No fatalities

Aircraft Stalls During Steep Turn in Formation Flight (VH-AGA)

Goulburn, AustraliaLanding (descent or approach)

On December 1, 1984, a Rockwell Aero Commander 500 (registration VH-AGA) operated by Fairburn Aviation Services was involved in an aviation accident near Goulburn, Australia during landing or approach. No fatalities were reported. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

While leading a formation of two aircraft for a training flight to Goulburn, a pilot stalled during a steep turn and was unable to recover before impact due to lack of awareness of stall speed in that configuration.

Incident Overview

An aircraft being used to transport equipment for members of an Aero Club, who were to carry out training at Goulburn, was involved in an accident during a formation flight. The pilot, who was undergoing formation flying training, had been designated to lead a formation of two aircraft for the flight. A briefing on the procedures to be followed was conducted prior to departure.

Flight Sequence

During the flight, the pilot of the second aircraft began to suspect the accuracy of his aircraft's airspeed indicator and requested that it be checked against that of the lead aircraft as the aircraft joined the circuit. The pilot of the lead aircraft extended the landing gear and flew the initial leg of the circuit at an indicated airspeed of 96 knots.

At the end of this leg, the pilot turned the aircraft steeply to the left. During the turn, the nose dropped slightly and the aircraft flicked into a steep right turn. Subsequently, the aircraft assumed a steep nose-down attitude. The pilot was able to level the wings and raise the nose to a level attitude before impact. However, the impact occurred at a very high rate of sink.

Pilot Experience and Maneuver

The pilot had not previously practiced steep turns at relatively slow airspeed and was not aware of the stalling speed in the given configuration and attitude. The pilot was subsequently unable to recall the reason for attempting a steeper than normal turn. When the aircraft stalled, the pilot was unable to effect a full recovery in the height available before impact with the ground.