Document ID: chunk:federal_register_of_legislation:F2006B08009:body:0
Version: federal_register_of_legislation:F2006B08009
Segment Type: other
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Character Range: 0–2556

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 - RB211 Series

 AD Name AD Number

 A.V.M. Indication and Oil Pressure Indication and M.E.L.Requirements,  AD/RB211/1 Amdt 4

 H.P. Compressor Stage 1 and 2 Disc - Removal AD/RB211/2

 Speed and Temperature Governing System AD/RB211/3 Amdt 2

 Group A Parts AD/RB211/4 Amdt 6

 Low Pressure Compressor Rotor (Fan) Axial Retention AD/RB211/5 Amdt 2

 Low Pressure Compressor Rotor (Fan) Axial Retention AD/RB211/6 Amdt 4

 Low Pressure Compressor Rotor (Fan) Shafts Inspection AD/RB211/7

 H.P. Compressor Rotor Stage 4 to 6 Shaft Assembly - Life Limitation AD/RB211/8

 Fan Cowl Support Strut Stowage AD/RB211/9

 High Pressure Compressor Disc AD/RB211/10 Amdt 1

 Fuel Metering Valve Torque Motor Test AD/RB211/11

 N3 Governor with Approved Wear Resistance AD/RB211/12

 Thrust Reverser Functional Test AD/RB211/13

 Thrust Reverser Resolver AD/RB211/14 Amdt 1

 IP Compressor Stage 6-7 Rotor Shaft Life AD/RB211/15

 Fuel Metering Unit - On Wing Test AD/RB211/16 Amdt 1

 Intermediate Pressure Compressor Stage 6-7 Rotor Shafts AD/RB211/17

 Low Pressure Fuel Tube Assembly AD/RB211/18 Amdt 1

 Combustion Liner AD/RB211/19 Amdt 6

 Fuel Flow Governor AD/RB211/20

 Radial Drive Steady Bearing AD/RB211/21 Amdt 2

 Spray Nozzle Fuel Supply Tube - Inspection AD/RB211/22 Amdt 1

 HP Compressor Rotor Shaft to HP Turbine Rotor Disc Retaining Bolts AD/RB211/23

 HP Turbine Disc - Inspection AD/RB211/24 Amdt 1

 Cold Stream Nozzle AD/RB211/25

 LP Compressor Fan Blades AD/RB211/26 Amdt 1

 LP Compressor Fan Blades AD/RB211/27 Amdt 2

 Engine Mounts AD/RB211/28 Amdt 1

 LP Compressor Blades AD/RB211/29 Amdt 1

 Thrust Reverser Inspection AD/RB211/30

 Engine Mount Bush - Replacement AD/RB211/31

 Stage 5 Compressor Disc - Inspection AD/RB211/32 Amdt 1

 High Speed Gearbox and Dedicated Generator - Modifications AD/RB211/33