Jump to Content
Download Final Report
[ Download PDF: 22KB]

Following a normal approach for a night landing, touchdown was made on the main landing gear. The pilot then noticed that the nose was lowering by an excessive amount, and he carried out a successful go around. Examinations from the ground and from a helicopter equipped with a searchlight revealed that the nosegear was inclined at about 30 degrees to the vertical. The position of the nosegear did not alter when the gear was cycled. After all attempts to lower the nosegear were unsuccessful, the pilot elected to carry out a landing with the maingear retracted. He was unable to use the grass flight strip alongside the lighted runway because of obstructions, and chose to land on an unlit strip. The left engine failed because of fuel exhaustion when the aircraft was on final approach. After touchdown, the aircraft slid off the end of the strip and came to rest against the boundary fence. It was determined that the nosegear retract rod plunger had failed from fatigue, resulting in the nosegear being isolated from the remainder of the landing gear system.

Download Final Report
[ Download PDF: 22KB]
General details
Date: 19 June 1987 Investigation status: Completed 
Time: 2101  
Location:Bankstown Investigation type: Occurrence Investigation 
State: New South Wales Occurrence type: Wheels up landing 
Release date: 18 September 1987 Occurrence class: Operational 
Report status: Final Occurrence category: Accident 
 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:Bankstown NSW
Departure time:2101
Destination:Sydney NSW
Share this page Provide feedback on this investigation