Helicopter enters rapid descent during maintenance test flight

Casualties unknown • Grand Junction, CO, US

A helicopter entered a rapid descent and experienced rotor blade folding during a functional flight check following maintenance work.

What happened

During a maintenance test flight intended to perform a functional flight check for vibration and autorotation, the helicopter entered a rapid descent. Witnesses observed the rotor system slowing down and the rotor blades "folding" over the top of the aircraft during the maneuver. As the rotor system slowed, fragments identified as pieces from the transmission cowling were seen exiting the helicopter. The aircraft subsequently descended into the ground while performing a right-hand turn.

The investigation

An examination of the wreckage showed no evidence of any structural or system failure or malfunction. Investigators found that engine power had been applied while the rotor system was at a low rotational speed, though there was no evidence of engine failure or malfunction prior to impact.

According to the manufacturer, when the main rotor system slows under aerodynamic load, the main gearbox can undergo horizontal orbital movement, known as "walking," on its mounting structure. This movement can cause the transmission cowling to make contact with the main rotor control rod ends.

Findings

Investigation revealed that the pilot had received no training from the operator regarding how to conduct a maintenance test flight. It was also noted that the FAA does not require such training.

Probable cause

The main gearbox moved on its mounting structure during rotor deceleration under aerodynamic load, causing the transmission cowling to strike the main rotor control rod ends; additionally, the pilot had received no specific training for conducting maintenance test flights.

Frequently asked questions

What happened in the 2001-02-28 Bell 412SP accident near Grand Junction, CO?

A helicopter entered a rapid descent and experienced rotor blade folding during a functional flight check following maintenance work.

What aircraft was involved and where did it happen?

The accident on 2001-02-28 involved a Bell 412SP, registration N412SM, operated by Petroleum Helicopters, Inc., at Grand Junction, CO.

What was the probable cause of the accident?

The main gearbox moved on its mounting structure during rotor deceleration under aerodynamic load, causing the transmission cowling to strike the main rotor control rod ends; additionally, the pilot had received no specific training for conducting maintenance test flights.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010320X00611. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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