AD/LEARJET 35/1 - Primary Control System Stop Bolts - Inspection and Replacement

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Legislation au F2006B11087 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

 


Gates Learjet 35 and 36 Series Aeroplanes

 

AD/LEARJET 35/1  Primary Control System Stop Bolts - Inspection and Replacement

Applicability: All model 35 with S/Nos. 35-001 to 35-039.

 

All model 36 with S/Nos. 36-001 to 36-016.

 

Document: Gates Learjet SB 35/36-27-3.

 

Compliance: Within 300 hours time in service after 30 April 1976.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


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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.