Airworthiness Directives 2004 - Revocation and Remaking - Cessna 525 Series Aeroplanes

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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

 Cessna 525 Series Aeroplanes

 AD Name AD Number

 Main Landing Gear Trunnion Bearings AD/CESSNA 525/1

 Direct Current Power Battery Switch AD/CESSNA 525/2

 Electric Pitch Trim System AD/CESSNA 525/3 Amdt 1

 Electric Pitch Trim Printed Circuit Board AD/CESSNA 525/4

 

Overview

The Airworthiness Directives 2004, enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, aims to ensure that specific airworthiness directives are up-to-date and accurately reflect the latest safety standards for civil aviation. This legislative instrument revokes and remakes certain airworthiness directives related to the Cessna 525 series aeroplanes, including directives concerning main landing gear trunnion bearings, direct current power battery switches, electric pitch trim systems, and the electric pitch trim printed circuit board. The primary objective is to maintain a consistent and reliable regulatory framework that aligns with the latest safety protocols and standards, thereby enhancing the overall safety of civil aviation operations.

Scope and Application

The Airworthiness Directives 2004, as promulgated by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, apply to specific airworthiness directives related to the Cessna 525 Series Aeroplanes. These directives are applicable to the particular aircraft types and components specified in the Schedule 1, which includes the Main Landing Gear Trunnion Bearings, Direct Current Power Battery Switch, Electric Pitch Trim System, and Electric Pitch Trim Printed Circuit Board. The directives are intended to ensure that these components meet the requisite safety standards. This legislative instrument operates on a national level and applies across Australia, encompassing all relevant entities and industries within the scope of civil aviation. The directives are designed to enhance the airworthiness of the specified aircraft models by mandating compliance with updated safety standards and procedures. The instrument revokes the previously existing directives and re-makes them to reflect the latest published editions, ensuring that all stakeholders are operating under the most current regulatory requirements.

Key Provisions

The Airworthiness Directives 2004, as promulgated by David Alan Villiers, delegate of the Civil Aviation Safety Authority, encompasses two primary actions detailed in the legislation. Firstly, it revokes the existing Airworthiness Directives listed in Schedule 1 (Section 1(a)). Secondly, it re-issues each of these revoked directives as separate instruments, maintaining their content identical to the latest published editions (Section 1(b)). These directives are specifically aimed at ensuring the safety and compliance of certain aircraft components, particularly those of Cessna 525 Series aeroplanes. The directives include modifications or inspections related to main landing gear trunnion bearings, direct current power battery switches, electric pitch trim systems, and electric pitch trim printed circuit boards. The obligations imposed by these directives are primarily directed towards aircraft owners, operators, and maintenance providers. They must ensure that the specified components are inspected, maintained, or modified according to the directives' requirements. This includes adhering to timelines for inspections, making necessary repairs or replacements, and keeping detailed records of compliance (Section 2). Failure to comply with these directives can result in serious safety risks, potentially leading to aircraft being grounded until the necessary actions are taken. The directives mandate a proactive approach to aircraft maintenance, ensuring that all identified issues are addressed promptly and effectively. Breaching the requirements set out in these Airworthiness Directives can lead to significant consequences. Under the Civil Aviation Safety Regulations 1998, non-compliance can be considered an offence. The potential penalties include fines and, in severe cases, criminal charges. The maximum penalties for such offences are not explicitly stated in the text but can be severe, reflecting the critical importance of air safety. The Civil Aviation Safety Authority has the authority to enforce these directives and take appropriate action against those who fail to comply, ensuring that the highest safety standards are maintained in the aviation industry.

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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.