NTSB CAROL · Event
Event MIA94GA072
Aircraft involved
Probable cause & findings
FAILURE OF THE PILOT-IN-COMMAND TO USE CARBURETOR HEAT DURING A POWEROFF AUTOROTATION, RESULTING IN THE ENGINE NOT RESPONDING TO THROTTLE INPUT DURING RECOVERY DUE TO CARBURETOR ICE BUILDUP.
Factual narrative
On February 14, 1994, at 1520 eastern standard time, a Robinson R22 Beta, N591PD, registered to the City of Fort Lauderdale, landed hard at Pompano Beach Airpark, Pompano Beach, Florida, following loss of engine power during recovery from a autorotation landing. The flight was a 14 CFR Part 91, public-use flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft received substantial damage and the airline transport-rated flight instructor was not injured. The commercial-rated dual student received minor injuries. The flight originated at Fort Lauderdale, Florida, on February 14, 1994, about 1445. Both pilots stated the instructor pilot was demonstrating a 180-degree autorotation with power recovery. The dual student was following on the flight controls. They had completed two previous autorotations. As they flared at the completion of the autorotation they heard the engine running at idle; however, when they applied power to recover, the engine did not respond. The helicopter touched down hard and the main rotor blades severed part of the tailboom and the tail rotor. The helicopter spun to the left several rotations and the right skid collapsed. The helicopter came to rest upright, leaning to the right. They stated the engine was at idle power for about 30 to 40 seconds during each autorotation and that they were not applying carburetor heat. After the accident the main rotor blades were removed and the tail rotor drive was disconnected from the transmission. The engine was started and operated to 3,000 rpm where it ran rough and popped. A magneto check was performed and the right magneto had over a 200 rpm drop. The left mag had a normal drop. The no. 2 cylinder bottom plug, which operates off the right magneto, was found to be fouled by oil and the ignition lead was not firing. All cylinders developed normal compression. The engine was removed from the helicopter and the exhaust valve guide clearance was measured. The nos. 1, 2, and 4 exhaust valve guides were found worn beyond maximum limits. No 3 cylinder exhaust valve guide was at maximum limit. The engine was placed in a test cell and operated to maximum power with no evidence of failure or malfunction. During initial running the carburetor fuel shutoff needle valve stuck partially open. This corrected itself shortly after start of the engine run. The no. two cylinder bottom spark lead from the right magneto operated normally during this test run. A review of carburetor icing probability curves indicate that for the conditions present at the time of the accident, temperature 72 degrees F and dewpoint temperature 55 degrees F, the helicopter was operating in conditions conducive to serious icing at glide power. The FAA approved flight manual for the Robinson R22 states " when conditions conducive to carburetor ice are known or suspected, such as fog, rain, high humidity, or when operating near water, use carb heat as follows: during autorotation or reduced power below 18 inches MP apply full Carb Heat regardless of CAT gage temperature." See attached icing probability curves and pages from the Robinson Flight Manual. Both pilots stated they were performing their third 180-degree autorotation with power recovery. They were not using the carburetor heat. They heard the engine running as they began the recovery but the engine did not respond to throttle input. The helicopter touched down hard and the main rotor blades contacted the tail boom and severed it and the tail rotor. The helicopter spun to the left several times and the right skid collapsed before the helicopter came to rest upright. After the accident the engine was operated in the helicopter and also in a test cell with no evidence to indicate failure or malfunction. At the time of the accident the helicopter was operating in conditions conducive to serious carburetor icing at glide power. The flight manual for the helicopter requires use of carburetor heat when operating in conditions conducive to carburetor icing. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_MIA94GA072.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 ↗