Jump to Content
Download Final Report
[ Download PDF: 15KB]
The glider was nearing the end of a 190 km cross country flight. The weather was fine, with good visibility and light west to north westerly winds. At about five km from the airfield the pilot decided to descend from 3,500 ft by increasing airspeed to 116 kt, some 3 kt less than the maximum airspeed limit. The pilot reported that initially the glider was flying normally at this speed, but suddenly the control stick was pulled from his grasp and vibrated back and forth, banging against its stops. He managed to regain his hold on the stick and began to raise the nose of the aircraft to reduce airspeed. At this point the glider rolled into an inverted attitude. Believing that the aircraft had suffered a major structural failure, the pilot elected to escape from the cockpit and make a parachute descent. Initially, he experienced difficulty in releasing the canopy, but once open he fell freely from the glider. The pilot made a successful parachute descent, whilst the glider proceeded to land in bushes, sustaining minimal damage. During a subsequent airworthiness inspection by the gliding authority, it was found that the mass balance of the tailplane was beyond limits. The out of balance condition had apparently occurred some three years previously when the glider had been rebuilt. As a result, elevator flutter had occurred as the aircraft reached its maximum airspeed limit. Under normal circumstances the critical airspeed for the onset of elevator flutter should have been well in excess of the maximum airspeed limit. The gliding authority has advised that it has taken action to prevent a recurrence by issuing an airworthiness directive, and conducting surveillance of the maintenance organisation concerned.
Download Final Report
[ Download PDF: 15KB]
General details
Date: 07 October 1995 Investigation status: Completed 
Time: 15:25 EST  
 Investigation type: Occurrence Investigation 
 Occurrence type: Flight control systems 
Release date: 02 May 1996 Occurrence class: Technical 
Report status: Final Occurrence category: Incident 
Aircraft details
Aircraft manufacturer: Schempp-Hirth Flugzeugbau GmbH 
Aircraft model: CIRRUS 75 
Aircraft registration: VH-XQZ 
Sector: Other 
Damage to aircraft: Minor 
Departure point:Central Mangrove NSW
Destination:Central Mangrove NSW
Share this page Provide feedback on this investigation
Last update 21 October 2014