Commonwealth legislation

AD/P68/12 - Propeller Control Rod End - Inspection and Replacement

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD requires owners/operators of Partenavia P68 and P68B aircraft with serial numbers below 160 to inspect the propeller control rod end within 50 hours TIS from 17 Oct 1978 and repeat every 50 hours until Part 2 of Partenavia Service Bulletin No. 37, Rev.1 is completed. Maintenance organisations must carry out replacements as indicated, following the Service Bulletin’s procedures, creating a recurring maintenance burden and dependence on the SB to terminate the inspections.

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AD/P68/12 - Propeller Control Rod End - Inspection and Replacement

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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 Partenavia P68 Series Aeroplanes

AD/P68/12 Propeller Control Rod End - Inspection

and Replacement Applicability: All models P68 and P68B with S/Nos. below 160. Document: Partenavia SB No. 37, Revision 1.

11/78

Compliance: Within 50 hours time in service after 17 October 1978 and thereafter at intervals not exceeding 50 hours time in service until Part 2 of Partenavia SB No. 37, Revision 1 is completed.

Source text

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