AD/CESSNA 400/16 - Elevator Control Bob Weight Arm - Inspection

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

Legislation au F2006B08303 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

 


Cessna 400 Series Aeroplanes

 

AD/CESSNA 400/16  Elevator Control Bob Weight Arm - Inspection


3/70

 

Applicability: All models which have exceeded 1500 hours time in service and are not modified to the satisfaction of the Secretary.

 

Requirement: Inspect the elevator control bob weight arm P/N 5091500-1 for cracking in the vicinity of the weld.

 

Compliance: At intervals not exceeding 100 hours time in service after 1 September 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.