Loss of control following improper reassembly of Skyranger ultralight

Casualties unknown • FR

An ultralight aircraft crashed shortly after takeoff at AD Gap (05) due to inverted aileron controls resulting from an incorrect reassembly process.

What happened

On Saturday, July 19, 2003, at 11:45 local time, an Aéros Kiev Skyranger "Best Off" ultralight, identified as 83-CR, crashed during a local flight at AD Gap (05). The aircraft was carrying two occupants: the pilot and a passenger. Shortly after departing the runway, the pilot observed the aircraft banking sharply to the right. Although the pilot attempted to correct the movement by applying left input, the right turn intensified, leading to a collision with the ground. The impact resulted in one injury and the total destruction of the aircraft.

The investigation

The investigation focused on the mechanical state of the aircraft following its recent transport. The pilot had previously operated the aircraft in Canada before it was disassembled for transport back to France. In June 2003, the owner and a representative from an ultralight company reassembled the aircraft. This was the second time the representative had performed this specific assembly procedure.

Investigators examined the wreckage and discovered that the aileron control cables had not been crossed according to the required specifications. This error caused the aileron movement at the control stick to be inverted. While the crew stated they had performed a pre-flight check to verify that stick movements corresponded to aileron movement, the investigation determined that the pre-flight inspections were insufficient to detect the mechanical error.

Probable cause

The accident was caused by the improper reassembly of the aircraft's control cables, which resulted in inverted aileron controls, and was compounded by insufficient pre-flight checks to identify the error.

Frequently asked questions

What happened in the 2003-07-19 aircraft accident near FR?

An ultralight aircraft crashed shortly after takeoff at AD Gap (05) due to inverted aileron controls resulting from an incorrect reassembly process.

What aircraft was involved and where did it happen?

The accident on 2003-07-19 involved a aircraft, registration 83-CR, at FR.

What was the probable cause of the accident?

The accident was caused by the improper reassembly of the aircraft's control cables, which resulted in inverted aileron controls, and was compounded by insufficient pre-flight checks to identify the error.

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