Jump to Content
Download Final Report
[ Download PDF: 22KB]

The pilot was positioning for a spray run and the aircraft was in the last third of the procedure turn at an angle of bank of about 45 degrees. The aircraft was reported to have overshot the alignment of the next run slightly. One witness said he saw the nose of the aircraft go down. Another witness indicated that the aircraft then rolled under in the turn and struck the ground. The aircraft hit the ground inverted and travelled only about another 20 metres. An explosion occurred on impact and only the left wing and maingear remained unburnt. The pilot was wearing a full helmet and his harness was correctly worn and fastened. No apparent attempt to egress had been made. Subsequent investigation could find no faults or anomalies with the airworthiness of the aircraft that might have contributed to the accident. Advice provided to the investigation indicates that the Pawnee, at or near the stall in a turn, will stall the lower wing and roll under if aileron alone is used to try and pick up that wing. It was likely that while the pilot was manoeuvring to regain the alignment of the spray run, the aircraft was inadvertently stalled. A draft of this report was addressed to interested parties for consideration prior to release.

Download Final Report
[ Download PDF: 22KB]
General details
Date: 09 December 1989 Investigation status: Completed 
Time: 845  
Location:30 km NW Penola Investigation type: Occurrence Investigation 
State: South Australia Occurrence type: Loss of control 
Release date: 29 June 1990 Occurrence class: Operational 
Report status: Final Occurrence category: Accident 
 Highest injury level: Fatal 
Aircraft details
Aircraft manufacturer: Piper Aircraft Corp 
Aircraft model: PA-25 
Aircraft registration: VH-CUN 
Serial number: 25-4612 
Type of operation: Aerial Work 
Damage to aircraft: Destroyed 
Departure point:Coonawarra SA
Departure time:0830
Destination:30 km NW Penola SA
Share this page Provide feedback on this investigation