Flaperon Control Failure Leads to Fatal Crash of MCR01 Sportster

Casualties unknown • FR

A mechanical failure in the flaperon control system caused a loss of roll control, resulting in the fatal crash of a Dyn’Aéro MCR01 VLA Sportster in France.

What happened

On September 25, 2011, a Dyn’Aéro MCR01 VLA Sportster, registration F-PSLA, departed from Mulhouse Habsheim aerodrome for a local flight. Approximately five minutes into the flight, witnesses observed the aircraft appear to stall, stabilize momentarily, and then stall a second time before impacting the ground near Heimsbrutnn. The pilot, who was the sole occupant, was killed in the crash, and the aircraft was destroyed.

The investigation

The investigation focused on the aircraft's unique flaperon system, which combines aileron and flap functions using a screw-and-nut mechanism (a screw-driven mobile carriage). Investigators examined the wreckage and found that the left flaperon's screw-driven mechanism had become detached from its threaded insert.

Technical analysis revealed significant wear on the threaded inserts of both the left and right flaperon controls. The investigation also scrutinized the aircraft's maintenance records and documentation. It was noted that the maintenance manuals contained contradictory instructions regarding the frequency and method of checking axial play. Furthermore, the investigation found that the maintenance of the aircraft's flaperon system was difficult to perform effectively due to a lack of specific tools and clear inspection procedures.

Findings

  • The primary cause of the accident was the failure of the flaperon control mechanism, which led to asymmetric lift and a subsequent loss of roll control.
  • Excessive axial play, likely exceeding the 0.3 mm limit, had caused the threads to wear down rapidly.
  • The wear pattern (described as "diabolo" shaped) indicated a misalignment between the screw and the insert, possibly due to improper assembly during construction or structural deformation.
  • The use of an ISO-profile screw, which is better suited for fastening than for heavy-duty guiding, contributed to the mechanical instability.
  • Inadequate maintenance documentation and the lack of a standardized inspection method prevented the detection of the excessive play before the failure occurred.

Probable cause

The accident was caused by the failure of the roll control mechanism due to an inadequate design of the flaperon control system and ineffective maintenance practices that failed to detect excessive axial play caused by mechanical wear and misalignment.

Frequently asked questions

What happened in the 2011-09-25 Dyn’Aéro MCR01 VLA Sportster à Heimsbrunn accident near FR?

A mechanical failure in the flaperon control system caused a loss of roll control, resulting in the fatal crash of a Dyn’Aéro MCR01 VLA Sportster in France.

What aircraft was involved and where did it happen?

The accident on 2011-09-25 involved a Dyn’Aéro MCR01 VLA Sportster à Heimsbrunn, registration F-PSLA, at FR.

What was the probable cause of the accident?

The accident was caused by the failure of the roll control mechanism due to an inadequate design of the flaperon control system and ineffective maintenance practices that failed to detect excessive axial play caused by mechanical wear and misalignment.

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