Aircraft stall and crash following takeoff

2 fatalities • Siuna, Nicaragua • Takeoff (climb)

An aircraft stalled and crashed into a wooded area shortly after departure, resulting in two fatalities and sixteen injuries.

What happened

During the initial climb phase following takeoff, the aircraft experienced an aerodynamic stall. The plane subsequently impacted a forested region situated approximately 2,400 meters beyond the threshold of the runway. A post-crash fire ignited upon impact, resulting in the total destruction of the airframe.

The accident resulted in two fatalities, including one crew member and one passenger. Additionally, sixteen other individuals on board sustained injuries during the event.

Findings

Investigations into the wreckage revealed a mechanical failure within the engine components. During the disassembly of the port propeller, inspectors identified that the distributor valve had fractured from its junction at the engine crankshaft, with the initial threads having failed. This structural failure was attributed to metal fatigue.

The primary factor in the accident was the rupture of the port propeller's distributor valve. The investigation also noted that the presence of difficult terrain, along with specific wind and altitude conditions, contributed to the severity of the outcome.

Probable cause

The failure of the port propeller distributor valve due to fatigue caused the aircraft to stall during climb.

Frequently asked questions

What happened in the 1960-04-05 Curtiss C-46 Commando accident near Siuna, Nicaragua?

An aircraft stalled and crashed into a wooded area shortly after departure, resulting in two fatalities and sixteen injuries.

Were there any fatalities in the 1960-04-05 Curtiss C-46 Commando accident?

The accident was fatal, resulting in 2 fatalities.

What aircraft was involved and where did it happen?

The accident on 1960-04-05 involved a Curtiss C-46 Commando, registration AN-AIN, operated by Lineas Aéreas de Nicaragua - LANICA, at Siuna, Nicaragua.

What was the probable cause of the accident?

The failure of the port propeller distributor valve due to fatigue caused the aircraft to stall during climb.

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