5 fatalities

Twin-Engine Aircraft Crash Near Breendonk Kills Five (OO-TPN)

Breendonk, BelgiumLanding (descent or approach)

On October 18, 1982, a Partenavia P.68 (registration OO-TPN) operated by Hessenatie-Sotramat Aviation was involved in an aviation accident near Breendonk, Belgium during landing or approach. 5 people were killed. Investigators recorded the probable cause as: Loss of control during descent under instrument flight conditions and exceeding airframe structural limits, with contributing factors including icing risk and crew inexperience. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

A twin-engine aircraft on a VFR flight from Avignon to Brussels crashed near Breendonk after entering a spiral descent. The airframe broke in flight due to aerodynamic overload. All five occupants were killed.

Accident Overview

On the day of the accident, a twin-engine airplane departed Avignon at 1631 local time on a visual flight rules (VFR) flight to Brussels. On board were two pilots and three passengers. As the aircraft approached its destination at an altitude of 7,000 feet, air traffic control cleared the crew to descend to 2,000 feet.

Sequence of Events

During the descent, while passing 6,400 feet, the airplane entered a left-hand spiral. The airframe failed due to aerodynamic overload, causing the tail, the upper left wing, and the leading edges of both wings to separate from the aircraft. The uncontrolled airplane then dove into the ground near Breendonk. All five occupants were killed in the crash.

Contributing Factors

Investigators identified several factors that contributed to the accident. The crew lacked the required licenses and qualifications to operate the twin-engine aircraft and to conduct flight in instrument meteorological conditions. The Pitot tube heating system was found in the OFF position at the time of the accident. Additionally, two onboard systems—the autopilot and the wing leading edge de-icing system—had been out of order for five days prior to the flight. Weather conditions posed a risk of icing.

During the descent, the pilot lost control of the aircraft, which entered a left-hand spiral. The pilot attempted a high-speed pull-up, but the resulting aerodynamic loads exceeded the structural limits of the airframe, leading to in-flight breakup.

Probable Cause

The official probable cause of the accident was loss of control of the aircraft during a descent under instrument flight conditions and exceeding the airframe's structural limits. Contributing factors included weather conditions posing a risk of icing, the crew's lack of experience and qualifications in flying a twin-engine aircraft and in instrument flight conditions, the inoperative Pitot tube heating, and the prolonged unavailability of the autopilot and wing de-icing systems.