Accident Details
Probable Cause and Findings
A partial loss of engine power for undetermined reasons.
Aircraft Information
Registered Owner (Historical)
Analysis
According to the instructor, the student pilot was making a practice autorotation to be followed by a powered recovery in preparation for his taking the private pilot practical test. When power was added, only 2500 rpm (revolutions per minute) instead of 3050 rpm was attained. A forced landing ensued and the helicopter slid approximately 2 feet on a rain-soaked field. The skid toes dug into the soft ground, stopping forward movement and causing the fuselage to shift forward. The main rotor blades contacted and severed the tail rotor driveshaft. In addition, the the tail rotor gearbox, tailboom, and a main rotor blade were damaged.
Post-accident examination of the engine and power train revealed no anomalies that would have prevented the engine from producing full power.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09CA257