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

The pilot was engaged in mustering operations and was attempting transition from a low forward speed to an out of ground effect hover in order to turn a breakway beast. As he approached the hover, the helicopter experienced a sudden partial power failure. The pilot maintained the aircraft heading, lowered the collective lever and attempted to gain some forward airspeed. In the attempted landing with partial power, the helicopter struck the ground heavily and its main rotor blades hit a small sapling. The forced landing was made in light downwind conditions. Investigation revealed that the No 2 cylinder exhaust valve had failed in fatigue and the valve seat and retaining cap had failed in overload. Further testing indicated that the exhaust valve had been subjected to higher than normal operating temperatures which would have contributed to the premature failure of the valve.

Download Final Report
[ Download PDF: 22KB]
 
 
 
 
General details
Date: 01 May 1986 Investigation status: Completed 
Time: 1345 Investigation type: Occurrence Investigation 
Location:5km East of Theda Station, 50 South of Kalumburu  
State: Western Australia  
Release date: 01 May 1987 Occurrence category: Accident 
Report status: Final Highest injury level: None 
 
Aircraft details
Aircraft manufacturer: Hughes Helicopters 
Aircraft model: 269 
Aircraft registration: VH-THY 
Type of operation: Aerial Work 
Sector: Helicopter 
Damage to aircraft: Substantial 
Departure point:Theda Station WA
Departure time:1345
Destination:Theda Station WA
 
 
 
Share this page Provide feedback on this investigation