1AD/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

 

Image unavailable in extracted text 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.