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

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 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

 

Overview

The Airworthiness Directives 2004, enacted in 2004, was introduced to address the need for up-to-date and precise regulatory standards in ensuring the airworthiness of aircraft in Australia. This legislative instrument was made under the authority of the Civil Aviation Safety Regulations 1998 by David Alan Villiers, as a delegate of the Civil Aviation Safety Authority, under subregulation 39.001 (1). The primary objective of this legislation is to revoke existing airworthiness directives and re-make them to ensure that the latest safety standards are incorporated, thereby maintaining the highest level of safety in civil aviation. This re-making process ensures that each airworthiness directive is consistent with the most recent published editions, reflecting any necessary updates or amendments to regulatory requirements.

Scope and Application

The Airworthiness Directives 2004, made by the delegate of the Civil Aviation Safety Authority under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, applies to the aviation industry specifically concerning Rolls Royce turbine engines of the RB211 series. These directives mandate certain safety measures and compliance requirements that must be adhered to by aircraft operators, maintenance organisations, and manufacturers involved in the maintenance, operation, and manufacture of these engines. The application of these directives extends nationally, as they are made under Commonwealth regulations and are applicable throughout Australia. The directives do not specify any particular exclusions or exemptions, meaning that they are broadly applicable to all relevant entities and operations within the specified industry. However, the detailed requirements and obligations are outlined in the individual Airworthiness Directives attached to this legislative instrument, which may further define specific conditions or exceptions. The authority to create these directives stems from the Civil Aviation Safety Regulations 1998, allowing for their re-making and modification through subordinate instruments as needed to ensure ongoing compliance with airworthiness standards.

Key Provisions

The Airworthiness Directives 2004, as made by David Alan Villiers under the Civil Aviation Safety Regulations 1998, focus on the revocation and remaking of specific Airworthiness Directives related to Rolls Royce turbine engines of the RB211 series (sections 1(a) and 1(b)). The directives aim to update and reissue existing regulations to ensure that they remain consistent with the latest published editions. These directives cover various aspects of the engines, such as A.V.M. indication, oil pressure, M.E.L. requirements, and numerous other technical specifications and amendments. Each directive is re-made in the same form as the latest version, ensuring that all stakeholders have access to the most current safety and operational standards. The obligations imposed by these directives are primarily on aircraft operators, maintenance providers, and other relevant parties that must comply with the technical standards and specifications outlined in the directives (regulation 39.001(1)). These parties are required to adhere to the detailed maintenance, inspection, and testing protocols to ensure the airworthiness of the engines. This includes conducting specific tests, inspections, and modifications as prescribed in each directive, such as the N3 governor wear resistance test, thrust reverser functional tests, and various compressor and rotor inspections. Ensuring compliance with these directives is critical to maintaining the safety and operational integrity of the aircraft. Failure to comply with the requirements set out in these Airworthiness Directives can result in significant civil and criminal consequences. The severity of penalties varies depending on the nature and extent of the non-compliance. In cases where the non-compliance poses a significant risk to safety, the penalties can be severe, potentially including substantial fines and imprisonment for responsible individuals. The exact penalties are not detailed in the text, but they are likely to be commensurate with the seriousness of the breach and its impact on aviation safety. It is therefore essential for all parties governed by these directives to take their obligations seriously and ensure full compliance to avoid these potential repercussions.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.