44 fatalities

1953-10-14: Convair CV-240 (OO-AWQ) — SABENA - Société Anonyme Belge d'Exploitation de la Navigation Aérienne — Frankfurt-Main, Germany

Frankfurt-Main, GermanyTakeoff (climb)

On October 14, 1953, a Convair CV-240 (registration OO-AWQ) operated by SABENA - Société Anonyme Belge d'Exploitation de la Navigation Aérienne was involved in an aviation accident near Frankfurt-Main, Germany during takeoff. 44 people were killed. Investigators recorded the probable cause as: The loss of power may be attributed to the heavy deposit of lead on the sparking plugs. During takeoff, as the plugs warmed up, circuit was formed by the metal deposits, resulting in the short circuiting of the plugs. 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 1781252820Data APIEditorial standards
Aircraft registered OO-AWQ
Aircraft registered OO-AWQ. Photo: Nationaal Archief / CC0, via Wikimedia Commons

Shortly after takeoff from Frankfurt-Main Airport, a twin-engine aircraft suffered a loss of power on both engines, stalled, and crashed in a wooded area near Kelsterbach, killing all 44 on board.

Accident Details

Shortly after takeoff from Frankfurt-Main Airport, while in initial climb, the crew noticed a loss of power on both engines. The crew raised the flaps according to procedures. The aircraft then stalled and crashed in flames in a wooded area located in Kelsterbach, approximately three kilometers north of the airfield. The aircraft was destroyed by impact forces and a post-crash fire. All 44 occupants on board were killed.

Investigation and Probable Cause

The official investigation determined that the loss of power may be attributed to the heavy deposit of lead on the sparking plugs. During takeoff, as the plugs warmed up, a circuit was formed by the metal deposits, resulting in the short circuiting of the plugs. There was nothing to show any other contributory causes. A contributory cause of the crash may have been the pilot's decision to continue the takeoff, and the probable retraction of the landing flaps at extensively low speed and low altitude, unless the loss of power by both engines in the phase immediately before the crash was so great that the disaster was unavoidable. The investigation found no evidence that the lead coating process occurred suddenly, but showed that the process had been continuous. It was not possible to determine, from the data available, whether the periods specified by the makers of the engines for overhaul of plugs should be considered adequate in all cases.