Commonwealth legislation

AD/PA-32/38 - Quick Disconnect Seat Retention Mechanism - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD requires owners/operators of specified Piper PA‑32‑260 and PA‑32‑300 aeroplanes (listed serial ranges) to inspect the quick‑disconnect seat retention mechanism per Piper Service Letter No. 763, within 100 hours TIS after 30 January 1976. It affects affected aircraft, their maintenance organisations and certifying mechanics; operators bear inspection and repair costs and may face downtime to comply.

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AD/PA-32/38 - Quick Disconnect Seat Retention Mechanism - Inspection

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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-32 (Cherokee Six) Series Aeroplanes

AD/PA-32/38 Quick Disconnect Seat Retention Mechanism - Inspection

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Applicability: Model PA32-260 with S/Nos. 32-01 to 32-7500002. Model PA-32-300 with S/Nos.

32-40001 to 32-7540028.

Document: Piper SL No. 763.

Compliance: Within 100 hours time in service after 30 January 1976.

Source text

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