Casualties unknown

Helicopter Damaged During Run-on Landing After Practice Autorotation (N8968F)

Wichita, KS, US

On April 7, 2003, a Schweizer 269C (registration N8968F) was involved in an aviation accident near Wichita, KS. Investigators recorded the probable cause as: 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. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

During a practice autorotation, a helicopter sustained substantial damage when the tailboom was severed by the main rotor after the nose pitched forward on landing. The grass landing area was smooth, firm, and dry. No malfunctions were reported.

Accident Overview

The helicopter was substantially damaged during a run-on landing that followed a practice autorotation. According to the flight instructor, as the helicopter touched down, it rotated forward, lifting the tailboom into the path of the main rotor, which then severed the tailboom. The aircraft subsequently turned left by approximately 90 degrees before coming to a stop.

Pilot Accounts

The instructor was demonstrating a full touchdown autorotation leading to a run-on landing on a grass area adjacent to a paved runway. The dual student reported that the initial touchdown was light and that the helicopter did not decelerate quickly until near the end of the ground run. Both pilots described the grass landing area as smooth, firm, and dry. Neither pilot reported any malfunctions with the helicopter or its engine prior to the accident.

Operational Guidance

The pilot's flight manual includes a caution: "Avoid rapid lowering of collective pitch control after ground contact." Additionally, the FAA Rotorcraft Flying Handbook notes that during a running landing, increased ground friction when lowering the collective can cause the helicopter's nose to pitch forward. It advises caution against correcting this pitch with aft cyclic, as such a movement could result in the rotor making contact with the tailboom.

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.