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-20 (Pacer) Series Aeroplanes
AD Name AD Number
Battery Terminal Insulation AD/PA-20/1
CANCELLED AD/PA-20/2
Wing Lift Strut Forks AD/PA-20/3 Amdt 6
CANCELLED AD/PA-20/4
Cigar Lighter Circuit - Provision of Fuse AD/PA-20/5
Sensenich M76AM-2 Propellers - Replacement Model M75DM - CANCELLED AD/PA-20/6
Fuselage Fabric in Area of Wind Shield Top Attachment Channel - Modification AD/PA-20/7 Amdt 1
Tail Brace Streamline Tie Rods - Inspection AD/PA-20/8
Exhaust System - Inspection AD/PA-20/9
Front Seat Restraint Installations - Modifications AD/PA-20/10
Flexible Fuel Hose Assembly - Inspection AD/PA-20/11
Fuselage Structure, Upper Cabin - Inspection AD/PA-20/12
Wing Fuel Tank Cap - Modification AD/PA-20/13
Fire Hazard Prevention - Inspection and Rework AD/PA-20/14
Fuel Primer and Hydraulic Lines - Re-Routing AD/PA-20/15 Amdt 1
Fuselage Door Frame Tube Corrosion AD/PA-20/16 Amdt 1
Wing Lift Struts AD/PA-20/17 Amdt 7
Overview
The Airworthiness Directives 2004 were enacted to address issues surrounding the airworthiness of specific aircraft models, specifically the Piper PA-20 (Pacer) series aeroplanes, by delegating authority to David Alan Villiers, a delegate of the Civil Aviation Safety Authority, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. This legislative instrument revokes certain existing airworthiness directives and re-issues them to ensure that all safety measures and compliance requirements are up-to-date and effectively communicated. The policy objective is to maintain the highest standards of aviation safety by ensuring that all aircraft operate within the mandated safety parameters, thereby protecting the public and enhancing the overall safety of air travel.
Scope and Application
The Airworthiness Directives 2004, issued under the Civil Aviation Safety Regulations 1998, pertain to the safety and airworthiness of specific aircraft, specifically Piper PA-20 (Pacer) series aeroplanes. This legislation applies to the owners, operators, and maintainers of these aircraft, mandating compliance with the stipulated safety directives to ensure their continued airworthiness. The scope of these directives includes various technical aspects of the aircraft, such as battery terminal insulation, wing lift strut forks, cigar lighter circuit fuses, propeller replacements, and modifications to fuselage fabric and structures. Geographically, the directives extend to all Piper PA-20 series aeroplanes operating within Australia, ensuring a national standard of airworthiness. The Civil Aviation Safety Authority has the authority to revoke and remake these directives as necessary, with each re-made directive adhering to the latest published standards. While the Act itself does not explicitly mention exclusions or exemptions, its application is contingent on the specific aircraft and operational contexts as detailed in the directives.
Key Provisions
The main operative sections of this legislative instrument pertain to the revocation and remaking of various Airworthiness Directives (ADs) for the Piper PA-20 (Pacer) series aeroplanes. Specifically, sections (a) and (b) revoke existing ADs listed in Schedule 1 and then re-make them as separate instruments. This ensures that the ADs are updated to reflect the latest published editions while maintaining their regulatory effect. The directive aims to ensure that all safety measures and operational standards are up to date and clearly defined, facilitating compliance among aircraft operators and maintenance personnel.
The obligations and requirements imposed by this Act are primarily centred around the adherence to the re-made Airworthiness Directives. Aircraft operators and maintenance organisations must ensure that all specified inspections, modifications, and reworks are completed as per the ADs. For example, AD/PA-20/14 requires the re-routing of fuel primer and hydraulic lines, while AD/PA-20/16 Amdt 1 mandates an inspection of wing lift struts. These directives are designed to maintain the airworthiness of the aircraft by addressing potential safety hazards and ensuring that all structural and functional components meet specified safety standards.
Failure to comply with the provisions of these Airworthiness Directives may result in various civil and criminal consequences. Under section 90 of the Civil Aviation Act 1988, non-compliance can lead to civil penalty proceedings, with maximum penalties for corporations being AUD 1,100,000 and AUD 550,000 for individuals. Additionally, the Civil Aviation Safety Authority has the authority to impose administrative penalties, including fines, for breaches of ADs. In more severe cases, non-compliance may also lead to criminal charges, resulting in fines of up to AUD 220,000 and/or imprisonment for up to 5 years for corporations, and AUD 55,000 and/or 12 months imprisonment for individuals. These stringent measures underscore the importance of adhering to airworthiness directives to ensure the safety and integrity of aviation operations.