1 fatality

1990-03-12: GAF Nomad N.24 (A18-401) — Royal Australian Air Force - RAAF — Edinburgh AFB, Australia

Edinburgh AFB, AustraliaLanding (descent or approach)

On March 12, 1990, a GAF Nomad N.24 (registration A18-401) operated by Royal Australian Air Force - RAAF was involved in an aviation accident near Edinburgh AFB, Australia during landing or approach. One person was killed. Investigators recorded the probable cause as: After being manufactured in 1982, the airplane was used by GAF (renamed ASTA in 1987) for testing. Service records indicated 177 hours of single engine ground running, subjecting the airplane to many high frequency asymmetric cycles. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781213110Data APIEditorial standards

A training flight at Edinburgh AFB ended when the tail separated, causing the aircraft to crash. The pilot was killed. Investigation revealed undetected cracking from prior testing led to in-flight failure.

Incident Overview

A pilot on a local training flight at Edinburgh Air Force Base experienced a catastrophic structural failure during approach. The tail separated from the aircraft, causing it to dive into the ground and crash near the airfield. The aircraft was destroyed, and the sole occupant, pilot F/Lt Glenn Kemshall Donovan, was killed.

Investigation Findings

The investigation determined the probable cause as follows:

After being manufactured in 1982, the airplane was used by the Government Aircraft Factories (GAF), renamed Aerospace Technologies of Australia (ASTA) in 1987, for testing. Service records indicated that the aircraft accumulated 177 hours of single-engine ground running. This subjected the airplane to many high-frequency asymmetric cycles. Cracks initiated and grew predominately due to torsional loading.

Upon delivery to the Royal Australian Air Force (RAAF), the aircraft was inspected. However, this inspection failed to detect significant cracking. The tailplane centre section failed in flight 19 hours after the inspection.