COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fuji FA-200 Series Aeroplanes
AD/FA-200/14 Main Landing Gear Assemblies - Modification NK
Applicability: All models with S/Nos. 2 to 201. Document: Fuji SB No. FAS-065.
Compliance: Within 100 hours time in service after 28 April 1972.
Overview
The Civil Aviation Regulations 1998 (Cth) were enacted to provide a comprehensive regulatory framework governing all aspects of civil aviation within Australia, ensuring the safety and efficiency of the national airspace. Within this extensive legislative instrument, Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives includes specific regulations tailored to various aircraft models, addressing particular safety concerns and mandating corrective actions. The 1998 Regulations were introduced to streamline and modernise the regulatory environment for civil aviation, aiming to enhance safety and operational standards across the industry.
One particular Airworthiness Directive, AD/FA-200/14, pertains to Fuji FA-200 Series Aeroplanes and mandates modifications to the main landing gear assemblies. This directive applies to all models with serial numbers 2 to 201, with compliance required within 100 hours of time in service following 28 April 1972. The directive references Fuji Service Bulletin No. FAS-065, underscoring the importance of adhering to manufacturer-specific guidelines to maintain airworthiness. The policy objective underlying these regulations is to ensure that all aircraft meet stringent safety standards, thereby protecting passengers, crew, and the general public from potential hazards.
Scope and Application
The Civil Aviation Regulations 1998, as amended, specifically Part 39 - 105 under the Civil Aviation Safety Authority, encompasses the Airworthiness Directives for various aircraft types, including Fuji FA-200 Series Aeroplanes. This regulation mandates compliance with AD/FA-200/14, which focuses on the modification of main landing gear assemblies. This directive applies to all Fuji FA-200 Series aeroplanes with serial numbers ranging from 2 to 201, requiring the implementation of the specified modifications within 100 hours of time in service following 28 April 1972. The directive references Fuji Service Bulletin No. FAS-065, which outlines the required modifications and procedures. The scope of this regulation extends across the Commonwealth of Australia, ensuring that all applicable aircraft within this jurisdiction adhere to the specified safety standards and modifications. No specific exclusions or exemptions are mentioned within the text, indicating that all affected aircraft must comply with the directive. The application of these regulations may be further detailed or extended through subordinate instruments issued by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39, specifically Section 105, pertain to the Fuji FA-200 Series Aeroplanes and mandate modifications to the main landing gear assemblies. This directive, AD/FA-200/14, applies to all Fuji FA-200 models with serial numbers (S/Nos.) 2 to 201, with compliance required within 100 hours of time in service after 28 April 1972, as documented in Fuji Service Bulletin No. FAS-065. This directive ensures that the specified aircraft models meet certain safety standards regarding their landing gear assemblies.
The regulations impose several obligations on the entities responsible for the maintenance and operation of the Fuji FA-200 Series Aeroplanes. Primarily, these entities must ensure that the modifications to the main landing gear assemblies are carried out as per the guidelines set out in Fuji Service Bulletin No. FAS-065. This includes conducting necessary inspections, making required alterations, and documenting the compliance process meticulously. Failure to adhere to these requirements can result in non-compliance with civil aviation safety standards.
Breaches of the provisions set out in the Civil Aviation Regulations 1998 can lead to significant consequences. Under these regulations, any entity that fails to comply with the mandatory modifications to the main landing gear assemblies within the specified timeframe may face enforcement actions. The potential penalties for non-compliance include fines and other regulatory sanctions, as outlined in the broader framework of the Civil Aviation Act 1988 and associated regulations. The exact penalties can vary, but they are intended to enforce compliance and maintain the high safety standards of civil aviation in Australia.