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 - Viper Series
AD Name AD Number
Life Limits Group 'A' Parts - CANCELLED AD/VIPER/1
Life Limits Group 'A' Parts - CANCELLED AD/VIPER/2
Blow Off Valve Operation Limit AD/VIPER/3
Blow-Off Valve AD/VIPER/4
Exhaust Cone Assembly AD/VIPER/5
Blow-Off Valve Operating Limit AD/VIPER/6
Oil Tank Drain Valve AD/VIPER/7
Oil Tank and Oil Pump Drain Valves AD/VIPER/8
Engine Centre Section AD/VIPER/9
Overview
The Airworthiness Directives 2004, enacted on 20 December 2004, are a legislative instrument that serves to revoke and re-make specific Airworthiness Directives, as outlined in the schedule. This legislative instrument was introduced by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, who acted under the authority granted by subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The objective of these directives is to ensure that airworthiness standards are consistently applied and updated to maintain the safety and reliability of aircraft operations, specifically targeting Rolls Royce Turbine Engines - Viper Series. Each Airworthiness Directive is re-made to reflect the latest published edition, ensuring compliance with current safety standards and practices.
Scope and Application
The Airworthiness Directives 2004, made by David Alan Villiers as a delegate of the Civil Aviation Safety Authority, pertains to the revocation and remaking of specific airworthiness directives concerning Rolls Royce Turbine Engines of the Viper Series. This legislative instrument applies to all entities involved in the design, manufacture, maintenance, or operation of the specified turbine engines, as well as to the aviation industry at large. The directives are applicable nationally, extending their reach across all states and territories within Australia. The legislation specifically addresses particular components of the Viper Series engines, such as the blow-off valve operation, exhaust cone assembly, and oil tank drain valves, among others, by setting out mandatory requirements and limits for their operational life and maintenance. Notably, this instrument does not specify exclusions or thresholds, but rather operates on the principle that all applicable entities must adhere to the newly remade directives as detailed in the attached schedules. The authority to extend or restrict the application of these directives is vested in subordinate instruments, which may further elaborate on specific operational contexts or additional components as required.
Key Provisions
The key sections of this legislative instrument, F2006B08012, concern the revocation and remaking of specific Airworthiness Directives related to Rolls Royce turbine engines, specifically the Viper series. Section 1(a) revokes the Airworthiness Directives listed in Schedule 1, while section 1(b) mandates the remaking of these directives as separate instruments, ensuring that they are attached to the legislative instrument. Each of these directives is reproduced exactly as they appear in the latest published edition, preserving their original form and content.
The obligations imposed by this legislative instrument are primarily administrative. The Civil Aviation Safety Authority (CASA) is tasked with ensuring that the revoked directives are removed from the regulatory framework and that the remade directives are correctly re-established. This involves meticulous record-keeping and verification to ensure that the changes are accurately reflected in the official documentation. Furthermore, relevant stakeholders, such as aircraft operators and maintenance organisations, must be notified of these changes to ensure compliance with the updated regulatory requirements.
Failure to comply with the provisions of these Airworthiness Directives can result in serious consequences. If an operator or maintenance organisation fails to adhere to the directives, it can lead to safety risks that could potentially compromise the airworthiness of the aircraft. The Civil Aviation Safety Regulations 1998 impose obligations on these entities to ensure compliance with all relevant directives. Non-compliance can lead to enforcement actions by CASA, which may include fines, sanctions, or even the grounding of affected aircraft until compliance is achieved. The specific penalties for non-compliance are detailed in the Civil Aviation Safety Regulations and can vary depending on the severity and circumstances of the breach.
The potential penalties for breach of these directives can be significant. Under the Civil Aviation Safety Regulations 1998, non-compliance can result in both civil and criminal penalties. Civil penalties may include substantial fines, with the exact amount determined by the seriousness of the breach. In more severe cases, criminal penalties may apply, leading to imprisonment for individuals responsible for the non-compliance. The maximum penalties are specified in the Civil Aviation Safety Regulations and can vary widely based on the nature and impact of the breach. These provisions underscore the importance of adhering to airworthiness directives to maintain the highest safety standards in aviation.