NTSB CAROL · Event
Event CHI99TA232
Aircraft involved
Probable cause & findings
the pilot-in-command's improper autorotational landing.
Factual narrative
On July 13, 1999, at 0913 central daylight time, a Hughes OH-6A, N911EP, sustained substantial damage during an autorotational landing to the surface. The pilot and check pilot reported no injuries. The public use flight was operating under provisions of 14 CFR Part 91 in visual meteorological conditions. No flight plan was on file. The local flight departed at 0830. The flight was for the purpose of the pilot-in-command receiving a check ride from a check pilot (flight instructor). In a verbal statement given to a Federal Aviation Administration inspector, the check pilot said that the pilot had been practicing various landings including autorotational landings to a hover. He said that on the seventh landing he told the pilot to "demonstrate a full touchdown." He said the helicopter touched down hard and the main rotor blade contacted and cut through the tail boom. A post accident examination failed to reveal any pre-existent mechanical anomalies. A rated helicopter pilot was acting as pilot-in-command with a check pilot. According to the check pilot who was interviewed after the accident, the pilot-in-command had accomplished several autorotational landings to a hover and he asked the pilot on the next one to 'demonstrate a full touchdown.' He said that the helicopter landed hard and received damage. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_CHI99TA232.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 ↗