NTSB CAROL · Event
Event WPR13CA142
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during the landing roll. Contributing to the accident was the pilot’s failure to adequately latch the canopy before takeoff.
Factual narrative
The pilot stated that he was practicing stop-and-go landings when during the second takeoff, as the airplane was about 10 feet above the runway, the cockpit canopy began to open up and rotate forward. The pilot reached up with his right hand to the canopy handle, located above his head, to hold the canopy down. He decided to abort the takeoff and pointed the airplane back toward the runway. With one hand on the stick and the other on the canopy he could not manipulate the throttle and the airplane landed faster than normal. During the landing roll, the airplane departed the runway, substantially damaging the left wing root and buckling the fuselage behind the firewall. Post accident examination of the canopy locking mechanism revealed that the canopy latch and handle was functioning correctly. The pilot reported that, as the airplane was about 10 feet above the runway during takeoff, the cockpit canopy began to open and rotate forward. The pilot reached up with his right hand to grab the canopy and hold it down. He decided to abort the takeoff and pointed the airplane back toward the runway. He could not manipulate the throttle with one hand on the stick and the other on the canopy, and the airplane landed at a groundspeed of about 55 knots. During the landing roll, the airplane departed the runway, substantially damaging the left wing root and buckling the fuselage behind the firewall. Postaccident examination of the canopy locking mechanism revealed that the canopy latch and handle were functioning properly. 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
- F Aircraft-Aircraft structures-Windows-windshield system-(general)-Unintentional use/operation - F
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- F Personnel issues-Task performance-Use of equip/info-(general)-Pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2013_WPR13CA142.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 ↗