Commonwealth legislation

AD/JT8D/8 - Second Stage Fan Blade Pin Rivets

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

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Airworthiness Directive AD/JT8D/8 applies to JT8D‑9, ‑11, ‑15 and ‑17 engines fitted with second‑stage fan pin P/N 520456, rivet P/N 520457 and bushing P/N 520458 and requires operators to carry out the actions set out in the referenced Requirement Document (FAA AD 76‑12‑06 or AD/PW‑T/36).

This places inspection, repair/replacement, record‑keeping and downtime costs on operators and matters because compliance depends on correctly identifying affected engines and following the external maintenance instructions.

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Current sections

Direct links to the current provisions in AD/JT8D/8 - Second Stage Fan Blade Pin Rivets.

AD/JT8D/8 - Second Stage Fan Blade Pin Rivets

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Pratt and Whitney Turbine Engines - JT8D Series

AD/JT8D/8 Second Stage Fan Blade Pin Rivets 7/76

Applicability: All JT8D-9, -11, -15 and -17 engines containing second stage fan blade pin P/N 520456, rivet P/N 520457 and bushing P/N 520458.

Document: 1. FAA AD 76-12-06 : Amendment 39-2639; or

AD/PW-T/36.

Compliance: As detailed in the Requirement Document.

Source text

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