NTSB CAROL · Event
Event FTW03LA122
Registry · N86238
FAA Aircraft Registry record.
Make / Model
ENSTROM F-28F
Year of manufacture
1985 · 18 years old at event
TCDS
H1CE · ENSTROM HELICOPTER CORP THE
Engine
LYCOMING HIO-360 SER (205 hp)
Seats / Engines
3 seats · 1 engine
Last airworthiness date
19850425
ADS-B equipped
Yes — Mode-S ABD927
Registrant of record
CRAWFORD THOMAS P
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain control of the helicopter. A contributing factor was the crosswind.
Factual narrative
On April 5, 2003, approximately 1113 central standard time, an Enstrom F-28F single-engine helicopter, N86238, was substantially damaged following a loss of aircraft control while hovering at the Monroe Regional Airport (MLU) near Monroe, Louisiana. The helicopter was registered to Tinwood Industries, Inc., of Monroe, and operated by Hanger One, also of Monroe. The private pilot rated student, sole occupant of the helicopter, was not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 instructional flight. The local solo flight originated from MLU, at 1010. The 221-hour private pilot rated student reported on the Pilot/Operator Aircraft Accident Report Form (6120.1/2), he was on his second helicopter solo flight and had completed several touch-and-go landings. While practicing hovering over taxiway Hotel, with the helicopter facing into the wind, the pilot initiated a left hovering turn. As the helicopter was turning to face downwind, it became unstable, and the pilot turned the helicopter back into the wind. During a second left hovering turn, and as the nose of the helicopter was 90-110 degrees from the wind, the pilot lost control of the helicopter. The right skid impacted the ground, and the helicopter came to rest on its left side. Examination of the helicopter, by the FAA inspector who responded to the accident site, revealed that the main rotor blades, tail rotor blades, and left horizontal stabilizer were damaged. The right skid was found separated from the fore and aft cross tubes, and the left side of the fuselage sustained structural damage. At 1053, the weather facility at MLU, reported that the wind was from 060 degrees at 8 knots, 10 statute miles visibility, few clouds at 9,500 feet, and an altimeter setting of 30.04 inches of Mercury. The temperature was 69 degrees Fahrenheit, and the dew point was 52 degrees Fahrenheit. The student pilot had acucmulated a total of 19.7 hours in helicopters. The helicopter student pilot reported he was on his second helicopter solo flight and had completed several touch-and-go landings. While practicing hovering over the taxiway, with the helicopter facing into the wind, he initiated a left hovering turn. As the helicopter was turning to face downwind, it became unstable, and the pilot turned the helicopter back to facing the wind. During a second left hovering turn, and as the nose of the helicopter was 90-110 degrees from the wind, the pilot lost control of the helicopter. The right skid hit the ground, and the helicopter came to rest on its left side. The pilot had accumulated a total of 19.7 hours in helicopters. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_FTW03LA122.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 ↗