Rotor Control Failure Leads to Fatal Magni M16 Crash

Casualties unknown • French is the work of reference., FR

A mechanical failure in the rotor control linkage caused a rotor blade to strike the cockpit of a gyroplane, resulting in a fatal accident near Vaux-Saules.

What happened

On March 2, 2022, a Magni M16 Tandem Trainer gyroplane, registration 21AGP, was conducting a local flight from Dijon-Darois aerodrome when it crashed in a wooded area near Vaux-Saules. The aircraft was flying at an altitude of approximately 2,750 feet in a north-easterly direction when the accident occurred. The impact resulted in one fatality (the pilot) and the total destruction of the aircraft.

The investigation

The BEA examined the wreckage and the rotor assembly to determine the cause of the loss of control. Investigators found significant impact marks on the leading edge of one rotor blade, which corresponded to the location of cockpit debris found away from the main wreckage. This indicated that a rotor blade had struck the right front section of the cockpit and the pilot during flight.

Technical analysis of the rotor control linkage revealed that the fixed connection between the rotor control fork and the rotor had failed. Specifically, the examination showed that a taper pin had gouged the fork, and a bolt used to secure the assembly had ruptured at both ends. These failures allowed the control fork to rotate independently of the rotor, leading to contact between the notched gear and the fork arm, which ultimately caused the rotor blade to move out of its intended plane.

Findings

  • The primary cause of the accident was the rupture of the rotor control linkage components, specifically the bolt and the taper pin.
  • This mechanical failure allowed for unintended relative movement between the rotor and the control fork.
  • The resulting instability caused a rotor blade to strike the cockpit and the pilot.
  • While the exact sequence of the component failures could not be determined, investigators could not rule out an initial rupture occurring under load during a sudden maneuver or a prior to flight.
  • Maintenance records showed the aircraft had undergone a 500-hour inspection, but this specific connection is not a required inspection point under the manufacturer's standard maintenance program.

Probable cause

The loss of control was caused by the failure of the connection between the rotor and the control linkage due to the rupture of a bolt and a taper pin, which led to a rotor blade striking the aircraft structure.

Frequently asked questions

What happened in the 2022-03-02 MAGNI - M16 Tandem Trainer accident near French is the work of reference., FR?

A mechanical failure in the rotor control linkage caused a rotor blade to strike the cockpit of a gyroplane, resulting in a fatal accident near Vaux-Saules.

What aircraft was involved and where did it happen?

The accident on 2022-03-02 involved a MAGNI - M16 Tandem Trainer, registration 21AGP, at French is the work of reference., FR.

What was the probable cause of the accident?

The loss of control was caused by the failure of the connection between the rotor and the control linkage due to the rupture of a bolt and a taper pin, which led to a rotor blade striking the aircraft structure.

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