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
Morava L200 Series Aeroplanes
AD Name AD Number
Fire Resistant Hose Assemblies - Installation AD/L200/1
Horizontal Stabiliser Attach Fittings - Modification AD/L200/2
Propeller De-Icing Control - Modification AD/L200/3
Nose Wheel Retract Strut - Inspection AD/L200/4
Front (Pilot) Seats Restraint Installation - Modification AD/L200/5
Wing and Tailplane Structural Fatigue Life AD/L200/6
Main Undercarriage Breakstrut Hinges - Inspection AD/L200/7
Fin and Stabiliser Front Attachment Hinges - Inspection AD/L200/8
Control Wheel Rod - Inspection AD/L200/9
Overview
The Airworthiness Directives 2004, enacted by David Alan Villiers as a delegate of the Civil Aviation Safety Authority under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, serve to revoke and re-make several Airworthiness Directives related to Morava L200 Series Aeroplanes. This legislative instrument addresses the need for updated and consistent regulatory standards for airworthiness, ensuring that all relevant directives are aligned with the latest safety requirements and published editions. The enactment aims to maintain and enhance aviation safety by providing clear, authoritative guidelines for the inspection, modification, and maintenance of specified aircraft components. The revocation and re-making process ensures that the directives remain effective and relevant, addressing any identified safety issues or gaps in the regulatory framework.
Scope and Application
The Airworthiness Directives 2004, enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority under the Civil Aviation Safety Regulations 1998, pertain specifically to the Morava L200 Series Aeroplanes. These directives are applicable to any person or entity involved in the operation, maintenance, or manufacture of the specified aircraft models, ensuring adherence to the outlined safety standards and modifications. The scope of the directives encompasses various aspects of aircraft maintenance and operational safety, including fire-resistant hose assemblies, structural modifications, and regular inspections. The legislation is geographically bound to the Commonwealth level and impacts all relevant entities within Australia. Subordinate instruments may extend or further specify the application of these directives, although the primary text focuses on the revocation and re-making of existing directives to align with current safety standards.
Key Provisions
The primary operative sections of this legislative instrument involve the revocation and remaking of several Airworthiness Directives (AD) for Morava L200 Series Aeroplanes. Section 1 revokes the Airworthiness Directives listed in Schedule 1, while Section 2 makes new, separate instruments for each of those ADs. The specific ADs mentioned in Schedule 1 are related to various aspects of the aircraft's maintenance and safety, including the installation of fire-resistant hose assemblies, modifications to horizontal stabiliser attach fittings and propeller de-icing controls, inspections of various structural components, and modifications to the front seat restraint installation. Each of these ADs is being remade in the same form as the latest published edition, ensuring that they remain current and effective.
The obligations imposed by this Act on the parties or entities it governs primarily revolve around compliance with the newly remade Airworthiness Directives. Aircraft owners, operators, and maintenance personnel are required to adhere to the specific instructions and requirements outlined in each AD. This includes conducting inspections, making modifications, and installing necessary components as stipulated in the ADs. Compliance with these directives is critical for maintaining the airworthiness of the Morava L200 Series Aeroplanes, ensuring that they meet safety standards set by the Civil Aviation Safety Authority (CASA).
Failure to comply with the provisions of the Airworthiness Directives can result in various consequences. While the specific offences, penalties, or civil and criminal consequences for breach are not detailed in the legislative instrument itself, it is known that non-compliance with ADs can lead to enforcement actions by CASA. These actions may include fines, legal proceedings, and potentially grounding the aircraft if it is deemed unsafe. The maximum penalties for such breaches can vary widely depending on the severity of the non-compliance and the specific regulatory provisions under the Civil Aviation Safety Regulations 1998. It is important for all parties governed by this Act to ensure strict adherence to the ADs to avoid any adverse outcomes.