N462BARobinson Helicopter R44 II · 2008

The purpose of the flight was aerial animal control. The pilot reported that while flying at about 30kts and 50 ft above the ground and during a sweeping turn to avoid the effects of an estimated 30 kt tailwind at low altitude, a strong wind gust occurred in the path of the tailwind, which led to an uncontrolled descent rate. Unable to arrest the descent rate, the pilot executed a run-on landing. Environmental conditions weakened the pilot’s depth perception, which resulted in a tail strike that sheared off the tail boom. The main rotor blades contacted the ground and the helicopter rolled on its side, substantially damaging the fuselage and tail boom. The pilot reported that there were no mechanical failures or malfunctions with the helicopter that would have precluded normal operation.