Document ID: chunk:federal_register_of_legislation:F2006B04474:body:0
Version: federal_register_of_legislation:F2006B04474
Segment Type: other
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Character Range: 0–766

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 206/19
 Amdt 1

 Tail Rotor Pedal Controls - Inspection 6/70

            Applicability: All model AB-206A fitted with hydraulically boosted tail rotor pitch control; and All model 206A with S/Nos. 4 to 497.

            Requirement: Check the tail rotor pedal spring and friction adjustment and re- adjust as necessary in accordance with the requirements of Section IV the Maintenance and Overhaul Instructions.

 Compliance: At intervals not exceeding 100 hours time in service. Background: AD/Agusta 206/10A equivalent.