Commonwealth legislation

AD/B-2/29 Amdt 1 - Tail Rotor Drive Shaft - Inspection and Corrosion Proofing

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive mandates that owners/operators of Brantly B‑2, B‑2A and B‑2B helicopters have the tail rotor drive shaft inspected and corrosion‑proofed per Brantly Service Bulletin B2B‑68‑2A. Work must be completed within 10 hours time‑in‑service after 31 December 1968.

It affects all listed airframes and their maintenance providers, imposes immediate cost and scheduling burdens on operators, and relies on the referenced service bulletin for technical steps.

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AD/B-2/29 Amdt 1 - Tail Rotor Drive Shaft - Inspection and Corrosion Proofing

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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 Brantly B-2 Series Helicopters

AD/B-2/29

Amdt 1

Tail Rotor Drive Shaft - Inspection and Corrosion Proofing

12/68

Applicability: All model B2, B2A and B2B. Document: Brantly SB No. B2B-68-2A.

Compliance: Within 10 hours time in service after 31 December 1968.

Source text

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