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Download Final Report
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CIRCUMSTANCES: "During a routine maintenance inspection on 2 March 1988 numerous creases were found in the surfaces of both wings. In addition, spar cap rivets were found to be damaged by shear load. The damage was indicative of the aircraft having been subjected to excessive positive `G' loading in flight. The circumstances leading to permanent deformation of the wings were not determined."
Download Final Report
[ Download PDF: 22KB]
 
 
 
 
General details
Date: 01 March 1988 Investigation status: Completed 
 Investigation type: Occurrence Investigation 
 Occurrence type:Airframe - Other 
 Occurrence class: Technical 
Release date: 08 November 1988 Occurrence category: Accident 
Report status: Final  
 
Aircraft details
Aircraft manufacturer: Beech Aircraft Corp 
Aircraft model: 200 
Aircraft registration: VH-IBC 
Sector: Turboprop 
Damage to aircraft: Substantial 
 
 
 
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