During the takeoff roll following his eighth landing, he said he felt a gust of wind push the plane to the left. He applied full right aileron, but could not arrest the turn. He then applied the brakes, but the airplane departed the left side of the runway, impacted a ditch, and came to rest inverted, resulting in substantial damage to the firewall, wings, and vertical stabilizer. During a subsequent examination of the wreckage, a Federal Aviation Administration inspector found the flaps in the FULL, 30-degree position. The inspector also reported that there were no anomalies with the airplane. The reported wind at the airport about the time of the accident was from 350 degrees at 7 knots. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2010_ERA11CA096.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 ↗