NTSB CAROL · Event
Event SEA95LA065
Registry · N721HH
FAA Aircraft Registry record.
Make / Model
ROBINSON HELICOPTER R22 BETA
Year of manufacture
1990 · 5 years old at event
TCDS
H10WE · ROBINSON HELICOPTER CO
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19900726
ADS-B equipped
Yes — Mode-S A9A7FA
Registrant of record
HAWAII PACIFIC AVIATION INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE DUAL STUDENT PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL OF THE HELICOPTER DURING THE PRACTICE HOVER AUTOROTATION TO LANDING, AND THE FLIGHT INSTRUCTOR'S FAILURE TO ADEQUATELY SUPERVISE THE DUAL STUDENT DURING THE LANDING. CONTRIBUTING TO THE ACCIDENT WAS AN UNFAVORABLE WIND.
Factual narrative
On March 12, 1995, about 0945 Pacific standard time, N721HH, a Robinson R-22 helicopter, operated by Hillsboro Helicopters, Inc., Hillsboro, Oregon, impacted terrain and rolled over while landing in Hillsboro. The helicopter was substantially damaged. The certified flight instructor (CFI) and student pilot were not injured. Visual meteorological conditions prevailed and a flight plan was not filed. The local instructional flight was conducted under 14 CFR 91. According to the CFI, the purpose of the flight was to practice hover autorotations. Immediately prior to the accident, both the CFI and pre-solo student pilot were at the controls. The helicopter was "... into the wind [approximately] 18 - 24 inches above grass on level ground." The CFI further stated: Closed throttle to perform hover auto. Aircraft began to settle and drift left. Full right cyclic was applied as aircraft contacted ground hard with left skid. Collective was lowered and aircraft's momentum seemed to stop. [The helicopter] paused for a second and then continued over on left side. According to an FAA aviation safety inspector from Hillsboro, Oregon, the helicopter rolled over onto its left side, causing substantial damage. No pre-impact mechanical malfunctions were reported. The wind conditions at the airport about five minutes after the accident were reported to be from 180 degrees at 15 knots. THE DUAL STUDENT PILOT AND FLIGHT INSTRUCTOR WERE PRACTICING HOVER AUTOROTATIONS ONTO THE GRASS. IMMEDIATELY PRIOR TO THE ACCIDENT, DIRECTIONAL CONTROL OF THE HELICOPTER WAS LOST WHILE THE DUAL STUDENT WAS RECEIVING INSTRUCTION ON AUTOROTATING TO LANDING FROM A HOVER ABOUT TWO FEET ABOVE THE GROUND. BOTH THE STUDENT AND INSTRUCTOR WERE ON THE CONTROLS AT THE TIME. THE HELICOPTER BEGAN TO DRIFT TO THE LEFT, AND THE FLIGHT INSTRUCTOR USED FULL RIGHT CYCLIC TO CORRECT FOR THE DRIFT. THE HELICOPTER'S LEFT LANDING SKID STRUCK THE GROUND 'HARD' AND THE HELICOPTER ROLLED OVER, CAUSING SUBSTANTIAL DAMAGE. THE WIND WAS BLOWING FROM THE SOUTH AT 15 KNOTS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_SEA95LA065.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 ↗