7 fatalities

In-Flight Fire Leads to Separation of Engine and Wing on Beech Queen Air near Alice Springs (VH-CMI)

Alice Springs, AustraliaTakeoff (climb)

On January 20, 1972, a Beechcraft 80 Queen Air (registration VH-CMI) operated by Connair was involved in an aviation accident near Alice Springs, Australia during takeoff. 7 people were killed. Investigators recorded the probable cause as: The probable cause of the accident was that, following an engine failure which resulted in severe vibration and a fire in the outboard rear section of the engine compartment, the integrity of the firewall and its attached exhaust ducting was lost and… 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 2026-06-12Data APIEditorial standards

On 20 January 1972, a Beech 65-80 Queen Air (VH-CMI) experienced an in-flight fire, causing separation of the starboard engine and outer wing. The aircraft crashed seven miles southwest of Alice Springs Airport, killing the pilot and six passengers.

Incident

At approximately 0745 hours Central Standard Time on 20 January 1972, an in-flight fire occurred in a Beech 65-80 Queen Air aircraft, registered VH-CMI. The fire led to the separation of the starboard engine and the starboard outer wing. The aircraft subsequently struck the ground about seven miles southwest of Alice Springs Airport in the Northern Territory.

Aircraft and Flight

The aircraft was a twin-engine Beech 65-80 Queen Air. At the time of the accident, it was operating a charter flight carrying passengers, mail, and freight from Alice Springs to Ayers Rock. The aircraft was destroyed by fire and impact forces.

Occupants and Fatalities

The pilot and six passengers were killed in the accident.

Investigation and Probable Cause

The official investigation determined the probable cause. Following an engine failure that resulted in severe vibration and a fire in the outboard rear section of the engine compartment, the integrity of the firewall and its attached exhaust ducting was lost. Structure at the rear of the engine nacelle was thereby exposed to fire.