TOMBALL, TX, USA
N515EH
BELL 206L-1
ACFT WAS SUBSTANTIALLY DAMAGED AS A RESULT OF A HARD LANDING DURING AN EMERGENCY AUTOROTATION FOLLOWING A COMPLETE POWER LOSS. THE POWER LOSS OCCURRED AS A RESULT OF AN UNCONTAINED FAILURE OF THE NO. 1 TURBINE WHEEL. THE WHEEL BURST AS A RESULT OF 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. THE ORGIN OF THE FATIGUE FRACTURE WAS FOUND IN THE SCALLOP AREA ON THE TURBINE END OF THE SHAFT. THE ENG FAILURE OCCURRED AT LOW ALTITUDE ON DEPARTURE AND THE PLT HAD TO MANEUVER THE ACFT IN ORDER TO MAKE THE ONLY AVAILABLE FORCED LANDING AREA.
Source: NTSB Aviation Accident Database
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