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The aircraft was cleared via a Standard Instrument DEPARTURE with an unrestricted climb to Flight Level (FL) 220. The aircraft climbed on track at an average rate of 1300 ft/min until FL130. The rate of climb then reduced to 350 ft/min until FL140, when the rate of climb increased to 1800 ft/min. At FL160 the aircraft entered a near vertical descent and radar contact was lost one minute later at 3100 feet. The aircraft impacted the ground in a near vertical attitude. Despite an extensive investigation, the reason for the loss of control leading to this accident could not be determined. There have been several other reported occurrences involving sudden loss of control in this aircraft type and the United States Federal Aviation Administration has conducted a certification review of the type. The results of that review do not appear to indicate any factors relevant to this particular accident.

Download Final Report
[ Download PDF: 22KB]
 
 
 
 
General details
Date: 24 May 1983 Investigation status: Completed 
Time: 433 Investigation type: Occurrence Investigation 
Location:2 km East of Bargo Occurrence type:Collision with terrain 
State: New South Wales Occurrence class: Operational 
Release date: 16 April 1986 Occurrence category: Accident 
Report status: Final Highest injury level: Fatal 
 
Aircraft details
Aircraft manufacturer: Mitsubishi Aircraft Int 
Aircraft model: MU-2 
Aircraft registration: VH-MLU 
Type of operation: Charter 
Damage to aircraft: Destroyed 
Departure point:Sydney NSW
Departure time:0433
Destination:Melbourne VIC
 
 
 
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Last update 13 May 2014