AD/LEARJET 35/11 - Elevator Control System - Modification

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Legislation au F2006B11089 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 35/11 Elevator Control System - Modification 1/79

Applicability: All model 35 with S/Nos. 35-002 to 35-041 and all model 36 with S/Nos. 36-002 to 36-016, unless modified in accordance with Kit Nos. AMK 75-10 or AMK 75-10A.

 

Requirement: To provide for increased reliability of the elevator control system: Modify the aeroplane by installing Kit No. AMK 75-10A.

Compliance: Within 300 hours time in service after 31 January 1979.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.