Airworthiness Directives 2004 - Revocation and Remaking - Rolls Royce Turbine Engines - Spey Series (Cth)

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