Commonwealth legislation

AD/CESSNA 320/31 - Auxiliary Fuel Pump Wiring Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive requires Cessna 320 aeroplanes that were previously modified under Cessna Service Bulletin MEB 88‑3 to incorporate the wiring changes in Revision 1 of that bulletin. It applies only to Model 320 aeroplanes that have already incorporated the original SB and must be done before the next Maintenance Release issued after 31 December 1989. The Civil Aviation Safety Authority mandates compliance, and operators must fund and schedule the retrofit work to meet the deadline.

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AD/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

View image in the official source 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.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.