Incident Overview
A helicopter encountered a dynamic rollover while the pilot was attempting to take off. The tie-down strap, which was still attached, did not give way as the aircraft began to lift off. This caused the helicopter to roll over to the right and subsequently impact the ground.
Post-Accident Examination
An examination of the wreckage conducted by the operator revealed structural damage to the right side of the helicopter. The rotor blades were completely destroyed, and the right skid was entirely detached from the aircraft.
Inspection Findings
According to the Federal Aviation Administration (FAA) inspector who responded to the accident site, the tie-down strap on the right skid had not been properly removed prior to the takeoff attempt. This oversight allowed the strap to remain secured during the flight, preventing the skid from freeing itself and contributing to the dynamic rollover.
Aircraft Condition
The helicopter sustained significant damage as a result of the rollover and ground impact. The right side structure bore the brunt of the force, with the skid and rotor system suffering extensive destruction.