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

The pilot was operating the aircraft from the top of a gently sloping ridge in light and variable wind conditions. He lifted the aircraft into a hover one metre above ground level and began to accelerate forward. At about translational lift speed, the helicopter lost height and the tail rotor struck the ground. The pilot was able to land the aircraft straight ahead. Damage was sustained to the tail rotor drive, gearbox, and blades. The pilot had started work at 0445 hours on the day of the accident. He had flown 4.5 hours and had sprayed five chemical loads prior to the accident. This was the first concentrated period of flying he had undertaken in more than three weeks. Also, it was his first early morning start in that time. Both these aspects could have led to the pilot suffering a degree of transient fatigue. This might have been sufficient to cause a slight degradation in his performance sufficient for him not to compensate fully for the nose-up pitch as the helicopter passed through translational lift. This accident was not the subject of an on-site investigation.

Download Final Report
[ Download PDF: 22KB]
 
 
 
 
General details
Date: 21 December 1988 Investigation status: Completed 
Time: 1030 Investigation type: Occurrence Investigation 
Location:Killarney (31 km ESE Warwick) Occurrence type:Collision with terrain 
State: Queensland Occurrence class: Operational 
Release date: 03 February 1989 Occurrence category: Accident 
Report status: Final Highest injury level: None 
 
Aircraft details
Aircraft manufacturer: Hiller Aviation 
Aircraft model: UH-12 
Aircraft registration: VH-PYH 
Serial number: N/K 
Type of operation: Aerial Work 
Damage to aircraft: Substantial 
Departure point:Killarney QLD
Departure time:N/A
Destination:Killarney QLD
 
 
 
Share this page Provide feedback on this investigation
Last update 13 May 2014