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At about 400 feet agl on climb, the helicopter suffered a partial loss of engine power. The pilot decided to use the available power to carry out a landing on the airfield. At about 50 feet agl, the engine stopped and the aircraft was subsequently landed heavily, collapsing the skids. The engine had seized. An inspection revealed that the condition of the engine was consistent with that of having been operated without oil. There was no evidence of inflight oil loss or of any component failure which might have caused the loss. When the engine began to lose power the helicopter was climbing at an airspeed of 60 knots. When the engine stopped the helicopter no longer had sufficient performance to allow the successful completion of an auto-rotational approach.

Download Final Report
[ Download PDF: 22KB]
 
 
 
 
General details
Date: 03 August 1985 Investigation status: Completed 
Time: 752 Investigation type: Occurrence Investigation 
Location:Hughenden  
State: Queensland  
Release date: 03 February 1986 Occurrence category: Accident 
Report status: Final Highest injury level: None 
 
Aircraft details
Aircraft manufacturer: Hiller Aviation 
Aircraft model: UH-12 
Aircraft registration: VH-FFX 
Type of operation: Private 
Damage to aircraft: Substantial 
Departure point:Hughenden QLD
Departure time:0752
Destination:Mt Pleasant QLD
 
 
 
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