ERA14CA055
2013-11-28 · Tunica, Mississippi, United States · None · 1 aircraft · Status: Completed
Airport UTA
Current FAA registration · N44DQ
- Make / Model
- ROBINSON HELICOPTER R44 II
- Year of manufacture
- 2005 · 8 years old at event
- Engine
- LYCOMING IO-540 SER (300 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20050713
- ADS-B equipped
- Yes — Mode-S A5489E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's failure to maintain control of the helicopter during the attempted takeoff, and the flight instructor's inadequate supervision of the student pilot.
Factual narrative
The flight instructor and the student pilot were practicing hovering autorotation maneuvers in a helicopter. Following a successful autorotation, and while the helicopter was on the ground with the collective pitch control fully lowered, the pilot told the student, "let's do another one." The flight instructor planned to remind the student pilot to center the anti-torque pedals, as some right pedal was still applied following the preceding autorotation. Before he could do so, the student pilot rapidly increased the engine throttle and the helicopter began yawing to the right. In order to keep the helicopter from sliding along the ground, the student forcefully increased the collective pitch. The helicopter lifted off the ground instantly and the flight instructor advised the student pilot, "I have controls." The student subsequently "locked up on the controls" and inadvertently applied full left anti-torque pedal as he attempted to brace himself. The helicopter yawed rapidly while in the air and the tail of the helicopter struck the ground, resulting in substantial damage. The flight instructor eventually regained control of the helicopter, reduced the throttle to idle, and performed a successful autorotation. The flight instructor and the student pilot were practicing hovering autorotation maneuvers in a helicopter. Following a successful autorotation, and while the helicopter was on the ground with the collective pitch control fully lowered, the pilot told the student, "let's do another one." The flight instructor planned to remind the student pilot to center the anti-torque pedals, as some right pedal was still applied following the preceding autorotation. Before he could do so, the student pilot rapidly increased the engine throttle and the helicopter began yawing to the right. In order to keep the helicopter from sliding along the ground, the student forcefully increased the collective pitch. The helicopter lifted off the ground instantly and the flight instructor advised the student pilot, "I have controls." The student subsequently "locked up on the controls" and inadvertently applied full left anti-torque pedal as he attempted to brace himself. The helicopter yawed rapidly while in the air and the tail of the helicopter struck the ground, resulting in substantial damage. The flight instructor eventually regained control of the helicopter, reduced the throttle to idle, and performed a successful autorotation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Student pilot - C
- C Personnel issues-Psychological-Attention/monitoring-Monitoring other person-Instructor/check pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2013_ERA14CA055.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.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (icing). All research papers
- arXiv 2026 · arXiv preprint Enabling Beyond-Visual-Line-of-Sight Drones Operation over Open RAN 5G Networks with Slicing
Among the foretold claims of the transition from 5G to 6G, Beyond-Visual-Line-of-Sight (BVLoS) drone operation has emerged as a prominent Internet-of-Robots enabler.
- 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…
- 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…
- 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…
- 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…