Commonwealth legislation

AD/B-2/27 - Tail Rotor Blades Strike Indicators - Installation

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

A safety directive requires owners/operators of Brantly B‑2 series helicopters (B2, B2A, B2B) with serial numbers below 474 to install tail‑rotor blade‑strike indicators within 100 flight hours from 21 March 1968, using the instructions in Brantly Service Letter No. 73. The devices reveal otherwise hidden tail‑rotor strikes, helping detect damage that could lead to catastrophic loss of control.

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AD/B-2/27 - Tail Rotor Blades Strike Indicators - Installation

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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-2/27 Tail Rotor Blades Strike Indicators - Installation 2/68

Applicability: All model B2, B2A and B2B prior to S/No. 474. Document: Brantly SL No. 73.

Compliance: Within 100 hours time in service after 21 March 1968.

Source text

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