Commonwealth legislation

AD/B727/85 - Main Landing Gear Side Strut

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This Airworthiness Directive applies to Boeing 727s (line numbers 1–1361) and, because incorrect parts may have been fitted in main‑landing‑gear side strut assemblies, mandates compliance with FAA AD 79‑20‑06 as the operative technical requirement. Affected operators must obtain and follow that FAA AD (and the cited Boeing service bulletin) for the specific inspections and corrective actions; the AD itself delegates technical detail rather than reproducing it.

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AD/B727/85 - Main Landing Gear Side Strut

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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 Boeing 727 Series Aeroplanes

AD/B727/85 Main Landing Gear Side Strut 1/80

Applicability: All model 727 with line numbers 1 to 1361 inclusive. Document: 1. FAA AD 79-20-06, Amdt. 39-3581; or

Boeing SB No. 727-32-268, Rev. 1.

Compliance: As per requirement document No. 1.

Background: Incorrect parts may have been installed in the M-L-G side strut assemblies at manufacture.

Source text

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