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

During the take-off roll the aircraft did not achieve flying speed by the point where it was normally expected to become airborne. The pilot abandoned the take-off and applied maximum braking, but was unable to prevent the aircraft over-running the strip. The aircraft broke through the boundary fence and came to rest in a small ditch. The reason the aircraft did not achieve flying speed could not be positively determined. In this aircraft type, it is important that the elevator trim is correctly set for take-off. If nose-down trim is inadvertently applied, excessive rearward pressure is required on the control column in order to raise the nose. However, the trim position set by the pilot was not established. When the take-off attempt was abandoned, there was probably sufficient strip remaining to stop the aircraft. However, the brake linings and discs were worn to the extent where full brake effectiveness could not be obtained.

Download Final Report
[ Download PDF: 22KB]
 
 
 
 
General details
Date: 03 February 1985 Investigation status: Completed 
Time: N/A Investigation type: Occurrence Investigation 
Location:Wilton Occurrence type:Runway excursion 
State: New South Wales Occurrence class: Operational 
Release date: 17 April 1986 Occurrence category: Accident 
Report status: Final Highest injury level: None 
 
Aircraft details
Aircraft manufacturer: Pilatus Britten-Norman Ltd 
Aircraft model: BN2 
Aircraft registration: VH-IGT 
Type of operation: Private 
Damage to aircraft: Substantial 
Departure point:Wilton NSW
Departure time:N/A
Destination:Wilton NSW
 
 
 
Share this page Provide feedback on this investigation