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
Turbomeca Turbine Engines - Makila Series
AD Name AD Number
Service Life Limits - CANCELLED AD/MAKILA/1
Governor Master and Auxiliary Cams AD/MAKILA/2
Electronic Control Unit AD/MAKILA/3
Electronic Control Unit AD/MAKILA/4
Exhaust Pipe Cracks AD/MAKILA/5
Exhaust Pipe Replacement AD/MAKILA/6
Overview
The Airworthiness Directives 2004 is a legislative instrument issued by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, acting under the authority granted by subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The purpose of this instrument was to revoke and simultaneously re-make several specific Airworthiness Directives concerning the Turbomeca Turbine Engines of the Makila series, which were identified as having specific service life limitations and other operational concerns. This legislative action was taken to ensure that the directives remained current and effective in maintaining the safety and airworthiness of these aircraft engines. Each directive that was re-made is presented in the exact form as it appeared in the latest published edition, ensuring that any revisions or updates made since the initial enactment were incorporated into the legal framework governing civil aviation safety in Australia.
The enacting body in this case is the Civil Aviation Safety Authority, operating under the overarching authority of the Civil Aviation Safety Regulations 1998. The policy objective of these directives is to maintain the highest standards of airworthiness for aircraft engines, thereby ensuring the safety of passengers and crew. By revoking and re-making the directives, the Civil Aviation Safety Authority aims to address any emerging issues or changes in operational practices that could affect the safety and reliability of the aircraft engines in question.
Scope and Application
The Airworthiness Directives 2004, made under the authority of David Alan Villiers, a delegate of the Civil Aviation Safety Authority, pertains specifically to the safety and operational standards of aircraft and their components. This legislative instrument revokes existing airworthiness directives pertaining to the Turbomeca Turbine Engines - Makila Series and remakes them in their latest form, as detailed in the attached schedules. The directives apply to entities involved in the operation and maintenance of these specific aircraft engines, ensuring adherence to updated safety standards. The geographic reach of these directives is inherently national, as they are issued under the Civil Aviation Safety Regulations 1998, which apply across Australia. The regulations do not specify exclusions or exemptions but implicitly apply to all entities and persons involved in the civil aviation industry within Australia. The legislative instrument extends its application through subordinate instruments by remaking the airworthiness directives in their latest form, ensuring compliance with the most current safety standards.
Key Provisions
The main operative sections of the Airworthiness Directives 2004 involve the revocation of existing airworthiness directives related to Turbomeca Turbine Engines of the Makila series, and the remaking of these directives as separate instruments. This process is detailed in section (a) which revokes the directives listed in Schedule 1 and section (b) which re-makes these directives as individual instruments. The directives that are revoked and remade include AD/MAKILA/1, AD/MAKILA/2, AD/MAKILA/3, AD/MAKILA/4, AD/MAKILA/5, and AD/MAKILA/6, each corresponding to specific aspects of the engines such as service life limits, governor master and auxiliary cams, electronic control units, and exhaust pipe issues.
The Act imposes several obligations and requirements on the parties or entities it governs. Firstly, it mandates the Civil Aviation Safety Authority (CASA) to ensure that airworthiness directives are kept up-to-date and accurately reflect the latest safety standards and operational requirements for the specified aircraft engines. The remaking of the directives ensures that they are legally enforceable and clearly defined, facilitating compliance for aircraft operators and maintenance personnel. Additionally, the directives provide specific instructions and guidelines for addressing issues such as service life limits, component replacements, and repair procedures, thereby ensuring that these engines are maintained to a high standard of airworthiness.
The legislation also outlines potential offences, penalties, or civil and criminal consequences for breaches. Although the specific penalties are not detailed within the text provided, under the Civil Aviation Safety Regulations 1998, failure to comply with airworthiness directives can result in substantial penalties. These can include fines, suspension or revocation of aircraft operating certificates, and potential criminal charges if the non-compliance leads to an accident or incident. The exact penalties can vary depending on the severity and circumstances of the breach but are intended to enforce stringent compliance with airworthiness standards to maintain the highest levels of aviation safety.