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
Piper PA-11 (Cub) & J3 Series Aeroplanes
AD Name AD Number
Elevator Control Connector Tube - Modification AD/PA-11/1
Wing Lift Strut Forks AD/PA-11/2 Amdt 5
Front Seat Restraint Installations - Modification AD/PA-11/3
Wing Fuel Tank Cap - Modification AD/PA-11/4
Wing Lift Struts AD/PA-11/5 Amdt 8
Overview
The Airworthiness Directives 2004, issued by David Alan Villiers, the delegate of the Civil Aviation Safety Authority (CASA) on 20 December 2004, aim to update and maintain the safety standards of certain aircraft by revoking and remaking specific airworthiness directives. This legislative instrument operates under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The directives target Piper PA-11 (Cub) and J3 series aeroplanes, focusing on modifications to elevator control connectors, wing lift struts, front seat restraints, and wing fuel tank caps, to ensure compliance with safety regulations and enhance airworthiness. Each directive is remade in the same form as the latest published edition, ensuring consistency and adherence to current safety standards.
The enactment of these directives by CASA, an authority established under the Civil Aviation Act 1988, reflects a commitment to addressing safety gaps and maintaining high aviation safety standards in Australia. The policy objective is to mitigate potential risks associated with the specified aircraft modifications, thereby safeguarding the integrity and safety of civil aviation within the country. The re-making of these directives ensures that they are current and reflect any recent safety improvements or regulatory changes.
Scope and Application
The Airworthiness Directives 2004, made under the authority of the Civil Aviation Safety Regulations 1998, apply to specific aircraft models, namely the Piper PA-11 and J3 series aeroplanes. This legislation pertains to certain modifications and requirements that must be met to ensure the airworthiness of these aircraft, specifically focusing on components such as the elevator control connector tube, wing lift strut forks, front seat restraint installations, and wing fuel tank caps. The directives are applicable nationwide, reflecting the Commonwealth’s jurisdiction over civil aviation safety. Each directive is meticulously remade to align with the latest published editions, ensuring that the regulations remain current and effective. Notably, this legislation does not specify any exclusions or exemptions, implying that all relevant aircraft must comply with the outlined modifications and requirements. The scope of application is extended through the subordinate instruments attached to the legislative instrument, which detail specific modifications and adherence to airworthiness standards.
Key Provisions
The legislative instrument, F2006B07949, titled "Airworthiness Directives 2004," involves the revocation and remaking of specific Airworthiness Directives (ADs) pertaining to Piper PA-11 (Cub) & J3 Series Aeroplanes. The operative sections of this instrument include the revocation of existing ADs as listed in Schedule 1 (section 1(a)) and the re-making of these ADs as separate instruments (section 1(b)). The ADs being addressed are AD/PA-11/1 concerning the Elevator Control Connector Tube, AD/PA-11/2 Amendment 5 regarding Wing Lift Strut Forks, AD/PA-11/3 focusing on Front Seat Restraint Installations, AD/PA-11/4 addressing the Wing Fuel Tank Cap, and AD/PA-11/5 Amendment 8 concerning Wing Lift Struts.
This legislation imposes several obligations and requirements on the parties governed by the ADs. Primarily, these directives mandate specific modifications and maintenance procedures for the listed aircraft components to ensure airworthiness and safety standards are maintained. For example, AD/PA-11/1 requires the modification of the Elevator Control Connector Tube, while AD/PA-11/2 Amendment 5 mandates alterations to the Wing Lift Strut Forks. The affected parties, including aircraft owners, operators, and maintenance personnel, must adhere to these specifications to comply with the safety regulations stipulated by the Civil Aviation Safety Authority (CASA).
Failure to comply with the Airworthiness Directives can result in various civil and criminal consequences. While the legislative instrument does not explicitly outline penalties within its text, violations of airworthiness standards generally attract severe penalties under the Civil Aviation Safety Regulations 1998. These can include fines, imprisonment, or both, depending on the severity of the non-compliance and the resultant risk to safety. The maximum penalties are determined by the relevant provisions of the Civil Aviation Act 1988 and associated regulations, which can vary based on the nature and impact of the breach.
In summary, the Airworthiness Directives 2004 legislative instrument revokes and re-makes specific ADs for Piper PA-11 (Cub) & J3 Series Aeroplanes to ensure that all modifications and maintenance requirements are met to maintain airworthiness. Compliance with these directives is mandatory for aircraft owners, operators, and maintenance personnel, with potential civil and criminal consequences for non-compliance, including fines and imprisonment.