Casualties unknown

2000-12-17: Robinson R22 (N7187W) — Sunnyvale, TX

Sunnyvale, TX, US

On December 17, 2000, a Robinson R22 (registration N7187W) was involved in an aviation accident near Sunnyvale, TX. Investigators recorded the probable cause as: The flight instructor's inadequate supervision of his student and his failure to maintain control of the helicopter. Factors were the student pilot allowing the airspeed and main rotor RPM to get too low during the simulated emergency. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

During a training flight, a student performed an autorotation after a simulated engine failure. The instructor took control at 100 feet AGL, attempted a power recovery, but the helicopter rolled over after uncontrolled movements.

Sequence of Events

While en route at 1,000 feet above ground level (AGL), the instructor pilot simulated an engine failure over a field and directed the student to execute an autorotation with a power recovery. The student pilot performed a gradual 360-degree turn while descending toward the field. According to the instructor, the student leveled the helicopter on final approach.

The instructor conducted a final scan for obstacles and then looked back into the cockpit. At that moment, the airspeed was 45 knots and the main rotor RPM was at the bottom of the green arc (approximately 97%). The helicopter was about 100 feet AGL when the instructor took over control and attempted a "high power recovery."

Instructor's Actions

The instructor rolled on the throttle and pulled up on the collective. He felt a "slight hesitation," after which the helicopter "snapped to the right." The instructor then applied left pedal and heard the low rotor RPM warning horn. The instructor stated that he believed the helicopter did not touch down level due to the rotation to the right.

The helicopter touched down in the field, then "hopped to the right approximately 40 degrees" and became airborne again. The instructor stated that he thought he still had full throttle applied and/or the collective raised. As the helicopter became airborne, it rotated 360 degrees to the right, contacted the ground with the tail rotor, and then with the right skid. Subsequently, the helicopter rolled over onto its right side.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001226X45485. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.