Aircraft crash during takeoff roll

No fatalities • Hradec Králové, Czech Republic • Takeoff (climb)

An aircraft crashed in a field shortly after takeoff following an engine power loss, resulting in no injuries to the crew.

What happened

During the initial stages of flight on runway 27, the aircraft reached rotation speeds between 140 and 150 km/h. As the plane climbed to an altitude of approximately 30 feet, a slight rightward turn occurred, coinciding with a suspected loss of power in the right engine.

In response to the situation, the pilot-in-command executed a left turn, deployed the flaps, and lowered the nose to increase airspeed. Although the aircraft managed to accelerate to 200 km/h, it subsequently struck the ground and crashed into a nearby field. The impact resulted in the aircraft being damaged beyond repair, though all three crew members escaped the accident uninjured.

Findings

Investigations into the incident revealed that there were no mechanical or technical malfunctions present on the aircraft. The crash was ultimately attributed to pilot error during the recovery attempt.

Probable cause

The accident was caused by pilot error rather than any technical failure of the aircraft.

Frequently asked questions

What happened in the 1953-04-24 Aero C-3A accident near Hradec Králové, Czech Republic?

An aircraft crashed in a field shortly after takeoff following an engine power loss, resulting in no injuries to the crew.

Were there any fatalities in the 1953-04-24 Aero C-3A accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1953-04-24 involved a Aero C-3A, registration AK-2, operated by Czech Air Force - Ceské Vojenské Letectvo, at Hradec Králové, Czech Republic.

What was the probable cause of the accident?

The accident was caused by pilot error rather than any technical failure of the aircraft.

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