AD/AC-CLA/5 - Shock Strut Assembly

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

Legislation au F2006B02198 Not in force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Aircraft Parts and Development (CALL AIR) A-9 Series Aeroplanes

 

AD/AC-CLA/5 Shock Strut Assembly 4/75

Applicability: All A-9 series.

 

Requirement: Main landing gear shock strut assemblies P/N 12018 shall be disassembled and inspected for general condition.

 

Note: Particular attention should be paid to the bore of the tube for reduction of wall thickness due to contact with the inner spring.

 

Compliance: At next major inspection after 30 April 1975 and thereafter at each major inspection.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.