Bountiful, UT, USA
N47WH
ROBINSON HELICOPTER COMPANY R22
While performing a simulated power-off autorotation with a power recovery, the certified flight instructor (CFI) and student noted that the main rotor rpm was decaying. About 150 to 200 feet above ground level (agl), the instructor took the flight controls, executed a flare about 50 feet agl, and realized that the helicopter was going to settle. The instructor then attempted a run-on landing, but the helicopter landed hard, spreading the skid landing gear and damaging the rotors, frame, engine and transmission. The helicopter then slid about 75 feet down the runway, departed the runway surface, and rolled four times before coming to rest on its left side. The CFI stated that there were no mechanical problems with the helicopter prior to the accident.
While performing simulated power-off autorotations with a power recovery, the certified flight instructor (CFI) and student noted that the main rotor rpm was decaying. About 150 to 200 feet above ground level (agl), the CFI took the flight controls and executed a flare about 50 feet agl, and realized the helicopter was going to settle. The CFI then attempted a run on landing, but the helicopter landed hard, spreading the skid landing gear. The helicopter then slid about 75 feet down the runway, departed the runway surface, and rolled four times before coming to rest on its left side. The CFI stated that there were no mechanical problems with the helicopter.
The student’s failure to maintain adequate rotor rpm and the flight instructor’s delayed remedial action, which resulted in a hard landing.
Source: NTSB Aviation Accident Database
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