Aviation Accident Summaries

Aviation Accident Summary CEN10CA417

Shreveport, LA, USA

Aircraft #1

N721BB

ROBINSON HELICOPTER COMPANY R44 II

Analysis

According to a written statement provided by the student helicopter pilot, he was practicing "sit downs and pick ups" to a grass field. The helicopter "sat down" uneventfully and the student pilot reduced power to chat with a friend. Shortly thereafter, the student pilot added power, ensured that all engine instruments were in the green, and attempted a takeoff. The student pilot detected a tailwind and applied left pedal correction; however, the helicopter yawed to the right one full rotation before the student pilot was able to set the helicopter back down. During the hard landing the horizontal stabilizer was bent, both tail rotor blades were damaged, the tail boom was wrinkled, and the fuselage was wrinkled on the right side. An examination of the helicopter and its related systems, conducted by a Federal Aviation Administration inspector, revealed no preexisting anomalies.

Factual Information

According to a written statement provided by the student pilot, he was practicing "sit downs and pick ups" to a grass field. The helicopter "sat down" uneventfully and the student pilot reduced power to chat with a friend. Shortly thereafter, the student pilot added power, ensured all engine instruments were in the green, and attempted a takeoff. The student pilot detected a tailwind and applied left pedal correction; however, the helicopter yawed to the right one full rotation before the student pilot was able to set the helicopter back down. During the hard landing the horizontal stabilizer was bent, both tail rotor blades were damaged, the tail boom was wrinkled, and the fuselage was wrinkled on the right side. An examination of the helicopter and its related systems, conducted by a Federal Aviation Administration inspector, revealed no anomalies.

Probable Cause and Findings

The student pilot's failure to maintain control of the helicopter during takeoff, resulting in a loss of tail rotor effectiveness and a subsequent hard landing.

 

Source: NTSB Aviation Accident Database

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