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
De Havilland DH 60 (Moth) Series Aeroplanes
AD Name AD Number
Compression Leg Tie-Rod - Inspection AD/DH 60/1
Seat Restraint Installations - Modification AD/DH 60/2
Datum Bolts AD/DH 60/3 Amdt 1
Cockpit Lateral Tie Rods and Aircraft Structure AD/DH 60/4 Amdt 1
Flight Limitations and Structural Inspection AD/DH 60/5 Amdt 1
Cockpit Safety Harness Installation - Integrity and Lifing AD/DH 60/6
Introduction of Increased Strength Seat Harness Transverse Cable AD/DH 60/7 Amdt 1
Overview
The Airworthiness Directives 2004 is a legislative instrument introduced by David Alan Villiers, acting as the delegate of the Civil Aviation Safety Authority (CASA). Enacted on 20 December 2004, this instrument serves to revoke and re-make specific Airworthiness Directives for certain de Havilland DH 60 (Moth) Series Aeroplanes. This was necessary to ensure that the regulatory framework governing the airworthiness of these aircraft remains current and compliant with the latest safety standards. The policy objective behind this legislation is to maintain and enhance aviation safety by ensuring that all airworthiness directives are up-to-date and accurately reflect the latest safety requirements. Each directive is re-made in the same form as it appears in the most recent published edition, ensuring consistency and clarity in aviation safety standards.
Scope and Application
The Airworthiness Directives 2004, promulgated by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, serves to both revoke and remake various Airworthiness Directives, as detailed in Schedule 1. This legislative instrument operates under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, indicating its application within the Commonwealth jurisdiction of Australia. The directives concern specific De Havilland DH 60 (Moth) Series Aeroplanes, covering aspects such as inspection, modification, and structural integrity. Each directive is being remade in the same form as the latest published edition, ensuring consistency and adherence to updated safety standards. The scope of these directives includes all relevant aircraft, their operators, and manufacturers within Australia, as they pertain to the maintenance and safety of the specified aircraft models. Notably, the legislative instrument does not introduce any exclusions or exemptions; instead, it strictly applies to the listed directives, thereby impacting the compliance requirements of those involved in the operation and maintenance of the De Havilland DH 60 (Moth) Series Aeroplanes.
Key Provisions
The Airworthiness Directives 2004 primarily involves the revocation and remaking of specific airworthiness directives for certain De Havilland DH 60 (Moth) series aeroplanes, as detailed in Schedule 1 (sections 3 and 4). This legislative instrument revokes existing airworthiness directives (section 3) and then re-makes them as separate instruments (section 4). The airworthiness directives in question cover various aspects such as inspections, modifications, and limitations for the specified aeroplanes.
The obligations and requirements imposed by this legislation are aimed at ensuring the safety and airworthiness of the De Havilland DH 60 (Moth) series aeroplanes. The re-made directives provide specific instructions and guidelines that must be followed by the operators and maintainers of these aeroplanes. For example, AD/DH 60/1 requires an inspection of the compression leg tie-rod, while AD/DH 60/2 mandates modifications to seat restraint installations. Each directive is intended to address identified safety concerns and ensure compliance with civil aviation safety standards.
Failure to comply with the provisions of these airworthiness directives can result in significant legal consequences. Although the specific penalties are not detailed in the text, under the Civil Aviation Safety Regulations 1998, non-compliance with airworthiness directives can lead to substantial fines and, in severe cases, criminal charges. The exact penalties may vary depending on the nature and severity of the breach, but they are designed to enforce strict adherence to the safety standards set forth by the Civil Aviation Safety Authority.
The legislative instrument underscores the importance of maintaining the airworthiness of aircraft by providing updated and specific directives for operators and maintainers. By re-making these directives, the Civil Aviation Safety Authority ensures that the latest safety standards and requirements are clearly communicated and enforced. This continuous effort to update and enforce airworthiness directives is crucial for the safety of aviation operations in Australia.