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

Spraying runs were being conducted over a paddock which had power lines along one boundary. The pilot had been passing beneath the lines during each run, however after completing about two thirds of the task the wire deflector on the aircraft snagged and broke the powerline. The pilot carried out a precautionary landing and discovered that the rudder of the aircraft had been substantially damaged by the wire strike. At the point where the wire strike occurred there was less clearance between the wires and the ground than that available during previous swath runs. The pilot was aware of the situation, but had been subject to a visual illusion, which had led him to believe that there was sufficient clearance to allow the aircraft to pass beneath the wires. By the time he realised that the clearance was insufficient he was unable to take avoiding action, and had elected to allow the wire to strike the deflector, rather than risk the landing gear contacting the ground. The anti-snag deflector plate on top of the rudder had failed, allowing the wire to contact the rudder. The upper portion of this component had then been torn from the aircraft.

Download Final Report
[ Download PDF: 22KB]
 
 
 
 
General details
Date: 28 November 1986 Investigation status: Completed 
Time: 1040 Investigation type: Occurrence Investigation 
Location:Rupanyup (17 km ENE Horsham) Occurrence type:Wirestrike 
State: Victoria Occurrence class: Operational 
Release date: 12 May 1987 Occurrence category: Accident 
Report status: Final Highest injury level: None 
 
Aircraft details
Aircraft manufacturer: Piper Aircraft Corp 
Aircraft model: PA-25 
Aircraft registration: VH-FAN 
Type of operation: Aerial Work 
Damage to aircraft: Substantial 
Departure point:Rupanyup VIC
Departure time:1040
Destination:Rupanyup VIC
 
 
 
Share this page Provide feedback on this investigation