Document ID: chunk:federal_register_of_legislation:F2006B08273:body:0
Version: federal_register_of_legislation:F2006B08273
Segment Type: other
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Character Range: 0–939

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Cessna 340 Series Aeroplanes

AD/CESSNA 340/28 Auxiliary Fuel Pump Wiring Modification 12/89

            Applicability: All models 340 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 MEB 88-3 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.