Airworthiness Directives 2004 - Revocation and Remaking - Morovan Zlin Z 526 Series Aeroplanes

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Legislation au F2006B07931 In force Legislative Instrument

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 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

 Morovan Zlin Z 526 Series Aeroplanes

 AD Name AD Number

 Elevator Control Countershaft Lever AD/Z 526/1

 Main Wing Spar Corrosion AD/Z 526/2

 

Overview

The Airworthiness Directives 2004 (F2006B07931) is a legislative instrument enacted to address the need for updated and revised safety regulations in the aviation industry, specifically targeting the airworthiness of certain aircraft. This instrument was issued under the authority of David Alan Villiers, as a delegate of the Civil Aviation Safety Authority, pursuant to subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The primary objective of this legislation is to ensure the continued safety and reliability of aircraft by revoking and remaking specific Airworthiness Directives to reflect the most current safety standards and requirements. This legislative instrument aims to maintain the integrity of civil aviation safety by ensuring that all airworthiness directives are consistent with the latest regulatory requirements and technological advancements.

Scope and Application

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority (CASA), pertain specifically to certain aircraft models and their airworthiness requirements. The legislation applies to the Morovan Zlin Z 526 series aeroplanes, with directives addressing particular issues such as elevator control countershaft lever and main wing spar corrosion, identified by their respective AD numbers AD/Z 526/1 and AD/Z 526/2. This Act impacts aircraft owners, operators, and maintenance personnel who are responsible for ensuring that these aeroplanes comply with the specified airworthiness standards. Its jurisdictional reach is nationwide, extending across all states and territories within Australia, as it operates under the auspices of the Commonwealth. The Act does not explicitly state exclusions or exemptions, but its application is limited to the specified aircraft series and issues. The authority to create, revoke, and remake these directives is exercised through subordinate instruments, ensuring that the directives remain aligned with current safety standards and practices.

Key Provisions

The Airworthiness Directives 2004 issued by David Alan Villiers, delegate of the Civil Aviation Safety Authority, primarily involve the revocation of existing Airworthiness Directives and their re-promulgation as separate instruments (sections 1(a) and 1(b)). Specifically, Schedule 1 lists the Airworthiness Directives that are revoked and subsequently re-made. The directives that are affected pertain to the Morovan Zlin Z 526 Series Aeroplanes, with specific AD numbers AD/Z 526/1 and AD/Z 526/2, addressing issues such as the elevator control countershaft lever and main wing spar corrosion. These Airworthiness Directives impose several obligations on the parties they govern. Primarily, they mandate compliance with specific safety standards and procedures to ensure the airworthiness of the Morovan Zlin Z 526 Series Aeroplanes. For instance, AD/Z 526/1 concerning the elevator control countershaft lever requires that specific maintenance actions be taken to address identified issues. Similarly, AD/Z 526/2 pertaining to main wing spar corrosion necessitates regular inspections and necessary repairs to prevent structural failure. The re-making of these directives ensures that the latest safety requirements are clearly communicated and must be adhered to by the relevant stakeholders. Failure to comply with these Airworthiness Directives can result in significant legal and operational consequences. Under the Civil Aviation Safety Regulations 1998, non-compliance with airworthiness directives can be considered a breach of safety regulations, leading to enforcement actions by the Civil Aviation Safety Authority. Civil penalties may include fines, and in severe cases, aircraft operators may face suspension or revocation of their airworthiness certificates. Additionally, non-compliance could result in criminal charges for individuals or corporations, with penalties that may include substantial fines and imprisonment, depending on the severity of the breach and its impact on aviation safety.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.