Commonwealth legislation

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

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Airworthiness Directive requires Cessna 310 aeroplanes that previously incorporated Cessna Service Bulletin MEB 88-3 to comply with Revision 1 of that Service Bulletin. Owners/operators must implement the auxiliary fuel-pump wiring modification before the next maintenance release after 31 December 1989; the Civil Aviation Safety Authority says the Directive ensures Revision 1 features are present on already-modified aircraft.

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AD/CESSNA 310/54 - 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 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.

Source text

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