SCHWEIZER(HUGHES)AIRCRAFT CORP TH55A/269A

Grinnell, IA — June 26, 2012

Event Information

DateJune 26, 2012
Event TypeACC
NTSB NumberCEN12CA402
Event ID20120628X22112
LocationGrinnell, IA
CountryUSA
Coordinates41.70583, -92.73473
AirportGrinnell
Highest InjuryNONE

Aircraft

MakeSCHWEIZER(HUGHES)AIRCRAFT CORP
ModelTH55A/269A
CategoryHELI
FAR Part091
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious0
Minor0
None2
Total Injured0

Event Location

Probable Cause

The pilot’s inadequate compensation for the wind during a hovering maneuver, which resulted in a loss of tail rotor effectiveness and directional control.

Full Narrative

The pilot and his passenger were returning to the airport after a local flight. In preparation to land, the pilot approached a grassy area adjacent to the runway and entered a hover into a 12 knot wind. The wind was also gusting to 16 knots. The pilot then made a right pedal turn downwind. He said that during the turn, the wind caught the tail and the helicopter began to spin. The pilot did not have enough left pedal to stop turning and the tailrotor struck a fence and the main rotor blades hit the ground. A review of photographs taken of the helicopter after the accident revealed the tail rotor blades, main rotor blades, and fuselage were substantially damaged. The pilot reported no mechanical malfunctions prior to the accident.

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

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