AD/BEECH 65/52 - Landing Gear Torque Tube - Inspection and Replacement

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B04148 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Beechcraft 65 and 70 (Queen Air) Series Aeroplanes

 

AD/BEECH 65/52 Landing Gear Torque Tube - Inspection

and Replacement

Applicability: Model 65-B80 with S/Nos. LD-506 to LD-511. Document:  Beechcraft SI No. 1049.

Compliance: Within 100 hours’ time in service after 31 August 1979.


8/79

 

Background: The landing gear torque tube is to be inspected for elongation or double drilling of the bolt hole where the nose gear drive sprocket attaches.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.