Casualties unknown

Helicopter Rolls Over During Student Practice Autorotation Landing (N1093Y)

Spring House, PA, US

On August 10, 1983, a Hughes 269C (registration N1093Y) was involved in an aviation accident near Spring House, PA. Investigators recorded the probable cause as: The student pilot's excessive cyclic control input just prior to touchdown during a practice autorotation landing, which resulted in the helicopter rolling onto its side after the tail rotor struck high grass. 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

A training helicopter rolled onto its side during a practice autorotation landing when the student pilot overrode the controls with excessive cyclic input just before touchdown.

What happened

The accident occurred during a flight training session involving a practice demonstration of an autorotation landing. The certified flight instructor (CFI) was initially controlling the aircraft while the student pilot monitored and prepared to take over. As the helicopter approached the ground for the simulated landing, the student pilot took control of the cyclic stick.

According to the instructor's account, the student applied excessive forward or lateral cyclic input just prior to touchdown. This abrupt control input caused the helicopter to roll sharply to the right. The tail rotor blade struck tall grass on the ground, which arrested its rotation and contributed to the loss of directional control. The force of the impact with the vegetation caused the main rotor system to contact the ground, resulting in the helicopter rolling over completely onto its side.

The investigation

Examination of the site revealed that the terrain consisted of high grass, which played a critical role in the final moments of the accident sequence. The tail rotor struck this vegetation, preventing normal yaw control and facilitating the rollover. No mechanical failures were reported as contributing factors; the event was attributed entirely to pilot input during the landing phase.

Findings

The primary factor leading to the accident was the student pilot's excessive cyclic control input during the critical low-altitude phase of the autorotation landing. The timing of this input, just before touchdown, left insufficient altitude or time for recovery. The presence of high grass at the landing site exacerbated the situation by striking the tail rotor, which prevented corrective action and ensured the helicopter rolled onto its side.

Safety message

Student pilots must be closely monitored during autorotation practice to ensure smooth control inputs. Excessive cyclic movement near the ground can lead to loss of control, especially when combined with environmental factors like tall grass that may interfere with tail rotor effectiveness.

Probable cause

The student pilot's excessive cyclic control input just prior to touchdown during a practice autorotation landing, which resulted in the helicopter rolling onto its side after the tail rotor struck high grass.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X44325. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.