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, enacted on 20 December 2004, is a legislative instrument issued by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, pursuant to subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. This instrument aims to revoke and re-make various Airworthiness Directives concerning Pratt and Whitney Turbine Engines of the JT8D-200 series. The policy objective is to ensure the continued airworthiness and safety of these engines by updating and re-issuing the directives in line with the latest published editions, thereby maintaining compliance with contemporary safety standards and regulatory requirements.
Each Airworthiness Directive mentioned in Schedule 1 is being re-made in exactly the same form as appears in the latest published edition of the Directive, which includes directives concerning life-limited components, number 4 and 5 bearing compartment oil fires, low pressure turbine anti-rotation pins, and number 4-1/2 bearing spacer. This legislative instrument is essential for addressing any discrepancies or updates in the regulatory framework governing the airworthiness of these engines, ensuring that they meet the stringent safety standards set forth by the Civil Aviation Safety Authority.
Scope and Application
The Airworthiness Directives 2004, promulgated by David Alan Villiers as the delegate of the Civil Aviation Safety Authority (CASA), pertains to the regulation of airworthiness for specific turbine engines, specifically the Pratt and Whitney JT8D-200 Series. This legislative instrument applies to entities and persons involved in the manufacture, maintenance, or operation of aircraft equipped with the specified engines, thereby impacting industries directly related to aviation and aeronautics. The scope of this Act encompasses a detailed remaking of several Airworthiness Directives listed in the Schedule, each addressing specific safety concerns such as oil fires in bearing compartments, low-pressure turbine anti-rotation pins, and bearing spacer issues. Geographically, this legislation operates under the Commonwealth jurisdiction, extending its regulatory authority across the entirety of Australia, ensuring consistent air safety standards are met nationwide. Notably, the Act includes provisions for the revocation of certain directives and their subsequent re-establishment, which is evident in the Schedule detailing the cancellation and remaking of specific directives. Additionally, the legislation may be extended or restricted through subordinate instruments, thereby allowing for flexibility and responsiveness to evolving safety concerns.
Key Provisions
The legislative instrument F2006B07977, issued by David Alan Villiers, a delegate of the Civil Aviation Safety Authority (CASA), contains two primary actions regarding airworthiness directives (ADs). Firstly, the instrument revokes the existing airworthiness directives listed in Schedule 1 (sections 2(a) and 3). These directives pertain specifically to Pratt and Whitney Turbine Engines of the JT8D-200 series, including directives related to oil fires in bearing compartments, low-pressure turbine anti-rotation pins, and a bearing spacer. Secondly, the instrument re-makes these directives as separate instruments, ensuring that they are published in the same form as the latest edition (sections 2(b) and 3).
The obligations imposed by this legislative instrument on the parties governed by these directives are significant. Aircraft operators and owners must comply with the re-made directives, ensuring that any required maintenance, inspections, or modifications are carried out as specified. This includes addressing issues such as potential oil fires in bearing compartments, ensuring the integrity of low-pressure turbine anti-rotation pins, and verifying the condition of the number 4-1/2 bearing spacer. Compliance is critical to maintaining the airworthiness of the aircraft and ensuring passenger safety.
Failure to comply with the requirements set out in these airworthiness directives can lead to serious consequences. Under the Civil Aviation Safety Regulations 1998, non-compliance with an airworthiness directive can result in civil penalties. For instance, an aircraft operator who fails to comply with a mandatory airworthiness directive can face fines of up to $275,000 for a corporation and $55,000 for an individual. Additionally, there can be criminal penalties for more severe breaches, including imprisonment for up to five years. These penalties underscore the importance of adhering to the directives to prevent potential hazards and ensure the continued safety of air travel.