Fatal aircraft accident during crop spraying operation

1 fatality • Seddon, New Zealand • Flight

A single-engine aircraft crashed in an open field after the right wing separated from the fuselage during a flight mission.

What happened

During a routine agricultural spraying mission, the pilot was operating an aircraft when a catastrophic structural failure occurred. While in flight, the starboard wing became detached from the rest of the airframe. This loss of control led to the aircraft impacting an open field, resulting in the total destruction of the plane. The pilot, who was the only person on board at the time of the incident, sustained fatal injuries.

Findings

Investigations into the wreckage determined that the accident was the result of the right wing separating from the aircraft while it was airborne. This structural failure was driven by a significant reduction in the strength of the wing assembly. Specifically, investigators identified extensive fatigue cracks located within the lower center wing wraparound and the internal doublers situated inboard of Station 142. The progression and eventual failure of these cracks were attributed to consistent overstress during flight operations.

Probable cause

The separation of the right wing was caused by structural failure resulting from fatigue cracks induced by repeated overstressing of the wing components.

Frequently asked questions

What happened in the 1973-02-23 Douglas DC-3 accident near Seddon, New Zealand?

A single-engine aircraft crashed in an open field after the right wing separated from the fuselage during a flight mission.

Were there any fatalities in the 1973-02-23 Douglas DC-3 accident?

The accident was fatal, resulting in 1 fatality.

What aircraft was involved and where did it happen?

The accident on 1973-02-23 involved a Douglas DC-3, registration ZK-AOI, operated by Southern Air Super, at Seddon, New Zealand.

What was the probable cause of the accident?

The separation of the right wing was caused by structural failure resulting from fatigue cracks induced by repeated overstressing of the wing components.

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