NTSB CAROL · Event
Event NYC02TA029
Registry · N361KA
FAA Aircraft Registry record.
Make / Model
BEECH 200
Year of manufacture
1980 · 21 years old at event
Engine
P&W CANADA PT6A-60A (1050 hp)
Seats / Engines
11 seats · 2 engines
Last airworthiness date
19800910
ADS-B equipped
Yes — Mode-S A410E5
Registrant of record
BEHRENS INVESTMENTS OF WISCONSIN LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain aircraft control while hovering. A factor related to the accident was the pilots lack of experience in type of aircraft.
Factual narrative
On November 14, 2001, about 1543 eastern standard time, a Kaman K-1200 helicopter, N361KA, operated by the United States Department of State, was substantially damaged after impacting the ground during a practice hovering autorotation, at the Kaman Aerospace Corporate Heliport, Bloomfield, Connecticut. The certificated commercial pilot sustained minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the instructional flight conducted under 14 CFR Part 91. According to the pilot, he had just completed a solo hovering autorotation. During the autorotation, he recalled being slow to apply aft cyclic, but the maneuver was completed satisfactory. He then began a second hovering autorotation. As the helicopter descended toward the ground, the pilot applied aft cyclic, and the helicopter began to drift rearward. The pilot increased the collective to stop the decent, and began to concentrate on the aft drift, when the helicopter touched down on the right main and nose landing gear. The pilot added left cyclic to level the helicopter, but due to low rotor rpm, the control input had little effect. The helicopter began to roll to the right, and the main rotor blades impacted the ground. The helicopter came to rest on its right side. According to the pilot's flight instructor, the accident flight was the pilot's fifth flight of the day, with the first four dual instructional flights being conducted in a Kaman H-43. The last flight was to be conducted solo in the K-1200. The pilot had previously flown the K-1200 four times. As the flight instructor observed the flight from the ground, he requested the pilot begin practicing hovering autorotations. The pilot positioned the helicopter into the wind, and from a 5-foot hover, performed a hovering autorotation. During the maneuver, the pilot maintained "good" directional control, "but was slow raising the nose" of the helicopter as it descended, and touched down first on the nose wheel, then the main landing gear. After discussing the maneuver over the radio, the flight instructor and pilot agreed the nose of the helicopter needed to be raised sooner, to allow the helicopter to land in a level attitude. The pilot then set up and commenced his second practice hovering autorotation. Once again, the nose of the helicopter dropped downward. As the nose wheel touched down, the helicopter began to rock backwards onto its main landing gear, with the nose rising back into the air. The helicopter rocked forward, and tilted to the right, with the right main and nose gear on the ground. The helicopter remained in the tilted position and the instructor radioed to the pilot "to lower the collective," but received no response. About 5 seconds later, the helicopter continued to slowly roll over onto its right side. The main rotor blades impacted the pavement and the helicopter came to rest with the engine running. The pilot evacuated, and once the remaining portions of the main rotor blades stopped turning, the flight instructor ran to the wreckage, and secured the engine. The recorded weather at a nearby airport, about the time of the accident, included winds from 210 degrees at 7 knots. As the helicopter descended towards the ground during hovering autorotation maneuvers, the pilot applied aft cyclic, and the helicopter began to drift rearward. The pilot increased the collective to stop the decent, and began to concentrate on the aft drift, when the helicopter touched down on the right main and nose landing gear. The pilot added left cyclic to level the helicopter, but due to low rotor rpm, the control input had little effect. The helicopter began to roll to the right, and the main rotor blades impacted the ground. The helicopter came to rest on its right side. According to the pilot's flight instructor, the accident flight was the pilot's fifth flight of the day, with the first four dual instructional flights being conducted in a Kaman H-43. The last flight was to be conducted solo in the K-1200. The pilot had previously flown the K-1200 four times. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_NYC02TA029.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 ↗