Casualties unknown

2007-08-26: Robin DR 400/180R, Remorquer — Flugplatz Iserlohn-Sümmern, DE

Flugplatz Iserlohn-Sümmern, DE

On August 26, 2007, a Robin DR 400/180R, Remorquer was involved in an aviation accident near Flugplatz Iserlohn-Sümmern, DE. Investigators recorded the probable cause as: The accident was caused by the **simultaneous conduct of winch operations and powered flight**, which violated airfield regulations. This summary draws on records from the German Federal Bureau of Aircraft Accident Investigation (BFU).

Sourcesthe German Federal Bureau of Aircraft Accident Investigation (BFU)Primary reportUpdated 1785665765Data APIEditorial standards

A Robin DR 400/180R towplane crashed into a forest after striking a descending glider winch cable during simultaneous flight operations.

What happened

On August 26, 2007, at Iserlohn-Sümmern airfield, a Robin DR 400/180R towplane was engaged in training operations. Following a landing with its engine shut down, the pilot restarted the engine and prepared for a subsequent takeoff. During this period, a glider winch launch was also being conducted.

As the towplane was in its initial climb, it encountered the descending winch cable of a glider. Due to a prevailing wind from the right, the cable had drifted diagonally across the runway path. The left wing of the Robin DR 400/180R struck the cable, which severed the wing's torsion box up to the level of the main spar. This impact caused a severe deceleration and a leftward yaw, forcing the aircraft into a steep descent. The aircraft struck the ground in a conifer forest approximately 25 meters southwest of the runway end. The pilot sustained fatal injuries and died at the scene.

The investigation

The BFU investigation examined the sequence of events, the airfield's operational procedures, and the meteorological conditions. Investigators found that the aircraft was properly maintained, with its last annual inspection completed in June 2007. The pilot was highly experienced, with approximately 4,100 total flight hours.

Technical examination of the wreckage revealed no mechanical failures in the aircraft. The investigation also focused on the airfield's regulations, which prohibit simultaneous winch operations and powered flight. The investigation confirmed that the winch cable, made of Dyneema, had been cut by the impact, and the cable end was found near the winch station.

Probable cause

The accident was caused by the **simultaneous conduct of winch operations and powered flight**, which violated airfield regulations. This was compounded by inadequate communication between the pilot and ground personnel, as the pilot proceeded with takeoff despite being notified of the ongoing winch launch. The collision was finalized by a crosswind that drifted the descending cable into the flight path of the climbing towplane.