Airworthiness Directives 2004 - Revocation and Remaking - Hiller UH-12 Series Helicopters

Overview

The Airworthiness Directives 2004 is a legislative instrument made by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. This instrument serves to revoke previously issued Airworthiness Directives pertaining to specific aircraft models and to re-issue them as separate instruments. The objective is to ensure that the directives are current and accurately reflect the latest safety standards and requirements. By remaking the directives, the Civil Aviation Safety Authority aims to maintain stringent oversight and compliance with aviation safety regulations, thus safeguarding public safety in the aviation sector. The Civil Aviation Safety Authority, through this instrument, addresses the need for updated and precise airworthiness directives for specified aircraft models, ensuring that all safety concerns and technical specifications are clearly defined and enforceable. The policy objective is to enhance aviation safety by providing clear, up-to-date directives that mandate specific actions and inspections to be carried out on aircraft, thereby preventing potential safety hazards and ensuring the continued airworthiness of the aircraft in question.

Scope and Application

The Airworthiness Directives 2004 applies to aircraft, specifically the Hiller UH-12 Series Helicopters, and regulates the airworthiness standards that must be met by these aircraft in Australia. As a legislative instrument under the Civil Aviation Safety Regulations 1998, it is enacted by the delegate of the Civil Aviation Safety Authority, David Alan Villiers. This instrument revokes existing airworthiness directives and re-makes them as separate instruments, ensuring that the directives are up to date and comply with the latest safety standards. The directives cover various aspects of the helicopters' maintenance and inspection, including the main rotor blades, transmission, and other critical components. The legislation has a national reach, applying across Australia, and does not specify any exclusions or exemptions. The application of this legislation can be extended or restricted through subordinate instruments, although no such extensions or restrictions are noted in this particular legislative instrument.

Key Provisions

The Airworthiness Directives 2004, made by the delegate of the Civil Aviation Safety Authority (CASA) under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, primarily focus on the revocation and remaking of specific Airworthiness Directives related to the Hiller UH-12 Series Helicopters. The directive revokes the listed Airworthiness Directives in Schedule 1 (sections 2(a) and (b)), and re-makes each directive as separate instruments, ensuring they appear in the latest published edition of the directive. These Airworthiness Directives impose various obligations and requirements on the operators and maintainers of the Hiller UH-12 Series Helicopters. They mandate detailed inspections, modifications, replacements, and operational limitations for specific components of the helicopters, such as the main rotor blades, tail rotor blade assembly, transmission systems, and other critical parts. For example, AD/HILLER 12/1 requires the inspection of the main rotor blade, while AD/HILLER 12/3 mandates the provision of a vent hole in the tail rotor blade assembly. Failure to comply with the provisions of these Airworthiness Directives can result in significant consequences. While the legislation does not explicitly state penalties, non-compliance with CASA directives generally can lead to enforcement actions. Such actions may include fines, enforcement notices, or even grounding of the aircraft until the required actions are completed. The severity of the penalties can depend on the nature and extent of the non-compliance, as well as any resultant safety risks. Operators are expected to adhere to these directives to ensure the continued airworthiness and safety of the aircraft under their management.