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
Pratt and Whitney Turbine Engines - JT8D-200 Series
AD Name AD Number
Life Limited Components - CANCELLED AD/JT8D-200/1
Number 4 and 5 Bearing Compartment Oil Fires AD/JT8D-200/2
Low Pressure Turbine Anti-Rotation Pins AD/JT8D-200/3
Number 4-1/2 Bearing Spacer AD/JT8D-200/4
Overview
The Airworthiness Directives 2004, promulgated by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, pursuant to subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, serve to address gaps and issues related to specific airworthiness directives previously in effect. The directives aim to ensure that aircraft maintain the highest standards of airworthiness, addressing specific concerns such as the life limitation of components and fire hazards associated with certain turbine engines. This legislative instrument revokes the previous directives and re-makes them in their latest form, as published, thereby ensuring that safety regulations remain current and effective. The policy objective is to safeguard the integrity and safety of aircraft in operation by maintaining and updating airworthiness standards as necessary.
The directives were enacted by the Civil Aviation Safety Authority to rectify identified problems within the airworthiness requirements for specific aircraft components, particularly those relating to Pratt and Whitney Turbine Engines of the JT8D-200 series. This measure ensures that the safety and reliability of these engines are consistently upheld by addressing issues such as oil fires in bearing compartments and the integrity of turbine anti-rotation pins. By revoking and re-making these directives, the Civil Aviation Safety Authority aims to provide a clear and updated framework for maintaining airworthiness, thereby enhancing the safety of air travel.
Scope and Application
The Legislative Instrument F2006B07978, issued by David Alan Villiers as a delegate of the Civil Aviation Safety Authority (CASA), revokes and re-makes several Airworthiness Directives under the Civil Aviation Safety Regulations 1998. The directives concern Pratt and Whitney Turbine Engines, specifically the JT8D-200 Series, and include measures to address issues such as life-limited components, oil fires in bearing compartments, low-pressure turbine anti-rotation pins, and the number 4-1/2 bearing spacer. This legislation applies to entities involved in the aviation industry, specifically those who manufacture, maintain, or operate aircraft equipped with the specified turbine engines. The geographic reach of this legislation is national, as CASA operates under the Commonwealth of Australia, thereby impacting all regions within Australia. Notably, the directives are re-made to align with the latest published edition, ensuring up-to-date safety standards. The instrument does not explicitly mention exclusions, exemptions, or thresholds but implies that compliance is mandatory for relevant entities. The application of these directives may also extend through subordinate instruments, as permitted under the Civil Aviation Safety Regulations 1998.
Key Provisions
The legislative instrument Airworthiness Directives 2004, issued by the delegate of the Civil Aviation Safety Authority, primarily involves the revocation and remaking of certain Airworthiness Directives (ADs) concerning Pratt and Whitney Turbine Engines, specifically the JT8D-200 series (sections 1 and 2). The ADs listed in Schedule 1 are revoked and subsequently remade as separate instruments, maintaining their form as per the latest published edition. This process ensures that the ADs are updated and comply with current safety standards.
The obligations imposed by this legislative instrument primarily concern aircraft operators and maintenance personnel. These parties must adhere to the newly remade ADs, ensuring that any specified actions or inspections are carried out on the relevant aircraft engines. Compliance with these ADs is crucial for maintaining the airworthiness of aircraft and ensuring passenger safety. Non-compliance could result in significant safety risks and potential regulatory action.
The legislative instrument does not explicitly outline specific offences or penalties for non-compliance with the ADs. However, non-compliance with ADs generally can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions may include the issuance of directives, fines, or the suspension or revocation of an aircraft operator's certificate. The maximum penalties for these actions can vary, but they can include substantial fines and the potential grounding of non-compliant aircraft, thereby impacting the operations and reputation of the affected entities.
In summary, the Airworthiness Directives 2004 require the revocation and remaking of specific ADs for Pratt and Whitney Turbine Engines, placing obligations on aircraft operators and maintenance personnel to comply with these directives to ensure airworthiness. While the legislative instrument itself does not detail specific penalties, non-compliance can lead to regulatory enforcement actions, including fines and operational disruptions.