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 Life-limited Rotating Engine Components - CANCELLED AD/CF6/42 High Pressure Compressor 3-9 Spool - CANCELLED AD/CF6/43 Amdt 1 High Pressure Turbine Disk - Stage 1 - CANCELLED AD/CF6/44 Fuel Tube Replacement AD/CF6/45 Inspection of Life Limited Parts AD/CF6/46 Low Pressure Turbine Shaft - Life Limit AD/CF6/47 Nozzle Guide Vanes AD/CF6/48 Amdt 1 High Pressure Compressor 3-9 Spool - Inspection AD/CF6/49 High Pressure Turbine - Inspection - CANCELLED AD/CF6/50 LPT Shroud - Replacement AD/CF6/51 Thrust Reverser - Inspection AD/CF6/52 Forward Engine Mount Platforms AD/CF6/53 High Pressure Turbine Disc AD/CF6/54 Vertical Link And Pylon Attachment Bolts AD/CF6/55 HP Stage 1 Turbine Discs AD/CF6/56 HPT S2 NGV Distress AD/CF6/57