2 fatalities

1959-03-30: Curtiss C-46 Commando (N7840B) — Riddle Airlines — Alma, United States of America

Alma, United States of AmericaFlight

On March 30, 1959, a Curtiss C-46 Commando (registration N7840B) operated by Riddle Airlines was involved in an aviation accident near Alma, United States of America in flight. 2 people were killed. Investigators recorded the probable cause as: The Board determines that the probable cause of this accident was the ignition of cargo in the aft belly compartment caused by contact with an unguarded light bulb. 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 1781247565Data APIEditorial standards

While en route from Orlando to Atlanta, a crew reported a cabin fire and requested diversion. The aircraft subsequently went out of control and crashed in flames in Alma, Georgia, disintegrating on impact. Both crew members were killed. Ground witnesses observed fire breaching the fuselage before impact.

Accident Overview

On a night flight from Orlando to Atlanta, the crew reported to air traffic control that a fire had erupted in the cabin and requested permission to divert to the nearest airport. Shortly thereafter, the aircraft went out of control and crashed in flames in a prairie located in Alma, Georgia. The aircraft disintegrated on impact, and both crew members were killed.

Sequence of Events

Prior to the crash, ground witnesses observed the fire burning through the fuselage, allowing burning cargo and debris to be scattered over a large area. After making several left circles, the burning aircraft plunged to the ground.

Probable Cause

According to the official investigation, the probable cause of this accident was the ignition of cargo in the aft belly compartment caused by contact with an unguarded light bulb. It is believed the fire then breached the compartment wall and damaged a hydraulic unit or line in the wing center section area at the rear spar, igniting the flammable hydraulic fluid.