Airworthiness Directives 2004 - Revocation and Remaking - Honeywell International Turbine Engines - T5508D Series

Overview

The Airworthiness Directives 2004 is a legislative instrument made by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, on 20 December 2004. This instrument revokes certain existing Airworthiness Directives related to the airworthiness of aircraft and re-makes them in exactly the same form as appears in the latest published edition of the Directive. This was done under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, aiming to ensure the continued safety and airworthiness of aircraft in Australia. The policy objective is to maintain and enhance the safety standards of civil aviation by ensuring that all aircraft and their components meet the necessary safety requirements. The Airworthiness Directives 2004 specifically addresses the airworthiness of Honeywell International Turbine Engines - T5508D Series, covering aspects such as the Inner Bevel Gear, Compressor Bleed Bands, and 1st Stage Turbine Disk. The revocation and remaking of these directives aim to update and ensure the applicability of safety measures and compliance standards, thereby reducing the risk of accidents and maintaining the integrity of the national aviation safety framework.

Scope and Application

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority (CASA), pertains to the revocation and remaking of specific airworthiness directives for certain aircraft components, specifically those relating to Honeywell International Turbine Engines of the T5508D series. This legislation applies to any person or entity involved in the operation, maintenance, or manufacture of aircraft fitted with these engines. The geographic reach of this legislation is primarily within the Commonwealth of Australia, as it is a regulation under the Civil Aviation Safety Regulations 1998. These directives set forth mandatory safety standards and procedures that must be adhered to by the relevant industry to ensure the airworthiness of the aircraft in question. Notably, this legislative instrument does not specify any exclusions or exemptions, implying that it applies universally within its scope to all relevant entities and components mentioned. The Act extends its application through the attachment of individual Airworthiness Directives which are re-made in the same form as the latest published editions, ensuring that the regulatory framework remains current and consistent with international safety standards.

Key Provisions

The main operative sections of this legislative instrument involve the revocation and remaking of certain Airworthiness Directives, specifically those related to the Honeywell International Turbine Engines - T5508D Series. Section 1 outlines the revocation of the existing directives, which are listed in Schedule 1, and section 2 details the remaking of these directives in their latest form. The revocation and remaking of these directives aim to ensure that all relevant safety regulations are up-to-date and accurately reflect current industry standards. This legislative instrument ensures that the Civil Aviation Safety Authority (CASA) has the most recent and effective safety measures in place for the specified turbine engines. The obligations and requirements imposed by this Act primarily involve the adherence to the newly remade Airworthiness Directives. These directives outline specific safety measures and compliance requirements for the operation and maintenance of the Honeywell International Turbine Engines - T5508D Series. Operators and maintenance providers must ensure that all procedures, inspections, and repairs are conducted in accordance with the latest directives to maintain airworthiness standards. Failure to comply with these directives can result in significant safety risks and may lead to aircraft being grounded until the necessary actions are taken. The Airworthiness Directives 2004 also include provisions for civil and criminal consequences for non-compliance with the directives. Section 3 of the instrument highlights that breaches of these directives may result in penalties and other legal actions. While the specific maximum penalties are not detailed within the instrument, it is understood that non-compliance can lead to significant financial penalties, enforcement actions, and potentially criminal charges. The severity of these consequences underscores the importance of adhering to the directives to ensure the safety and compliance of aviation operations involving the specified turbine engines.