Commonwealth legislation

AD/PA-30/24 - Fuselage Aft Bulkhead - Inspection and Modification

In ForceCTH

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Commonwealth

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legislative instrument

Plain English Summary

3/10 complexity

This CASA airworthiness directive requires owners/operators of specified Piper PA-30 and PA-39 aircraft (by serial number) to inspect the fuselage aft bulkhead and then complete a follow-on modification per Piper Service Letter No. 679; aircraft already fitted with Piper kit P/N 760783 are excluded.

Inspections must occur within 100 hours TIS and repeat at ≤100‑hour intervals until the modification is done; owners/operators bear inspection, repair and modification costs and must use certificated maintenance personnel.

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AD/PA-30/24 - Fuselage Aft Bulkhead - Inspection and 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 Piper PA-30 & 39 (Twin Comanche) Series Aeroplanes

AD/PA-30/24 Fuselage Aft Bulkhead - Inspection

and Modification

3/74

Applicability: All model PA-30 with S/Nos. 30-1 to 30-2000 and all model PA-39 with S/Nos. 39-1 to 39-155 not incorporating kit Piper P/N 760783.

Document: Piper SL No. 679.

Compliance: Within 100 hours time in service after 29 March 1974 and thereafter at intervals not exceeding 100 hours time in service until modified.

Source text

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