Document ID: chunk:federal_register_of_legislation:F2006B06684:body:0
Version: federal_register_of_legislation:F2006B06684
Segment Type: other
Provision Reference: 
Character Range: 0–593

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Rolls Royce Turbine Engines - Spey Series

 AD/RRT-S/3 Stage 2 and 3 H.P. Compressor Discs - Increased
                     Thickness Neck and Diaphragm

 9/74

 Applicability: Spey 505-5F, 506-14, 506-14A, 506-14AW, 506-14D, 511-5W, 511-8, 511-14, 511-
            14W, 555-15.

 Requirement: Rolls Royce Spey SB No. Sp 72-715 Part 1 and Part 2.

 Compliance: As per the requirement document or at 4000 disc cycles, whichever occurs first.