Airworthiness Directives 2004 - Revocation and Remaking - SAAB 2000 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

 SAAB 2000 Series Aeroplanes

 AD Name AD Number

 Emergency Pitch Trim System AD/SB2000/1

 Ceiling and Lavatory Fluorescent Lamps AD/SB2000/2

 Dual Shuttle Valve AD/SB2000/3

 

Overview

The Airworthiness Directives 2004 is a legislative instrument enacted by David Alan Villiers, as the delegate of the Civil Aviation Safety Authority, on 20 December 2004. This instrument was introduced to address the need for the revocation and remaking of specific Airworthiness Directives that are integral to ensuring the safety and airworthiness of aircraft. The enactment follows subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, reflecting the legislative intent to streamline and update safety measures within the aviation industry. Each Airworthiness Directive listed in the schedule is re-made in the same form as it appears in the latest published edition, ensuring that all directives remain current and effective in maintaining safety standards. The policy objective is to uphold and improve the safety of air travel by ensuring that all relevant directives are accurately and consistently applied.

Scope and Application

The Airworthiness Directives 2004, issued by David Alan Villiers as a delegate of the Civil Aviation Safety Authority, under the authority of subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, applies to the specified airworthiness directives listed in Schedule 1. These directives pertain to the Saab 2000 series aeroplanes, specifically addressing issues such as the emergency pitch trim system, ceiling and lavatory fluorescent lamps, and the dual shuttle valve. The legislation operates under Commonwealth jurisdiction and is applicable to aircraft operators and owners within Australia. These directives are designed to ensure that the specified aircraft meet the necessary airworthiness standards and safety requirements. The revocation and remaking of these directives are executed to align with the latest published editions, ensuring consistency and up-to-date compliance with safety standards. Any exclusions or exemptions are not explicitly stated within this particular legislative instrument, and the directives are intended to maintain high safety standards across the aviation industry.

Key Provisions

The primary operative sections of this legislative instrument, the Airworthiness Directives 2004, involve the revocation and remaking of specific airworthiness directives related to SAAB 2000 Series Aeroplanes (sections 1 and 2). These directives cover the Emergency Pitch Trim System (AD/SB2000/1), Ceiling and Lavatory Fluorescent Lamps (AD/SB2000/2), and the Dual Shuttle Valve (AD/SB2000/3). The instrument revokes the existing directives and re-makes them as separate instruments, ensuring that each directive appears in the same form as it is presented in the latest published edition. The directives address safety and operational standards for specified components of the SAAB 2000 Series Aeroplanes. The obligations and requirements imposed by this Act primarily concern compliance with the newly re-made airworthiness directives. Operators and owners of SAAB 2000 Series Aeroplanes must adhere to the specific standards and procedures outlined in each directive. This includes ensuring that the Emergency Pitch Trim System, Ceiling and Lavatory Fluorescent Lamps, and the Dual Shuttle Valve meet the prescribed safety and operational requirements. Failure to comply with these directives can lead to potential safety risks and operational issues, thereby affecting the overall airworthiness of the aircraft. In terms of consequences for breach, the Airworthiness Directives 2004 do not explicitly state specific offences or penalties within the text provided. However, the Civil Aviation Safety Regulations 1998, under which this instrument is made, generally impose stringent measures for non-compliance with airworthiness directives. Penalties for breaches can include fines and, in severe cases, the grounding of aircraft until compliance is achieved. The exact penalties would be determined based on the specific breach and the severity of the non-compliance, but they can be substantial, reflecting the critical importance of adhering to airworthiness standards. To summarise, this legislative instrument revokes and re-makes specific airworthiness directives for SAAB 2000 Series Aeroplanes, imposing strict compliance requirements on operators and owners. While the specific penalties for non-compliance are not detailed in the text, they are likely to be severe, given the importance of airworthiness standards in ensuring flight 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.