Loss of Control During Ground Roll Leads to Landing Gear Failure in Jodel DR 1050

Casualties unknown • Samedan, GR, CH

A training flight in a Jodel DR 1050 ended in a ground loop and collapsed landing gear after simultaneous braking inputs caused a loss of directional control.

What happened

On November 5, 2015, a Jodel DR 1050, registration HB-SEW, was performing training maneuvers at Samedan Airport. Following a series of touch-and-go landings, the aircraft performed a full-stop landing on runway 21. During the landing roll, the aircraft began to drift left of the centerline at a speed of approximately 30 to 40 km/h.

In an attempt to correct the drift, the student pilot applied right rudder. Simultaneously, the instructor applied light pressure to the right toe-brake to assist in the correction. However, the student pilot also applied a significant amount of pressure to the right toe-brake. This simultaneous application of braking force from both seats caused a massive increase in braking effectiveness, triggering the tailwheel lock to disengage. The aircraft then swung violently to the right, rotating approximately 110 degrees. During this rotation, the lateral forces caused the left main landing gear to collapse, resulting in the left wing striking the pavement. There were no injuries to the two occupants.

The investigation

SUST examined the mechanical and operational aspects of the incident. The investigation confirmed that the aircraft's weight and center of gravity were within limits and that there were no pre-existing technical defects. A key technical finding was that a recent modification had replaced the original heel brakes with toe-brakes accessible from both the front left and right seats. Because the braking systems are independent but share a reservoir, simultaneous application of the toe-brakes by both the instructor and the student results in an additive effect, significantly increasing braking force.

Findings

  • The primary cause of the accident was a loss of directional control during the landing roll due to excessive braking force.
  • The instructor's lack of coordination during the transition of control led to the additive braking effect.
  • The instructor's limited experience in the specific role of flight instructor on a tailwheel aircraft demanding for basic training was a contributing factor.
  • The instructor failed to use the standard "my controls" call to clearly establish command during the critical phase of the rollout.

Probable cause

The accident was caused by a loss of lateral control on the runway due to excessive braking, specifically the additive effect of both the instructor and student applying the right toe-brakes simultaneously, which caused the tailwheel to unlock and the aircraft to ground loop.

Frequently asked questions

What happened in the 2015-11-04 CENTRE EST AERONAUTIQUE JODEL DR 1050 accident near Samedan, GR, CH?

A training flight in a Jodel DR 1050 ended in a ground loop and collapsed landing gear after simultaneous braking inputs caused a loss of directional control.

What aircraft was involved and where did it happen?

The accident on 2015-11-04 involved a CENTRE EST AERONAUTIQUE JODEL DR 1050, registration HB-SEW, at Samedan, GR, CH.

What was the probable cause of the accident?

The accident was caused by a loss of lateral control on the runway due to excessive braking, specifically the additive effect of both the instructor and student applying the right toe-brakes simultaneously, which caused the tailwheel to unlock and the aircraft to ground loop.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/2304.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.

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