Document ID: chunk:federal_register_of_legislation:F2006B07882:body:0:p1
Version: federal_register_of_legislation:F2006B07882
Segment Type: other
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Character Range: 1–3215

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

 Eddy Current Inspection of High Pressure Turbine Thermal Shields AD/CF6/21

 Fuel Manifold Inspection and Replacement AD/CF6/22

 High Pressure Turbine Rotor Stage 1 Disc/Shaft Inspection and Removal From  AD/CF6/23

 High Pressure Compressor Rotor Spools Stages 3 to 9 - CANCELLED AD/CF6/24 Amdt 2

 Fan Disks - Removal From Service AD/CF6/25

 Stage 11 to 13 Compressor Spool Inspection AD/CF6/26

 High Pressure Turbine Thermal Shield Inspection AD/CF6/27

 CF6-80C2 Stage 1 High Pressure Turbine Disc Inspection AD/CF6/28

 High Pressure Turbine - Stage 1 Disc Rim Bolt Holes and Stage 2 Disc Rim and  AD/CF6/29 Amdt 1

 CF6-80A Stage 1 High Pressure Turbine Disc Inspection AD/CF6/30

 Fan Stator Case Stiffening Ring and Stage 1 Fan Shroud AD/CF6/31

 Oil Quantity and Flame Arrestor Plug AD/CF6/32

 HPT Stage 2 Disk Life Limits AD/CF6/33

 Fan Reverser Centre Drive Unit AD/CF6/34

 Compressor Rear Frame Midflange AD/CF6/35

 Forward Engine Mount Assembly AD/CF6/36

 High Pressure Compressor Rotor (HPCR) Stages 3-9 - Replacement AD/CF6/37

 Stage 1 Fan Disk Inspection AD/CF6/38

 Accessory Gearbox Idler Adaptor - Inspection AD/CF6/39

 Fan Mid Shaft AD/CF6/40

 High Pressure Compressor 3-9 Spool - CANCELLED AD/CF6/41 Amdt 1

 Inspection of Critical