15 fatalities

Propeller Blade Separation Leads to Crash in Kasai Province, Killing All 15 Occupants (OO-CBN)

Kikwit, Democratic Republic of CongoFlight

On February 4, 1952, a Douglas C-47 Skytrain (DC-3) (registration OO-CBN) operated by SABENA - Société Anonyme Belge d'Exploitation de la Navigation Aérienne was involved in an aviation accident near Kikwit, Democratic Republic of Congo in flight. 15 people were killed. Investigators recorded the probable cause as: The propeller blade severed the cables used to control the elevator, which explains the loss of control. Investigations indicate that the sudden shutdown of the right engine was caused by the upper half of the main connecting rod head becoming jammed between… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards

An aircraft lost control and crashed in Kasai province after a propeller blade separated from the right engine. All 15 occupants were killed. Investigation found the blade severed elevator cables and engine failure from a piston lug fracture.

Incident

On the day of the accident, at 1205 local time, an aircraft was overflying the Kasai province when it experienced a technical problem with its right engine. A propeller blade separated from the engine and penetrated the cabin. The aircraft subsequently went out of control, nosed down, and crashed two minutes later in the Dibata forest, approximately 20 kilometers from Kikwit. All 15 occupants were killed in the crash.

Occupants

The crew consisted of pilot Michael Joseph Adendorff, radio navigator Pierre Bisschop, and mechanic Willy Fauck. The passengers were Françoise Devos, Pierre Devos, Mercédès Dumont, André Hubens, Albert Lemaire, Mrs. Albert Lemaire, Claude Lemaire, Anne-Marie Lemaire, Norman Orne, André Paquay, Mrs. André Paquay, and Jacqueline Sailliez.

Investigation

The official investigation determined that the propeller blade severed the cables used to control the elevator, which resulted in the loss of control. Further investigation indicated that the sudden shutdown of the right engine was caused by the upper half of the main connecting rod head becoming jammed between the crankshaft counterweight and the crankcase at the opening of cylinder number 14. The initial cause of the observed malfunctions was the fracture of a lug on piston number 6.

Probable cause

The propeller blade severed the cables used to control the elevator, which explains the loss of control. Investigations indicate that the sudden shutdown of the right engine was caused by the upper half of the main connecting rod head becoming jammed between the crankshaft counterweight and the crankcase at the opening of cylinder n°14. The initial cause of the malfunctions observed was the fracture of a lug on piston n°6.