NTSB CAROL · Event
Event LAX97LA203
Aircraft involved
Probable cause & findings
The pilot's improper use of the elevator and his subsequent failure to maintain directional control during a touch-and-go landing. A factor in the accident was the pilot's application of full power following the loss of directional control, which increased the turning moment already generated by the initial swerve.
Factual narrative
On June 8, 1997, at 1835 hours Pacific daylight time, a Cessna 180, N3343D, ground looped while the pilot was practicing touch-and-go landings at Frazier Lake Airpark, Hollister, California. The aircraft came to rest at the edge of the runway and was destroyed by fire. The private pilot, the sole occupant, evacuated the aircraft with no injuries and there was no property damage. Visual meteorological conditions prevailed for the personal flight and no flight plan was filed for the local flight. The pilot stated in his report that he did not bring the wheel back to place the elevator in the full up position after landing, which he felt reduced directional response to both the aerodynamic rudder and the steerable tail wheel. Then, when the aircraft began to veer to the left, he attempted to go around, but the application of power caused the aircraft to veer harder to the left into a fully developed ground loop. The right wingtip contacted the ground which caused the wing fuel tank to start leaking. The fuel was subsequently ignited and consumed the aircraft. The aircraft was destroyed by fire following a ground loop during a touch-and-go landing. The pilot stated that he did not place the elevator in the full up position after landing, which he felt reduced directional response to both the aerodynamic rudder and the steerable tail wheel. When the aircraft began to veer to the left, he added full power in an attempt to go around, which torqued the aircraft into a fully developed ground loop. During the ground loop, the right wingtip contacted the ground which caused the wing fuel tank to start leaking. The fuel was subsequently ignited and the fire consumed the aircraft. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_LAX97LA203.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
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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.
- AOPA Air Safety Institute 2020 · Safety advisor
Safety Advisor: Aircraft Icing
Safety advisor on in-flight airframe icing in piston GA aircraft. Covers icing physics, identification of structural vs induction vs carb ice, escape strategies (climb / descend / 180), use of weather…
- 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…
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