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The particular aircraft is a glider fitted with a retractable engine. Shortly after takeoff for a soaring flight, the pilot noticed that the airspeed indicator (ASI) appeared to be operating erratically. The flight was continued with the pilot estimating the airspeed, but no thermals were found and the pilot decided to return to the departure point using engine power. The aircraft stalled during the landing flare and the left wing struck the ground. The aircraft slewed to the left and touched down while travelling sideways. The fuselage was fractured during the ensuing ground slide. The approach was flown with landing flap and a substantial degree of air-brake deployed. With the engine also extended the glider was in an extremely high drag situation. Although the flight manual is specific about the degradation in performance of the glider with the engine extended, the pilot reported that his endorsement training failed to adequately address this aspect. Investigation also revealed that some dirt and insects were present in the pitot/static plumbing connected to the ASI. These may have caused the reported erratic readings during the initial stages of the flight.

Download Final Report
[ Download PDF: 22KB]
 
 
 
 
General details
Date: 02 April 1987 Investigation status: Completed 
Time: 1320 Investigation type: Occurrence Investigation 
Location:Lilydale Occurrence type:Loss of control 
State: Victoria Occurrence class: Operational 
Release date: 14 August 1987 Occurrence category: Accident 
Report status: Final Highest injury level: None 
 
Aircraft details
Aircraft manufacturer: Eiriavion Oy 
Aircraft model: PIK-20 
Aircraft registration: VH-MQN 
Serial number: 20298 
Type of operation: Gliding 
Damage to aircraft: Substantial 
Departure point:Lilydale VIC
Departure time:1255
Destination:Lilydale VIC
 
 
 
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Last update 13 May 2014