38 fatalities

Nice Airport Takeoff Accident: Four-Engine Aircraft Crashes After Aileron Jamming (F-BCUM)

Nice, FranceTakeoff (climb)

On March 3, 1952, a SNCASE SE.161 Languedoc (registration F-BCUM) operated by Air France was involved in an aviation accident near Nice, France during takeoff. 38 people were killed. Investigators recorded the probable cause as: The probable cause was the unclamping of a link cheek of the upper rear chain of the co-pilot's control column, which caused the chain to slip off the sprocket and jam the ailerons to the left at approximately 10 degrees. 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

A four-engine aircraft crashed near Nice Airport seconds after takeoff due to a left aileron blockage. The accident killed all but one passenger, who died days later.

Incident Overview Forty-five seconds after departing runway 04 at Nice Airport, the four-engine aircraft entered an unusual flight path during its initial climb. The airplane banked sharply to the left, overturned, and crashed in a major explosion near the Saint-Augustin station, located north of the airfield. The aircraft disintegrated upon impact. Only one female passenger was initially found alive, but she succumbed to her injuries four days later. Among the fatalities were French actresses Michèle Verly and Lise Topart, and Welsh politician John Emlyn-Jones. The crew consisted of pilot Mr. Farrugia, radio operator Mr. Fraillon, mechanic Mr. Cavaille, and steward Mr. Biancheri. ## Investigation Findings The official investigation determined that the aircraft's unusual path immediately following takeoff was caused by the ailerons being blocked to the left at an angle of approximately 10 degrees. Analysis revealed that the probable cause of this blockage was the unclamping of a link cheek of the upper rear chain of the co-pilot's control column. This failure allowed the chain to slip off its sprocket and jam against the internal boss of the pin used to lock the ailerons in the neutral position. ## Safety Implications The investigation highlighted significant difficulties in setting and inspecting the chains within the dual control columns. These challenges were directly attributed to the design of the system. The findings indicated that certain chains, which had not been adequately studied for their intended service, could become unclamped by torsion during maintenance and setting operations.