Airworthiness Directives 2004 - Revocation and Remaking - General Electric Turbine Engines - CF6 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

General Electric Turbine Engines - CF6 Series

AD Name AD Number

CF6-50 Life Limits - Engine Components - CANCELLED AD/CF6/1 Amdt 1

CF6-80 Life Limits - Engine Components - CANCELLED AD/CF6/2 Amdt 1

First Stage High Pressure Turbine Discs - CANCELLED AD/CF6/3

High Pressure Turbine Rotor Spacer/Impeller Inspection Requirements - AD/CF6/4

Fuel Supply Manifold AD/CF6/5

First Stage High Pressure Turbine Disc Embossment Radii AD/CF6/6

First Stage High Pressure Turbine Disc Embossment Radii AD/CF6/7

Low Pressure Turbine Cooling Air Manifold AD/CF6/8

High Pressure Turbine Impeller Spacer Eddy Current Inspection AD/CF6/9

Fuel Manifold AD/CF6/10 Amdt 1

High Pressure Turbine Rotor - Stage 2 Disc Forward Embossment Inner AD/CF6/11

Turbine Mid Frame Aft Circumferential Weld AD/CF6/12 Amdt 2

Accessory Compartment Fire Shields AD/CF6/13

High Pressure Turbine Discs AD/CF6/14

High Pressure Compressor Rear Shaft Bolt Hole AD/CF6/15 Amdt 2

Fuel Manifold Support Bracket AD/CF6/16

Stage 1 Fan Rotor Disc AD/CF6/17

High Pressure Turbine Inspection and Improved Shroud Cooling AD/CF6/18

High Pressure Compressor Rotor Inertia Weld AD/CF6/19

High Pressure Compressor Rotor Stages 11 to 14 Vane to Spool Rubs AD/CF6/20