Incident Overview

Date: Monday 12 March 1990
Aircraft Type: GAF Nomad N.24A
Owner/operator: Royal Australian Air Force – RAAF
Registration Number: A18-401
Location: near Mallala, SA – ÿ Australia
Phase of Flight: Approach
Status: Destroyed, written off
Casualties: Fatalities: 1 / Occupants: 1
Component Affected: Tailplane centre sectionTailplane centre section
Category: Accident
A GAF Nomad N.24A transport plane crashed near Mallala, SA, Australia, resulting in the pilot’s death. The tailplane broke off during flight due to torsional loading, leading to a crash. The aircraft was used for testing by the Royal Australian Air Force (RAAF) and experienced significant asymmetric cycle operation, ultimately resulting in the tailplane centre section failure.A GAF Nomad N.24A transport plane crashed near Mallala, SA, Australia, resulting in the pilot’s death. The tailplane broke off during flight due to torsional loading, leading to a crash. The aircraft was used for testing by the Royal Australian Air Force (RAAF) and experienced significant asymmetric cycle operation, ultimately resulting in the tailplane centre section failure.

Description

The GAF Nomad N.24A transport plane was destroyed in an accident near Mallala, SA, Australia. The pilot was killed. The tail plane broke off in flight and the aircraft crashed. The aircraft was allocated by the Royal Australian Air Force (RAAF) to the Aircraft Research and Development Unit (ARDU). After being manufactured in 1982, the airplane was used by GAF (renamed Aerospace Technologies of Australia – ASTA in 1987) for testing. Amongst others, service records indicated 177 hours of single engine ground running. This meant that the airplane was subjected to many high frequency asymmetric cycles. Cracks initiated and grew predominately due to torsional loading. Upon delivery to the RAAF, the airplane was inspected but this failed to detect significant cracking. The tailplane centre section failed in flight, 19 hours after the inspection.

Primary Cause

Torsional loading during asymmetric cycle operation.Torsional loading during asymmetric cycle operation.

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