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The pilot reported that he had obtained normal indications when he selected the landing gear down. The subsequent touchdown was normal but as the nosewheel was lowered to the ground, the nose gear leg collapsed. The eyebolt between the nose gear retract aft rod and the landing gear motor had failed, resulting in the nose gear failing to lock down and allowing it to retract on ground contact. The eyebolt had failed at the beginning of the thread, adjacent to the eye. Specialist examination indicated that the initial fracture was indicative of fatigue and had been present for some time. The aircraft had only recently been returned to service following an earlier accident which involved a fatigue failure of the nose gear retract rod plunger fork. It was considered likely that the fracture had initiated at the same time as the earlier failure.

Download Final Report
[ Download PDF: 22KB]
 
 
 
 
General details
Date: 28 April 1988 Investigation status: Completed 
Time: 735 Investigation type: Occurrence Investigation 
Location:Warkworth Occurrence type:Wheels up landing 
State: New South Wales Occurrence class: Operational 
Release date: 07 February 1989 Occurrence category: Accident 
Report status: Final Highest injury level: None 
 
Aircraft details
Aircraft manufacturer: Beech Aircraft Corp 
Aircraft model: 55 
Aircraft registration: VH-MKE 
Serial number: TE-592 
Type of operation: Charter 
Damage to aircraft: Substantial 
Departure point:Maitland NSW
Departure time:0725
Destination:Warkworth NSW
 
 
 
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