NTSB CAROL · Event
Event LAX03CA274
Aircraft involved
Probable cause & findings
the student pilot's inappropriate remedial action through the application of excessive aft cyclic during a run-on landing. A factor in the accident was the student's disregard for company procedures.
Factual narrative
On September 1, 2003, about 1720 Pacific daylight time, a Bell 47D-1, N64580, main rotor struck the tail boom while the pilot was attempting a run-on landing at Chino Airport, Chino, California. Zemlock Helicopters was operating the helicopter under the provisions of 14 CFR Part 91. The student helicopter pilot, who possessed an airplane private pilot certificate, was not injured. The helicopter sustained substantial damage. Visual meteorological conditions prevailed, and no flight plan had been filed. The pilot reported in a written statement that he was practicing run-on landings. During the second landing, the right skid dug into the dirt and the main rotor made contact with the tail boom. The pilot did not report any mechanical problems prior to the accident. The pilot had an estimated 2,024 hours of total flight time; approximately 58 of those hours were in helicopters, with 7 logged as pilot-in-command. The Safety Board investigator-in-charge interviewed the helicopter operator. The operator stated that the pilot was practicing run-on landings. During the accident landing, he touched down on the heels of the skids. The helicopter rocked forward and the pilot pulled back on the cyclic. The main rotor blades made contact with the tail boom. The operator also noted that the student was not allowed to practice run-on landings without an instructor on board. The helicopter's main rotor struck the tail boom while the pilot was practicing a run-on landing. While the student pilot was attempting to execute a landing, he touched down on the heels of the skids. The helicopter rocked forward and the pilot pulled back on the cyclic. As a result, the main rotor blades made contact with the tail boom. No mechanical problems were noted with the helicopter. The student pilot had accumulated about 58 hours in helicopters, with 7 as pilot-in-command. The operator reported that students were not permitted to practice run-on landings during solo flight. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_LAX03CA274.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.
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