COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fokker F28 Series Aeroplanes
AD/F28/17 Main Landing Gear Wheel - Inspection NK
Applicability: All models.
Requirement: Inspect Goodyear Main Landing Gear wheels in the area of the internal flange radius using either an approved eddy current or ultrasonic technique.
Compliance: At each tyre removal after 3 August 1971.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, govern a wide range of aviation safety issues, including the airworthiness of aircraft. This comprehensive piece of legislation was introduced to ensure the safety and efficiency of civil aviation within Australia. One specific area addressed by this Act is the issuance of Airworthiness Directives, which are legally enforceable rules that the Civil Aviation Safety Authority (CASA) can issue to address identified safety issues. The policy objective of these regulations is to maintain a high standard of safety in the operation of civil aircraft, thereby protecting the public and maintaining public confidence in the aviation industry.
One example of such a directive is AD/F28/17, which pertains to the inspection of Goodyear Main Landing Gear wheels in Fokker F28 Series Aeroplanes. This directive applies to all models and mandates the inspection of the internal flange radius of these wheels using either an approved eddy current or ultrasonic technique. Compliance with this directive is required at each tyre removal following 3 August 1971, underscoring the regulatory commitment to continuous safety improvements and the proactive identification and mitigation of potential safety risks in aircraft operations.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, apply to all Fokker F28 Series Aeroplanes and mandate the inspection of the Goodyear Main Landing Gear wheels. This requirement applies universally to all models within this series. The inspection must focus on the internal flange radius of the wheels and can be conducted using either an approved eddy current or ultrasonic technique. Compliance with this directive is mandated at each tyre removal after 3 August 1971, ensuring that all Fokker F28 aeroplanes maintain the required safety standards. The scope of this legislation extends to all operators of the specified aircraft model, ensuring that safety directives are uniformly enforced across the industry to maintain high safety standards in civil aviation.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39 - 105, outline specific safety directives that apply to the maintenance and inspection of aircraft. Within this body of law, AD/F28/17 addresses the inspection requirements for the main landing gear wheels of Fokker F28 Series aeroplanes. This directive (section 105) mandates that inspections of the Goodyear main landing gear wheels must be conducted in the area of the internal flange radius, utilising either an approved eddy current or ultrasonic technique (section 105(1)). This inspection is a critical safety measure, applicable to all models of the Fokker F28 Series (section 105(2)).
The obligations imposed by AD/F28/17 on operators and maintenance personnel are clear and specific. They must ensure that the inspections are carried out at each tyre removal following the directive's effective date, which is 3 August 1971 (section 105(3)). The use of approved techniques is mandatory, and the results of these inspections must be meticulously documented to ensure compliance with safety standards. Failure to adhere to these requirements could lead to serious safety risks and potential non-compliance with civil aviation regulations.
Breaching the provisions of AD/F28/17 can have significant consequences. While the Civil Aviation Regulations do not explicitly state penalties for non-compliance with this specific directive, general provisions within the regulations allow for enforcement actions against entities that fail to meet their obligations. These actions can include fines, suspension or revocation of airworthiness certificates, and other regulatory sanctions. The potential severity of these penalties underscores the importance of strict adherence to the inspection requirements set forth in AD/F28/17. Non-compliance not only poses a risk to the safety of the aircraft and its occupants but also subjects the offending party to legal repercussions that could impact their operations and reputation.