Jump to Content
Download Final Report
[ Download PDF: 16KB]
The pilot reported that he was in the Coolangatta training area practising forced landing procedures with a student pilot. An autorotation was entered by lowering collective initially, then the throttle was wound off. Carburettor heat was selected fully on, carburettor air temperature was indicating approximately 12 degrees Celsius, and the engine was idling. The pilot said he turned towards the forced landing area and was briefing the student on the wind direction. The rotor RPM was in the green range and indicated airspeed was 55 knots, the correct autorotation airspeed. The pilot said that at this stage he was downwind (5-10 knots approx) and was ready to turn into wind at approximately 300 ft AGL. The collective was raised and the throttle was opened fully, but the manifold pressure increased only to 14-15 inches, there was a definite lack of power and the rotor RPM decayed. He maintained heading and airspeed and re-entered autorotation heading for the forced landing area when he noticed the engine had stopped. He said he attempted a restart but at this stage he was too low to risk a turn and accepted his present direction. The landing was made onto a tree lined track. The main rotor contacted trees and the aircraft rolled over to the right on the sandy surface. The pilot suspected that carburettor icing may have been the problem. The weather conditions at the time were light drizzle or rain with a temperature of 18 -20 deg C. These conditions were conducive to carburettor icing. The pilot said that he had experienced power loss with this type of helicopter in similar situations, but usually on the initial entry into the autorotation. The aircraft manufacturer carried a technical investigation and found no evidence of any failure or malfunction that may have led to the accident. The manufacturer stated that the carburettor heat fully applied in autorotation produces an indication on the carb air temp gauge of full scale deflection. However, this has not been the operators experience. The operator advised that with full carb heat the temperature remains in the mid (caution) range and pilots have been advised to terminate autorotations and apply power if the carb air temp falls below this value. The operator now requires pilots to practice autorotations over a clear landing site, so that a landing may be terminated should the situation recurr.
Download Final Report
[ Download PDF: 16KB]
General details
Date: 08 May 1997 Investigation status: Completed 
Time: 13:30 EST  
 Investigation type: Occurrence Investigation 
 Occurrence type: Forced/precautionary landing 
Release date: 22 July 1997  
Report status: Final Occurrence category: Accident 
Aircraft details
Aircraft manufacturer: Schweizer Aircraft Corp 
Aircraft model: 269C-1 
Aircraft registration: VH-CBZ 
Sector: Helicopter 
Damage to aircraft: Substantial 
Departure point:Coolangatta QLD
Destination:Coolangatta QLD
Share this page Provide feedback on this investigation
Last update 28 October 2014