CEN21LA095
2020-12-20 · Morris, Illinois, United States · Minor · 1 aircraft · Status: Completed
Airport C09
Current FAA registration · N3264U
- Make / Model
- ROBINSON HELICOPTER R44
- Engine
- LYCOMING O-540-F1B5 (260 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20070507
- ADS-B equipped
- Yes — Mode-S A38791
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate pedal application during liftoff with a tailwind, which resulted in a loss of yaw control and a subsequent impact with terrain.
Factual narrative
The pilot stated that he had initially completed pickups and set downs on four different headings, then departed the area for a local flight. When he returned to the airport, he again practiced pickups and set downs in the same spot on the ramp, and the wind was from the west as he completed these maneuvers. During the final maneuver, the wind shifted, and he lost control of the helicopter. There were three weather observations recorded from around the accident time and the wind was from 240° to 250° at 6 to 7 knots, with no reported gusts. An airport surveillance video showed that during accident sequence, the helicopter was facing east when it briefly touched down and wobbled, then lifted up as the tail boom swung around in a clockwise direction. The tail rotor impacted the ramp then climbed and continued to rotate. The helicopter completed about 1.5 rotations as it descended and impacted the ground and rolled onto its right side. The helicopter manufacturer had previously issued a safety notice for unanticipated yaw, which stated in part, “A pilot's failure to apply proper pedal inputs in response to strong or gusty winds during hover or low-speed flight may result in an unanticipated yaw…To avoid unanticipated yaw, pilots should be aware of conditions (a left crosswind, for example) that may require large or rapid pedal inputs.” The accident is consistent with the inadequate pedal application during the liftoff with a tailwind, which resulted in a loss of yaw control and a subsequent impact with terrain. The pilot reported that there were no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Yaw control-Not attained/maintained
- — Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Decision related to condition
Verbatim from NTSB's published report. Source file
NTSB_2020_CEN21LA095.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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