Airworthiness Directives 2004 - Revocation and Remaking - Eagle X-TS Series Aeroplanes

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Legislation au F2006B07847 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

 Eagle X-TS Series Aeroplanes

 AD Name AD Number

 Exhaust System Inspection - Heat Exchanger AD/X-TS/1

 Rudder Cable Pulleys AD/X-TS/2

 Canard Rear Spar Reinforcement AD/X-TS/3

 Engine Controls AD/X-TS/4

 Flap Hinge Support Bracket AD/X-TS/5 Amdt 1

 Main Undercarriage Attach Bracket AD/X-TS/6

 Co-Pilot Rudder Pedal Assembly AD/X-TS/7

 

Overview

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority (CASA) by David Alan Villiers, a delegate, primarily focus on the revocation and remaking of specific airworthiness directives. Enacted on 20 December 2004, this legislative instrument addresses the need to update and reaffirm certain safety regulations concerning the airworthiness of specific aircraft models, namely the Eagle X-TS Series Aeroplanes. The instrument aims to ensure that the latest safety standards and directives are consistently applied, thereby enhancing aviation safety. Each directive in the schedule is re-made in its latest published form to reflect any amendments or updates necessary for compliance with current safety requirements. This legislative action underscores the commitment of CASA to maintaining high safety standards within the aviation industry.

Scope and Application

The Airworthiness Directives 2004, issued by David Alan Villiers as the delegate of the Civil Aviation Safety Authority under the Civil Aviation Safety Regulations 1998, pertains specifically to certain series of aeroplanes and their components. This legislative instrument revokes the previously mentioned Airworthiness Directives and re-makes each of them as separate instruments, ensuring they are in alignment with the latest published editions. The directives apply to specific components of Eagle X-TS series aeroplanes, such as the exhaust system, rudder cables, canard rear spar, engine controls, flap hinge support brackets, main undercarriage attach brackets, and co-pilot rudder pedal assemblies. The geographic reach of this legislation is national, covering all civil aviation operations within Australia, thereby ensuring that all aeroplanes operating under Australian jurisdiction comply with these airworthiness standards. The Act does not specify any exclusions or exemptions, implying that the directives apply to all relevant aircraft and operators without exception. Additionally, the application of these directives may be extended or restricted through subordinate instruments, ensuring that the regulations can be adapted to new findings or technological advancements in aviation safety.

Key Provisions

The primary operative sections of the Airworthiness Directives 2004 (F2006B07847) involve the revocation of existing Airworthiness Directives and their re-making in identical form (sections 1(a) and 1(b)). The directive specifically targets several airworthiness directives related to Eagle X-TS Series Aeroplanes, listed in Schedule 1, including AD/X-TS/1 for Exhaust System Inspection - Heat Exchanger, AD/X-TS/2 for Rudder Cable Pulleys, and others up to AD/X-TS/7 for Co-Pilot Rudder Pedal Assembly. These sections aim to ensure that the latest safety and compliance standards are uniformly applied across all relevant aircraft. The Act imposes clear obligations and requirements on the parties and entities it governs. Owners, operators, and maintenance providers of the Eagle X-TS Series Aeroplanes must adhere to the specified airworthiness directives. This includes conducting necessary inspections, repairs, and modifications as outlined in each directive. The directives mandate that all maintenance and modifications be performed by authorised personnel and in accordance with the instructions provided, ensuring that the safety and airworthiness of the aircraft are maintained. Failure to comply with the requirements set out in the Airworthiness Directives can lead to various consequences, including offences and penalties. While the legislation does not explicitly state the penalties for non-compliance, breaches of airworthiness directives are typically serious and can result in substantial fines and legal action. In some cases, non-compliance may lead to the grounding of aircraft until the required actions are taken, potentially causing significant operational disruptions and financial losses for operators. Furthermore, persistent non-compliance could result in more severe penalties, including revocation of operating certificates or licenses, thereby affecting the ability of the parties involved to continue their operations. The re-making of the airworthiness directives ensures that there is no ambiguity or discrepancy in the regulations, as each directive is presented in the same form as the latest published edition. This meticulous approach underscores the importance of maintaining high safety standards and ensuring that all stakeholders are fully informed of their obligations. The consistent application of these directives helps to mitigate risks and promote the safe operation of Eagle X-TS Series Aeroplanes within Australian airspace.

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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.