AD/BELL 206/44 - Rotor Brake Disc Assembly P/N 4000071 - Inspection and Modification

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B04500 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters

 

AD/BELL 206/44 Rotor Brake Disc Assembly

P/N 4000071 - Inspection and Modification

Applicability: All models fitted with rotor brake kit P/N 206-706-032-1. Document:  Bell SB No. 206-50-73-2.


5/73

Compliance: 1. For Part 1 of SB 206-50-73-2 For helicopters estimated to have had 300 or more rotor brake stops - within the next 25 rotor brake applications after 19 April 1973. For helicopters estimated to have had less than 300 rotor brake stops - prior to 325 rotor brake stops.

 

2. For Part 2 of SB 206-50-73-2: At intervals not exceeding 300 hours time in service.

 

Background: AD/Agusta 206/33 equivalent.

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.