2 fatalities

1980-03-23: Cessna 414 Chancellor (G-BAOZ) — Northair Aviation — Leeds-Bradford, United Kingdom

Leeds-Bradford, United KingdomLanding (descent or approach)

On March 23, 1980, a Cessna 414 Chancellor (registration G-BAOZ) operated by Northair Aviation was involved in an aviation accident near Leeds-Bradford, United Kingdom during landing or approach. 2 people were killed. Investigators recorded the probable cause as: It is concluded that the aircraft entered the spin from an accelerated stall, possibly as the result of the pilot attempting to regain the approach centre line by a higher rate or turn than normal. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781224135Data APIEditorial standards

A post-maintenance flight from Leeds-Bradford Airport crashed while on final approach, entering a left spin and catching fire. Both pilot and engineer were killed. The investigation concluded an accelerated stall as the probable cause.

Accident

A post-maintenance flight departed Leeds-Bradford Airport in the mid-morning, carrying one pilot and one engineer. The aircraft was scheduled for transfer to Pakistan the following day on behalf of the United Nations Organization. Witnesses observed the aircraft on final approach to runway 15, flying more slowly than usual and at a low height. As the aircraft turned onto final approach, it developed into a spin to the left. After two or three rotations, the aircraft crashed into a wooded area and caught fire. Both occupants were killed.

Investigation

Investigators examined the circumstances of the accident, including the aircraft's performance and environmental conditions. It was noted that the aircraft's flap system had been modified, which affected its handling characteristics.

Cause

The official investigation concluded that the aircraft entered the spin from an accelerated stall, possibly as a result of the pilot attempting to regain the approach centerline by a higher rate of turn than normal. The relatively slow speed of the aircraft, the gusty conditions, and the handling characteristics associated with the aircraft's modified flap system were considered contributory factors.

Probable cause

It is concluded that the aircraft entered the spin from an accelerated stall, possibly as the result of the pilot attempting to regain the approach centre line by a higher rate or turn than normal. The relatively slow speed of the aircraft, the gusty conditions and the handling characteristics associated with the aircraft's modified flap system are considered to have been contributory factors.