AD/CESSNA 310/54 - Auxiliary Fuel Pump Wiring Modification

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

Legislation au F2006B08181 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 310 Series Aeroplanes

 

AD/CESSNA 310/54 Auxiliary Fuel Pump Wiring Modification 12/89

Applicability: All models 310 which have been modified in accordance with Cessna Service Bulletin MEB 88-3.

 

Requirement: Unless already accomplished, action in accordance with Cessna Service Bulletin MEB 88-3 Revision 1.

 

Note: This Requirement does not apply to aeroplanes that have not incorporated SB MEB 88-3.

 

Compliance: Prior to the issue of the next Maintenance Release after 31 December 1989.

 

Background: Compliance with the original issue of SB MEB88-3 was not considered to warrant the issue of an Airworthiness Directive. This AD is raised to ensure that necessary features of Revision 1 are incorporated into modified aeroplanes.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.