SEA01LA107
2001-05-30 · Gardiner, Montana, United States · None · 1 aircraft · Status: Completed
Airport 29S
Current FAA registration · N2361S
- Make / Model
- ROTARY AIR FORCE MARKETING RAF 2000 GTX SE
- Engine
- SUBARU ALL MDLS A/B (400 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 20010127
- ADS-B equipped
- Yes — Mode-S A22156
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to rotate the aircraft until he was well past the normal takeoff rotation speed, and his abrupt rotation at this higher speed.
Factual narrative
On May 30, 2001, approximately 0800 mountain daylight time, an experimental Herriford RAF 2000 gyrocopter, N2361S, collided with the terrain during an attempted takeoff at Gardiner Airport, Gardiner, Montana. The private pilot, who was the sole occupant, was not injured, but the aircraft, which was owned and operated by the pilot, sustained substantial damage. The local 14 CFR Part 91 recreational flight was taking place in visual meteorological conditions. No flight plan had been filed. According to the pilot, he inadvertently allowed the gyrocopter to remain on the ground too long during the takeoff roll by applying excessive forward cyclic. Because it was accelerating, the aircraft reached a speed greater than that at which it should have lifted off. When the pilot realized the aircraft's speed was such that it should have already lifted off, he rotated too rapidly, stalling the main rotor blades. The blades immediately flexed downwards, impacting the ground and severing the aircraft's tail. During the takeoff roll, the pilot failed to rotate the gyrocopter until he was well past the normal takeoff rotation speed. When he did rotate, he did so abruptly, causing the rotor blades to stall. The blades then flapped downwards, impacting the terrain and cutting the tail off the aircraft. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_SEA01LA107.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…