Glider Stall Leads to Fatal Crash During Competition Flight

Casualties unknown • Le Tranger, FR

A single-seat LS8-15 glider crashed in Le Tranger, France, after the pilot lost control during an attempt to land in a field.

What happened

On June 8, 2005, a pilot participating in a gliding competition near Romorantin, France, was conducting a triangular navigation flight. After passing the first waypoint at Clion, the pilot noted a continuous loss of altitude. At approximately 12:37 UTC, the pilot notified the Italian flight team via radio of the intention to perform a field landing due to the decreasing altitude, confirming that the landing gear had been extended.

As the pilot attempted to maneuver for the landing, GPS data indicates a series of turns. While attempting a steep turn to the right to reach a chosen landing area, the aircraft entered a stall. The impact occurred at a very low altitude, leaving insufficient height for the pilot to recover control of the LS8-15.

The investigation

The investigation focused on the aircraft's flight path and its weight and balance configuration. Investigators examined the wreckage of the D-6315 and recovered a GPS unit that allowed for the reconstruction of the final flight segments. The investigation also reviewed the aircraft's loading requirements and the pilot's experience.

Technical analysis of the wreckage showed no mechanical malfunctions. However, investigators found that the water ballast tanks in the wings and tail were empty. The investigation also noted that while the pilot was fully qualified, the aircraft's specific loading instructions—which were provided in German—were not properly addressed regarding the pilot's weight.

Findings

  • The pilot was attempting a field landing due to a lack of rising air.
  • The aircraft was flying with an aft center of gravity because no compensatory ballast was installed to offset the pilot's weight.
  • This aft CG made the glider unstable and difficult to handle, particularly during high-bank maneuvers at low speeds.
  • During a steep turn, the combination of high angle of attack and the unstable CG caused the aircraft to stall at an altitude too low for recovery.
  • The pilot did not use the required movable ballast to balance the aircraft's center of gravity.

Probable cause

The accident was caused by the pilot losing control of the glider during the final approach for a field landing. The lack of compensatory ballast to offset the pilot's weight resulted in an aft center of gravity, which contributed to the loss of control.

Frequently asked questions

What happened in the 2005-06-08 LS8-15 accident near Le Tranger, FR?

A single-seat LS8-15 glider crashed in Le Tranger, France, after the pilot lost control during an attempt to land in a field.

What aircraft was involved and where did it happen?

The accident on 2005-06-08 involved a LS8-15, registration D-6315, at Le Tranger, FR.

What was the probable cause of the accident?

The accident was caused by the pilot losing control of the glider during the final approach for a field landing. The lack of compensatory ballast to offset the pilot's weight resulted in an aft center of gravity, which contributed to the loss of control.

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