Airworthiness Directives 2004 - Revocation and Remaking - Rolls Royce Turbine Engines - RB211 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 - 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