Pilot Debrief

ROBINSON HELICOPTER R44 near Johnson, KS — 2021-04-05

Final reportCEN21LA184
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Date
2021-04-05
Location
Johnson, KS, USA
Aircraft
ROBINSON HELICOPTER R44
Registration
N8348X
Category
Helicopter
Highest injury
None
Fatalities
0
Phase of flight
Hover

Probable cause

The pilot's inadequate pedal application during a transition to hover, which resulted in a loss of yaw control and a subsequent impact with terrain.

NTSB narrative

The pilot was flying over his wheat fields as the wind was from the south at 10 knots. The pilot transitioned to a hover close to the ground and experienced a sudden unanticipated yaw to the left. The helicopter completed more than one full rotation to the left, then landed hard in the field and sustained substantial damage to the main rotor blades and fuselage. Examination of the helicopter and flight control system did not reveal any preimpact mechanical malfunctions or anomalies that would have precluded normal operation. 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.” Given that the postaccident examination of the helicopter did not reveal any preimpact anomalies and the 10-knot wind at the time of the accident, it is likely that the pilot did not apply adequate pedal input to avoid the loss of yaw control while transitioning to a hover.

Analysis

Primary failure mode
Loss of control
First missed decision gate
Pilot could have applied proper pedal inputs to prevent unanticipated yaw.

NTSB coding

Evidence available

  • Photos
  • 6 docket documents
View NTSB final reportView NTSB docket

Docket documents6

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