Aircraft stall and crash following engine failure during takeoff

No fatalities • Helsinki-Malmi, Finland • Takeoff (climb)

An aircraft experienced an engine failure immediately after rotation, leading to a stall and subsequent crash during the initial climb phase.

What happened

During the takeoff sequence, the aircraft experienced a critical loss of power immediately after reaching rotation speed. As the plane entered its initial climb, the loss of thrust resulted in an aerodynamic stall. The aircraft subsequently impacted the ground, resulting in a crash.

While the airframe sustained damage that was deemed beyond repair, there were no fatalities or injuries reported among those on board.

Findings

Official investigations determined that the primary factor leading to the accident was an engine failure occurring just after the aircraft rotated from the runway.

Probable cause

The engine failed immediately following rotation, causing the aircraft to stall during its initial climb.

Frequently asked questions

What happened in the 1951-02-07 Douglas DC-2 accident near Helsinki-Malmi, Finland?

An aircraft experienced an engine failure immediately after rotation, leading to a stall and subsequent crash during the initial climb phase.

Were there any fatalities in the 1951-02-07 Douglas DC-2 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1951-02-07 involved a Douglas DC-2, registration DO-3, operated by Finnish Air Force - Suomen Ilmavoimat, at Helsinki-Malmi, Finland.

What was the probable cause of the accident?

The engine failed immediately following rotation, causing the aircraft to stall during its initial climb.

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