AD/BEECH 55/28 - Landing Gear Upper and Lower Torque Link Clevis Pins

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

Legislation au F2006B03977 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

 


Beechcraft 55, 58 and 95-55 (Baron) Series Aeroplanes

 

AD/BEECH 55/28 Landing Gear Upper and Lower

Torque Link Clevis Pins

Applicability: All models which have exceeded 1000 hours’ time in service.


3/72

 

Requirement: Remove and inspect the AN or MS lock pins in the upper and lower torque link clevis pins on the main and nose landing gear assemblies. Any pins which exhibit wear or corrosion shall be replaced.

 

Compliance: Within 100 hours’ time in service after 29 March 1972 and thereafter at intervals not exceeding 3 years.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.