Training flight accident at RAF Newton

6 fatalities • Newton AFB, United Kingdom • Landing (descent or approach)

A training flight involving a crew of seven ended in a fatal crash at RAF Newton after an attempted go-around during poor visibility.

What happened

During a local training mission conducted at RAF Newton, the aircraft was on its final approach when it encountered challenging meteorological conditions. After descending through the final cloud layer at approximately 200 feet, the pilot managed to locate the runway briefly. However, due to the presence of scattered fog, the runway became obscured from view.

In response to the loss of visual contact with the landing strip, the pilot initiated a go-around maneuver. As the aircraft began its climb, it experienced a stall, leading to a high-impact crash and a subsequent large explosion. The accident resulted in six fatalities and left one crew member with serious injuries.

Findings

Investigations into the accident highlighted several critical elements. A significant contributing factor identified was that the aircraft's total weight exceeded its maximum allowable landing weight. This overweight condition is believed to have played a role in the aerodynamic failure during the climb phase.

Probable cause

The aircraft exceeded its maximum landing weight, which contributed to an aerodynamic stall during a go-around maneuver in low visibility.

Frequently asked questions

What happened in the 1953-12-04 Avro 652 Anson accident near Newton AFB, United Kingdom?

A training flight involving a crew of seven ended in a fatal crash at RAF Newton after an attempted go-around during poor visibility.

Were there any fatalities in the 1953-12-04 Avro 652 Anson accident?

The accident was fatal, resulting in 6 fatalities.

What aircraft was involved and where did it happen?

The accident on 1953-12-04 involved a Avro 652 Anson, registration VS507, operated by Royal Air Force - RAF, at Newton AFB, United Kingdom.

What was the probable cause of the accident?

The aircraft exceeded its maximum landing weight, which contributed to an aerodynamic stall during a go-around maneuver in low visibility.

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