Jump to Content
Download Final Report
[ Download PDF: 13KB]
 
 
 
During the pre-flight inspection the pilot noticed that the left aileron was buckled. Further inspection revealed diagonal wrinking of the lower surface of the left wing, the leading edge of the left wing outboard of the engine nacelle, and evidence of movement in the left wing attachment area. The pilot stated that when he flew the aircraft on the previous day it had handled normally. The weather conditions on that day were such that at cruise the flight was smooth with light turbulence during the descent. An analysis of the damaged aileron concluded that it had failed in static overload. An engineering assessment of the damaged to the aircraft concluded that the most likely scenario to cause the damage was one involving high speeds and gusts. These conditions were not reported by the pilot.
Download Final Report
[ Download PDF: 13KB]
 
 
 
 
General details
Date: 17 November 1994 Investigation status: Completed 
 Investigation type: Occurrence Investigation 
 Occurrence type:Airframe - Other 
 Occurrence class: Technical 
Release date: 12 March 1996 Occurrence category: Accident 
Report status: Final  
 
Aircraft details
Aircraft manufacturer: Beech Aircraft Corp 
Aircraft model: 300LW 
Aircraft registration: VH-KDV 
Sector: Turboprop 
Damage to aircraft: Substantial 
Departure point:Planet Downs
Destination:Canobie
 
 
 
Share this page Provide feedback on this investigation
Last update 21 October 2014