NTSB CAROL · Event
Event NYC95LA126
Registry · N8541E
FAA Aircraft Registry record.
Make / Model
ROBINSON HELICOPTER R22 ALPHA
Year of manufacture
1984 · 11 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
19841005
ADS-B equipped
Yes — Mode-S ABB8B4
Registrant of record
FLYING SERVICES INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's failure to maintain control of the helicopter. The student's lack of experience in the type of operation (solo flight) was a related factor.
Factual narrative
On May 27, 1995, about 1541 eastern daylight time, a Robinson, R- 22A, helicopter, N8541E, collided with the terrain at the Essex County Airport (CDW), Fairfield, New Jersey. The student pilot was not injured. The helicopter was substantially damaged. Visual meteorological conditions prevailed, and no flight plan had been filed. The local, solo, instructional flight was being conducted under 14 CFR Part 91. The student pilot had been practicing hovering and landings in the grass area to the west of runway 04. The pilot said that she was in the area for about 40 minutes and had conducted numerous landings and take offs from the grass. She further stated that she had landed the helicopter and was firmly on the ground when she removed her hand from the throttle and collective, because her hand had become fatigued. Her next recollection was that the helicopter was off the ground, approximately 1 to 2 feet. She did not recall what happened next, except that she was on the ground and had exited the helicopter. The pilot stated that she did not have any mechanical difficulty with the helicopter. The helicopter came to rest on it's right side. The white blade was found approximately 240 feet south of the main wreckage, disconnected from the hub and lying on the east side of runway 04. The other blade with the mast and the pylon was found approximately 100 feet south of the main wreckage. Examination of the helicopter and engine did not reveal any discrepancies. The student pilot's total flight time at the time of the accident was 68.7 hours, of which 55.7 hours were in this make and model helicopter, including 5 hours of solo time. The pilot received her solo endorsement on April 28, 1995. The CDW weather, reported at 1045, was; 5000 feet scattered, visibility 15 miles, wind 360 degrees at 5 knots, temperature 75 degrees F, dew point 47 degrees F, altimeter 30.22 inches Hg. THE STUDENT PILOT HAD BEEN PRACTICING HOVERING AND LANDINGS IN A GRASS AREA WEST OF THE RUNWAY FOR ABOUT 40 MINUTES. AFTER CONDUCTING NUMEROUS LANDINGS AND TAKEOFFS AND WITH THE HELICOPTER FIRMLY ON THE GROUND, SHE REMOVED HER HAND FROM THE THROTTLE AND COLLECTIVE, BECAUSE HER HAND HAD BECOME FATIGUED FROM OPERATING THE CONTROLS. HER NEXT RECOLLECTION WAS THAT THE HELICOPTER WAS OFF THE GROUND, APPROXIMATELY 1 TO 2 FEET. SHE DID NOT RECALL WHAT HAPPENED NEXT, EXCEPT THAT SHE FOUND HERSELF ON THE GROUND OUTSIDE THE HELICOPTER. THE HELICOPTER CAME TO REST ON ITS RIGHT SIDE WITH THE MAIN ROTOR BLADES SEPARATED. THE PILOT STATED THAT SHE DID NOT HAVE ANY MECHANICAL DIFFICULTY WITH THE HELICOPTER. AT THE TIME OF THE ACCIDENT, THE STUDENT PILOT HAD 5 HOURS OF SOLO FLIGHT TIME. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_NYC95LA126.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 ↗