Helicopter rollover during landing approach

Casualties unknown • Cicero, NY, US

A helicopter experienced a 360-degree rotation and subsequent rollover after the rotor and engine RPM decreased during a landing flare.

What happened

During a landing approach to the runway, the pilot was at the controls while receiving instruction. As the helicopter neared the runway, the pilot flared and leveled the aircraft approximately 3 feet above the ground with no forward airspeed.

At this point, the Certified Flight Instructor (CFI) observed that the engine and rotor RPM began to decrease, causing the helicopter to turn to the left. The CFI took control of the aircraft in an attempt to correct the situation; however, the helicopter underwent a 360-degree rotation. During this maneuver, the left landing skid struck the ground, causing the helicopter to roll onto its left side before coming to rest. There were no injuries reported.

The investigation

An examination of the helicopter and its powerplant revealed no failures occurring prior to the impact. Investigators noted that the right landing skid had separated from the struts and its fasteners had been sheared. Additionally, dirt was found packed into the heel of the skid. The middle and aft skid shoes showed deformation and a clockwise twist on the skid. The observed damage was consistent with the skid making contact with the ground while moving in a right lateral direction under significant impact force.

Probable cause

The decrease in rotor and engine RPM during the landing flare, which led to an uncontrolled rotation and subsequent ground contact.

Frequently asked questions

What happened in the 2001-08-08 Schweizer 300C accident near Cicero, NY?

A helicopter experienced a 360-degree rotation and subsequent rollover after the rotor and engine RPM decreased during a landing flare.

What aircraft was involved and where did it happen?

The accident on 2001-08-08 involved a Schweizer 300C, registration N1281R, operated by Highland Helicopter Services, at Cicero, NY.

What was the probable cause of the accident?

The decrease in rotor and engine RPM during the landing flare, which led to an uncontrolled rotation and subsequent ground contact.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010830X01827. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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