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 (Hedaro) CA25 Series Aeroplanes
AD Name AD Number
Life Limited Components AD/CA25/1 Amdt 2
Wing Strut Carry Through Structure AD/CA25/2 Amdt 1
Air Filter Box Rear Mounting Bracket AD/CA25/3
Tail Wheel Springs AD/CA25/4
Throttle Control Grub Screw AD/CA25/5
Gazelle Exhaust System AD/CA25/6
Aileron Hanger Ribs AD/CA25/7 Amdt 1
Carburettor Heat Modification Number 7/97 AD/CA25/8
Alternator Circuit Breaker Switch AD/CA25/9
Ailerons AD/CA25/10 Amdt 1
Engine Air Intake Hoses AD/CA25/11
Rudder Pedal Cable Attachment Lug AD/CA25/12
Overview
The Airworthiness Directives 2004, enacted by David Alan Villiers, a delegate of the Civil Aviation Safety Authority (CASA), under the authority of subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, serves to revoke existing airworthiness directives and remake them as separate instruments. This legislative instrument was introduced to ensure that airworthiness directives are clearly and accurately documented and readily accessible to the aviation industry, maintaining high safety standards in civil aviation. Each directive is remade in the same form as it appears in the latest published edition, reflecting the CASA’s commitment to transparency and consistency in aviation safety regulations. The policy objective is to uphold stringent safety protocols and enhance the regulatory framework governing airworthiness directives.
Scope and Application
The Airworthiness Directives 2004, made under the authority of the Civil Aviation Safety Authority (CASA), specifically targets the maintenance and operational standards of certain aircraft, particularly those in the Skyfox Aviation (Hedaro) CA25 Series Aeroplanes category. This legislative instrument applies to all aircraft within this series and mandates specific safety measures and compliance with the airworthiness directives listed in the Schedule. The directives themselves cover a range of components, including the wing strut carry-through structure, air filter box rear mounting bracket, tail wheel springs, and throttle control grub screw, among others. The application of these directives is national in scope, affecting all entities and individuals who own, operate, or maintain the specified aircraft within Australian jurisdiction. The directives are designed to ensure the continued airworthiness of the aircraft, thereby enhancing safety and compliance with civil aviation standards. This legislation does not specify any exclusions or exemptions but mandates strict adherence to the detailed requirements set out in the remade directives, which are attached and re-made in the same form as the latest published edition.
Key Provisions
The Airworthiness Directives 2004, issued under the authority of David Alan Villiers as the delegate of the Civil Aviation Safety Authority, primarily serve to revoke existing Airworthiness Directives and re-make them as separate instruments. This legislative instrument is structured to ensure that the latest editions of these directives are published and in effect, thereby maintaining the safety and compliance standards in the aviation sector. The directives listed in Schedule 1 are specifically targeted for revocation and re-making, ensuring that all relevant stakeholders are aware of the updated requirements and specifications. Each directive is re-made in exactly the same form as it appears in the most recent published edition, providing clarity and consistency for compliance purposes.
The Airworthiness Directives 2004 impose clear obligations on the parties and entities it governs. These directives set forth specific requirements and instructions that must be adhered to in order to maintain the airworthiness of certain aircraft components. For instance, the directives detail modifications, maintenance schedules, and inspection criteria for various parts of the aircraft, such as the wing strut carry-through structure, air filter box rear mounting bracket, and tail wheel springs. Compliance with these directives is mandatory for aircraft operators and maintenance personnel to ensure that the aircraft remain safe and operational according to the Civil Aviation Safety Regulations 1998.
Failure to comply with the Airworthiness Directives 2004 can result in significant legal consequences. The regulations outline specific offences, penalties, and civil or criminal ramifications for breaches. Non-compliance with these directives may be considered a breach of the Civil Aviation Safety Regulations 1998, potentially leading to enforcement actions by the Civil Aviation Safety Authority. The penalties for such breaches can include fines and, in severe cases, criminal charges against the responsible individuals or entities. The exact penalties are determined by the severity of the breach and the specific provisions of the Civil Aviation Safety Regulations 1998, but they are designed to enforce strict adherence to airworthiness standards.