Overview
An aircraft experienced a complete power loss during departure, leading to an emergency autorotation and a hard landing that resulted in substantial damage to the aircraft. The power loss occurred at low altitude, and the pilot was required to maneuver the aircraft to the only available forced landing area.
Engine Failure
The power loss was caused by an uncontained failure of the No. 1 turbine wheel. The wheel burst after a fatigue failure of the turbine-to-compressor coupling, which allowed the shaft to decouple. When the turbine section decoupled, the engine experienced an overspeed. Metallurgical examination traced the origin of the fatigue fracture to the scallop area on the turbine end of the shaft.
Emergency Landing
Following the engine failure at low altitude, the pilot maneuvered the aircraft to the only suitable forced landing area. The subsequent autorotation landing was hard, causing substantial damage to the aircraft.