AD/CESSNA 320/31 - Auxiliary Fuel Pump Wiring Modification
1AD/CESSNA 320/31 - Auxiliary Fuel Pump Wiring Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Cessna 320 Series Aeroplanes
AD/CESSNA 320/31 Auxiliary Fuel Pump Wiring Modification 12/89
Applicability: All models 320 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.