Commonwealth legislation

AD/HU 369/34 Amdt 1 - Tail Rotor Hub - Inspection and Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This Airworthiness Directive (AD/HU 369/34 Amdt 1) mandates inspection and modification of specified tail rotor hub assemblies and blade attachment bolts on 500 model 369H Series helicopters, by requiring compliance with Hughes Service Information Note HN-128.1.

It affects owners/operators of those helicopters listed in the SIN, who must follow the Hughes procedures (and bear associated costs/downtime) under the Commonwealth Part 39 airworthiness regime.

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AD/HU 369/34 Amdt 1 - Tail Rotor Hub - 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 McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters

AD/HU 369/34

Amdt 1

Tail Rotor Hub - Inspection and Modification 4/79

Applicability: All 500 model 369H Series with tail rotor hub assemblies and tail rotor blade attachment bolts as listed in Hughes SIN No. HN-128.1.

Document: Hughes SIN No. HN-128.1. Compliance: As per requirement document.

Source text

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