Robinson R22T10 accident near runway

Casualties unknown • Wichita, KS, US

A Robinson R22T10 sustained significant damage during a running landing following an instructor-led demonstration of a full touchdown autorotation.

What happened

During a flight training session, the pilot was demonstrating a full touchdown autorotation transitioning into a running landing on a grass area adjacent to a paved runway. The aircraft touched down lightly and continued along the ground. As the ground run progressed, the helicopter's nose pitched forward, causing the tailboom to rotate into the path of the main rotor.

The investigation

Investigators examined the aircraft and the flight conditions. The instructor reported that the forward pitch of the aircraft caused the main rotor to make contact with the tailboom, resulting in its severance. The students involved in the demonstration noted that the initial touchdown was light and that the helicopter did not experience rapid deceleration until the end of the ground run.

Findings

  • The Robinson R22T10 sustained damage including a severed tailboom.
  • There were no injuries reported among the crew members.
  • The landing area was characterized as smooth, firm, and dry.
  • No malfunctions of the engine or helicopter were reported prior to the accident.
  • A critical factor in the accident was the pilot's movement of the collective pitch control; the aircraft's flight manual specifically cautions against the rapid lowering of the collective pitch after ground contact.

Frequently asked questions

What happened in the 2003-04-07 Schweizer 269C accident near Wichita, KS?

A Robinson R22T10 sustained significant damage during a running landing following an instructor-led demonstration of a full touchdown autorotation.

What aircraft was involved and where did it happen?

The accident on 2003-04-07 involved a Schweizer 269C, registration N8968F, at Wichita, KS.

What was the probable cause of the accident?

The premature lowering of the collective and the improper use of the cyclic during the run-on landing performed by the flight instructor, as well as the main rotor/tail boom contact. Contributing factors were the intentional run-on landing, the grass landing surface and the severed tail boom.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030410X00479. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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