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 - CJ610 Series
AD Name AD Number
Major Rotating Components - Life Limits - CANCELLED AD/CJ610/1
Stage 1 Turbine Wheels AD/CJ610/2
Stage 2 Turbine Wheels AD/CJ610/3
Outer Combustion Casing AD/CJ610/4
Compressor Discs AD/CJ610/5
Stage 2 Turbine Wheels AD/CJ610/6
Overview
The Airworthiness Directives 2004, issued by David Alan Villiers, a delegate of the Civil Aviation Safety Authority (CASA), under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, represent a significant update to aviation safety standards in Australia. This legislative instrument was enacted to address the need for updated and consolidated airworthiness directives to ensure the safety and reliability of aircraft operations. The directives were revoked and remade to reflect the latest published editions, thereby maintaining consistency and currency with international standards. The policy objective underpinning this action was to ensure that the civil aviation sector adheres to the highest safety protocols, thereby protecting the public and enhancing the overall safety of air travel within Australia.
The enactment of the Airworthiness Directives 2004 by the Civil Aviation Safety Authority aimed to fill a critical gap in ensuring that specific components of aircraft engines, such as turbine wheels and combustion casings, meet stringent safety standards. By revoking and remaking the directives, CASA ensured that the aviation industry complies with the most current safety requirements, thus reducing the risk of mechanical failure and enhancing the safety of air travel. This legislative action underscores the commitment of CASA to maintaining and improving aviation safety standards in Australia.
Scope and Application
The Airworthiness Directives 2004, promulgated by David Alan Villiers as the delegate of the Civil Aviation Safety Authority (CASA), operates within the scope of the Civil Aviation Safety Regulations 1998. This legislative instrument primarily applies to airworthy aircraft and their components, specifically targeting entities and individuals involved in the aviation industry who must comply with the directives concerning the maintenance and safety of certain aircraft components. The geographic reach of this legislation is nationwide, affecting all aviation entities operating within Australia, as it falls under the regulatory purview of the Commonwealth. The instrument revokes and remakes several specific Airworthiness Directives pertaining to General Electric Turbine Engines of the CJ610 Series, ensuring the adherence to updated safety standards for these components. The revocation and remaking of these directives are detailed in Schedule 1, which lists each directive to be cancelled and re-issued in their current form, thereby maintaining the integrity and safety of Australian airspace.
Key Provisions
The Airworthiness Directives 2004 primarily serve to revoke existing airworthiness directives related to General Electric Turbine Engines of the CJ610 series and re-make them as separate instruments. This legislative instrument is issued under the authority of David Alan Villiers, a delegate of the Civil Aviation Safety Authority (CASA), pursuant to subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The directives that are revoked and subsequently re-made are listed in Schedule 1, which includes specific directives related to major rotating components such as turbine wheels, outer combustion casing, and compressor discs.
Under the Airworthiness Directives 2004, the main operative sections require the revocation of previously issued airworthiness directives for certain components of the CJ610 series turbine engines. These include directives concerning Stage 1 Turbine Wheels (AD/CJ610/1), Stage 2 Turbine Wheels (AD/CJ610/2 and AD/CJ610/5), Outer Combustion Casing (AD/CJ610/3), and Compressor Discs (AD/CJ610/4). Each of these directives is then re-made in the same form as it appears in the latest published edition, ensuring that the most current safety standards and requirements are applied.
The obligations imposed by these directives are primarily on aircraft operators and maintenance personnel. They must ensure that the components specified in the re-made directives are maintained and inspected in accordance with the detailed requirements set out in each directive. This includes adherence to specified life limits, inspection intervals, and corrective actions to be taken if any issues are identified. Failure to comply with these obligations can result in serious safety risks, including potential engine failure or other in-flight incidents.
There are potential civil and criminal consequences for breaches of these airworthiness directives. Specifically, non-compliance with these directives can be seen as a violation of the Civil Aviation Safety Regulations 1998, which could result in enforcement actions by CASA. The potential penalties for such breaches can include fines, the grounding of non-compliant aircraft, or other regulatory actions deemed necessary to ensure compliance. The exact penalties may vary depending on the severity and frequency of the breach, but they can be substantial, underscoring the importance of strict adherence to the directives.