Airworthiness Directives 2004 - Revocation and Remaking - Skyfox Aviation (Calair/Hedaro) CA21 and CA22A Series Aeroplanes

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Legislation au F2006B08031 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

 Skyfox Aviation (Calair/Hedaro) CA21 and CA22A Series Aeroplanes

 AD Name AD Number

 Air Filter Box Rear Mounting Bracket AD/CA21/1

 Wing Lift Struts AD/CA21/2

 Rudder Actuator Horn AD/CA21/3

 Tail Wheel Springs AD/CA21/4

 Wing Strut Carry Through Structure AD/CA21/5

 Life Limited Components AD/CA21/6

 Aileron Hanger Ribs AD/CA21/7 Amdt 1

 Throttle Control Grub Screw AD/CA21/8

 Carburettor Heat Modification Number 7/97 AD/CA21/9

 Ailerons AD/CA21/10 Amdt 1

 Engine Air Intake Hoses AD/CA21/11

 Rudder Pedal Cable Attachment Lug AD/CA21/12

 

Overview

The Airworthiness Directives 2004, promulgated by David Alan Villiers as the delegate of the Civil Aviation Safety Authority (CASA) under the Civil Aviation Safety Regulations 1998, serve to address gaps in the safety and airworthiness standards for specific aircraft models. The primary objective of these directives is to ensure the ongoing safety of civil aviation by revising or revoking previous airworthiness directives and issuing updated versions. This legislative instrument was enacted to provide a structured approach to managing airworthiness directives, ensuring that all relevant safety concerns are addressed comprehensively and uniformly across the affected aircraft fleet. The directives aim to maintain a high standard of safety in civil aviation by enforcing compliance with specific airworthiness requirements for aircraft such as the Skyfox Aviation (Calair/Hedaro) CA21 and CA22A series aeroplanes. This is achieved through detailed amendments to existing directives, covering a range of components including the air filter box, wing lift struts, rudder actuator horn, and other critical parts. The re-making of these directives ensures that the latest safety standards and findings are incorporated, providing a clear and enforceable framework for maintaining the airworthiness of these aircraft.

Scope and Application

The Airworthiness Directives 2004, issued by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, pertains to the aviation industry specifically concerning the maintenance and safety of certain aircraft models. These directives apply to aircraft owners, operators, and maintenance personnel who must adhere to the specified airworthiness standards to ensure the safety and compliance of Skyfox Aviation (Calair/Hedaro) CA21 and CA22A series aeroplanes. The scope of this legislation extends nationally across Australia, as it is issued under Commonwealth authority. The directives include detailed instructions on modifications and maintenance procedures for various components of the aircraft, such as the air filter box, wing lift struts, rudder actuator horn, tail wheel springs, and other structural elements. Each directive is re-made in the same form as the latest published editions, ensuring consistency and up-to-date safety standards. Notably, the application of these directives is comprehensive, covering all relevant aircraft within the specified series, with no explicit exclusions mentioned within the text. Subordinate instruments may extend or refine the application of these directives, providing further clarification or updates as necessary.

Key Provisions

The legislative instrument F2006B08031, titled "Airworthiness Directives 2004," primarily addresses the revocation and remaking of various Airworthiness Directives related to specific aircraft models. These directives are crucial for ensuring the safety and airworthiness of the aircraft, as they outline necessary maintenance, repair, or modification actions that must be undertaken (section 1). The primary sections involved in this legislative instrument are sections (a) and (b), which respectively revoke and re-make the specified Airworthiness Directives as listed in Schedule 1. The Airworthiness Directives in question pertain to Skyfox Aviation's (Calair/Hedaro) CA21 and CA22A series aeroplanes, with specific directives numbered from AD/CA21/1 to AD/CA21/12. The obligations and requirements imposed by this Act on the parties or entities it governs include adherence to the newly re-made Airworthiness Directives. Aircraft operators, maintenance organisations, and other relevant stakeholders must comply with the specific maintenance, repair, or modification actions outlined in these directives to ensure the continued airworthiness of the affected aircraft. This includes actions such as ensuring the correct mounting of the air filter box rear bracket, inspecting and maintaining wing lift struts, and addressing issues with the rudder actuator horn, among other specified components. Compliance with these directives is essential to maintain the safety standards required by the Civil Aviation Safety Authority. The Airworthiness Directives 2004 legislative instrument also delineates the consequences for non-compliance with the specified requirements. While the text does not explicitly state the penalties for breach, it is understood that failure to comply with Airworthiness Directives can lead to severe consequences. These may include administrative actions such as fines or other monetary penalties, as well as potential criminal charges in cases where non-compliance results in accidents or other significant safety incidents. The maximum penalties for such breaches are not explicitly mentioned in this text but are generally governed by the broader aviation safety regulations and can vary based on the severity and impact of the non-compliance. Operators and other stakeholders must therefore ensure strict adherence to the directives to avoid any legal repercussions.

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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.