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