Aviation Accident Summaries

Aviation Accident Summary DEN05LA082

Provo, UT, USA

Aircraft #1

N553SH

Robinson R22 Beta

Analysis

The flight instructor and student pilot were practicing hovering with the student controlling the cyclic. The helicopter began to oscillate and drift to the right. The student put in more right cyclic and then released the controls when the LOW ROTOR RPM warning sounded. The instructor took the controls and attempted to recover but the aircraft struck terrain and rolled over. Damage to the aircraft included a severed tail boom, shattered windscreen, buckled rotor mast, and wrinkled skin.

Factual Information

On May 23, 2005, at 1210 mountain daylight time, a Robinson R22 Beta, N553SH, operated by Silver State Helicopters and flown by a student pilot under the supervision of a commercial certificated flight instructor, was substantially damaged during an uncontrolled descent and impact with terrain near Provo, Utah. Visual meteorological conditions prevailed at the time of the accident. The local instructional flight was being conducted under the provisions of 14 CFR Part 91 without a flight plan. The student pilot was not injured, but the flight instructor sustained minor injuries. The flight originated at Provo, Utah. The flight instructor said that they were practicing hovering and the student had control of the cyclic. The helicopter began to oscillate and drift to the right. The student put in more right cyclic control, and then released the controls when the LOW ROTOR RPM warning sounded. The instructor "pulled collective and hard left cyclic" in an attempt to regain control of the aircraft but was unsuccessful, and the helicopter impacted terrain and rolled over. FAA investigators said the tail boom was severed, the main rotor was bent and separated from the engine, the rotor mast torsionally buckled, the windscreen was shattered, and the skin was wrinkled. The winds at the Provo airport, located 15 miles northeast of the accident site, at the time of the accident were 290 degrees at 6 knots and the instructor noted light turbulence.

Probable Cause and Findings

the dual student’s failure to maintain adequate rotor rpm and the inadequate supervision by the instructor.

 

Source: NTSB Aviation Accident Database

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