Incident Overview

Date: Saturday 7 December 1957
Aircraft Type: Scottish Aviation Twin Pioneer 1
Owner/operator: Scottish Airlines
Registration Number: G-AOEO
Location: Fezzan – ÿ Libya
Phase of Flight: Unknown
Status: Destroyed, written off
Casualties: Fatalities: 6 / Occupants: 6
Component Affected: Outer panel of the left hand wingOuter panel of the left hand wing
Category: Accident
A Twin Pioneer aircraft, operated by the manufacturer, experienced a catastrophic crash 285 miles south-west of Tripoli after a scheduled 3.5-hour flight back to Idris. The aircraft crashed outside the main wreckage, with the outer panel of the left wing damaged. The probable cause was a failure in fatigue of the forward tube of the ‘V brace’ structure, resulting in the separation of the port wing’s outer panel.A Twin Pioneer aircraft, operated by the manufacturer, experienced a catastrophic crash 285 miles south-west of Tripoli after a scheduled 3.5-hour flight back to Idris. The aircraft crashed outside the main wreckage, with the outer panel of the left wing damaged. The probable cause was a failure in fatigue of the forward tube of the ‘V brace’ structure, resulting in the separation of the port wing’s outer panel.

Description

The Twin Pioneer aircraft, operated by the manufacturer, had performed a local flight at the Atshan Esso Petroleum camp when it took off at 14:27 for an expected 3,5 hour flight back to Idris. The aircraft did not arrive at its destination and was found to have crashed 285 miles SSW of Tripoli. The outer panel of the left hand wing was found 1200 yards from the main wreckage. PROBABLE CAUSE: “The failure in fatigue of the forward tube of the “V brace” structure in the outer panel of the port wing. This failure led to the breaking away of the outer panel of the port wing from the aircraft in flight. The aircraft was then rendered completely uncontrollable and dived vertically to the ground.”

Primary Cause

Fatigue failure of the forward tube of the ‘V brace’ structure in the outer panel of the port wing.Fatigue failure of the forward tube of the ‘V brace’ structure in the outer panel of the port wing.

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