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

The pilot was conducting joy flights. The aircraft had just been refuelled. During a takeoff, the helicopter reached a height of about 20 feet and an airspeed of approximately 30 knots when engine power decreased briefly and rotor RPM decayed. The helicopter was over a dam at the time. While attempting to reach the nearby bank, the pilot turned downwind and overpitched the main rotors. The helicopter descended into 1.5 metres of fresh water. An engineering examination has disclosed that the right hand magneto had an intermittent fault and that the number three cylinder lower spark plug lead had an intermittent short. The findings cannot be considered to be totally conclusive due to water immersion. However it is considered probable that the engine power loss was an intermittent total spark loss on number three cylinder. This accident was not the subject of an on-scene investigation.

Download Final Report
[ Download PDF: 22KB]
 
 
 
 
General details
Date: 24 November 1990 Investigation status: Completed 
Time: 1458 Investigation type: Occurrence Investigation 
Location   (show map):Lethbridge  
State: Victoria  
Release date: 19 June 1991 Occurrence category: Accident 
Report status: Final Highest injury level: Minor 
 
Aircraft details
Aircraft manufacturer: Hughes Helicopters 
Aircraft model: 269 
Aircraft registration: VH-NCL 
Serial number: 1230265 
Type of operation: Charter 
Sector: Helicopter 
Damage to aircraft: Substantial 
Departure point:Lethbridge VIC
Departure time:N/A
Destination:Lethbridge VIC
 
 
 
Share this page Provide feedback on this investigation