Document ID: chunk:federal_register_of_legislation:F2006B04500:body:0
Version: federal_register_of_legislation:F2006B04500
Segment Type: other
Provision Reference: 
Character Range: 0–892

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.