Commonwealth legislation

AD/PA-28/56 - Quick-Disconnect Seat Retention Mechanism - Inspection

In ForceCTH

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Commonwealth

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legislative instrument

Plain English Summary

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This Airworthiness Directive mandates an inspection of the quick‑disconnect seat retention mechanism on specified Piper PA‑28 series aircraft (listed by model/serial range) to be completed within 100 hours TIS after 30 January 1976. The AD refers to Piper SL No. 763 for technical procedures.

Owners/operators are responsible for compliance and will bear inspection, repair and downtime costs; maintenance organizations perform the work and must consult the referenced Piper document for inspection criteria.

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AD/PA-28/56 - 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-28 Series Aeroplanes

AD/PA-28/56 Quick-Disconnect Seat Retention Mechanism - Inspection

Applicability: Model PA-28-180 with S/Nos. 28-7105001 to 28-7505046.

Model PA-28R-180 with S/Nos. 28R-7130001 to 28R-7130013. Model PA-28R-200 with S/Nos. 28R-7135001 to 28R-7535041. Model PA-28-235 with S/Nos. 28-7110001 to 28-7510016.

Document: Piper SL No. 763.

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

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Source text

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