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

Nearing the completion of the task the aircraft struck a single power line. The aircraft remained airborne but the pilot decided to land in a paddock and assess the damage. He found that the top 30 centimetres of the rudder had been torn off. Prior to spraying the paddock, the pilot had physically checked the position of the powerline. During the application he had flown under it at least 12 times but whilst considering the best method to complete the clean-up runs, he forgot about its presence. The front mounting of the wire deflector had been attached to the top of the fibreglass cockpit and not mounted onto the solid roll-cage framing. When the powerline contacted the wire deflector, the fibreglass failed and allowed the deflector wire to sag under the imposed load. This allowed the powerline to run a lower path and sever the rudder substantially below the rear deflector attach point.

Download Final Report
[ Download PDF: 22KB]
General details
Date: 19 May 1987 Investigation status: Completed 
Time: 1340  
Location:Warunda (24 km NW of Port Lincoln) Investigation type: Occurrence Investigation 
State: South Australia Occurrence type: Wirestrike 
Release date: 18 September 1987 Occurrence class: Operational 
Report status: Final Occurrence category: Accident 
 Highest injury level: None 
Aircraft details
Aircraft manufacturer: Piper Aircraft Corp 
Aircraft model: PA-25 
Aircraft registration: VH-BCP 
Serial number: 25-4386 
Type of operation: Aerial Work 
Damage to aircraft: Substantial 
Departure point:Port Lincoln SA
Departure time:1340
Destination:Port Lincoln SA
Share this page Provide feedback on this investigation