Federal Register of Legislation
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
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