No fatalities

Engine Power Loss Forces Landing in Paddocks (VH-ANJ)

Warrnambool, AustraliaTakeoff (climb)

On April 2, 1965, a Douglas C-47 Skytrain (DC-3) (registration VH-ANJ) operated by Airlines of New South Wales was involved in an aviation accident near Warrnambool, Australia during takeoff. No fatalities were reported. Investigators recorded the probable cause as: The cause of the accident was that the pilot-in-command, on becoming aware of a loss of engine power, took action to feather the propeller after adopting procedures which failed to ensure correct identification of the defective engine. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards
Aircraft registered VH-ANJ
Aircraft registered VH-ANJ. Photo: Paul Nelhams from Shannon, Ireland / CC BY-SA 2.0, via Wikimedia Commons

On a scheduled domestic flight, an aircraft experienced engine power loss shortly after takeoff. The pilot feathered the port engine but found starboard power insufficient, leading to a forced landing in grassy paddocks. All occupants survived, but the aircraft was written off.

Incident Overview

A scheduled domestic flight from Hamilton to Melbourne, with an intermediate stop at Warrnambool, Victoria, landed uneventfully at Warrnambool at 2159 hours GMT. After a 17-minute ground stop during which load changes occurred, the aircraft taxied to runway 31 for takeoff. Pre-takeoff checks indicated no abnormalities.

Takeoff and Power Loss

Shortly after becoming airborne, and before the undercarriage was retracted, a loss of engine power occurred. The pilot-in-command deduced that the port engine had failed and feathered its propeller. However, he then realized that the starboard engine was delivering only partial power, which was insufficient to sustain flight.

Emergency Landing

The pilot immediately selected a suitable area and executed a landing with wheels and flaps retracted in grassy paddocks on level terrain. During the landing, the aircraft passed through three fences before coming to rest. All occupants survived the incident.

Damage

The aircraft sustained substantial damage and was written off.

Probable Cause

The official finding stated that the cause of the accident was that the pilot-in-command, on becoming aware of a loss of engine power, took action to feather the propeller after adopting procedures which failed to ensure correct identification of the defective engine.