Document ID: chunk:federal_register_of_legislation:F2006B08010:body:0
Version: federal_register_of_legislation:F2006B08010
Segment Type: other
Provision Reference: 
Character Range: 0–1669

Airworthiness Directives 2004

 I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety
 Authority, acting under subregulation 39.001 (1) of the Civil
 Aviation Safety Regulations 1998:

 (a) revoke the Airworthiness Directives mentioned in
 Schedule 1; and

 (b) make, as separate instruments, each Airworthiness
 Directive mentioned in Schedule 1 and attached.

 David Villiers
 Delegate of the Civil Aviation Safety Authority

  20 December 2004

 Note:   Each attached Airworthiness Directive is being re-made in exactly the
 same form as appears in the latest published edition of the Directive.

 Schedule 1 Revocation and Remaking of
 Airworthiness Directives

 Rolls Royce Turbine Engines - Spey Series

 AD Name AD Number

 Group 'A' Component Lives - CANCELLED AD/RRT-S/1 Amdt 8

 Group 'A' Component Lives - CANCELLED AD/RRT-S/2 Amdt 4

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

 H.P. Fuel Shut Off Valve Primary Strainer - Inspection AD/RRT-S/4 Amdt 1

 In-Field Rectification of Low Power Indication - Performance Monitoring AD/RRT-S/5

 Malfunction of Bleed Valve Mechanism Featuring Mod. 5866 - Operational and  AD/RRT-S/6

 Airflow Control Bleed Valve - Removal of Mod. 5866 AD/RRT-S/7

 Combustion Section - Primary Airscoop AD/RRT-S/8

 Transply Combustion Liners AD/RRT-S/9

 HP2 Turbine Disc Locating Sleeve AD/RRT-S/10

 Steel Turbine Discs AD/RRT-S/11

 Stage 2 Low Pressure Turbine Blades - CANCELLED AD/RRT-S/12 Amdt 2

 Low Pressure Turbine Stage 2 NGV Seal Support AD/RRT-S/13 Amdt 1

 LPT Stage 2 NGV Seal Support AD/RRT-S/14

 Stage 2 Low Pressure Turbine Blades AD/RRT-S/15