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-200/15 Nose Landing Gear Piston Stop NK
Plate Screws - Modification
Applicability: All models with S/Nos. 12 to 52. Document: Fuji SB No. FAS-060.
Compliance: Within 100 hours time in service after 28 April 1972.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Government, serve as a comprehensive set of rules governing civil aviation in the country. One of the specific legislative instruments under this broader framework is F2006B09927, which was introduced to address safety concerns related to the Fuji FA-200 Series Aeroplanes. This legislative instrument was enacted to ensure that all models with serial numbers 12 to 52 comply with the specified airworthiness directives, particularly regarding modifications to nose landing gear piston stop NK plate screws. The policy objective behind this regulation is to enhance aviation safety by mandating specific compliance actions within a defined time frame. This regulatory action was put in place by the Civil Aviation Safety Authority to ensure that the aviation industry adheres to stringent safety standards, thereby protecting the public and maintaining the integrity of civil aviation operations.
Scope and Application
The Civil Aviation Safety Authority (CASA) has issued Airworthiness Directive AD/FA-200/15 under the Civil Aviation Regulations 1998, specifically within Part 39. This directive pertains to the Fuji FA-200 Series Aeroplanes, particularly those with serial numbers ranging from 12 to 52. The directive is concerned with the modification of nose landing gear piston stop NK plate screws. This requirement applies to all relevant aircraft models and mandates compliance within 100 hours of time in service after the directive's issuance date of 28 April 1972. This directive is part of a broader regulatory framework aimed at ensuring the safety and airworthiness of the specified Fuji FA-200 Series aeroplanes, and adherence to the stipulated conditions is mandatory for continued operation of these aircraft within Australia’s jurisdiction. The directive’s applicability extends to the specified models, ensuring that modifications are made in accordance with the guidance provided in Fuji Service Bulletin No. FAS-060.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes Airworthiness Directives (AD) aimed at ensuring the safety of aircraft operations. One such directive, AD/FA-200/15, pertains to Fuji FA-200 Series Aeroplanes and specifically addresses the nose landing gear piston stop NK plate screws. This directive applies to all models with serial numbers between 12 and 52 (subsection 39.105(1)). Compliance with this directive is mandatory and must be achieved within 100 hours of time in service after 28 April 1972 (subsection 39.105(2)). The directive references Fuji Service Bulletin No. FAS-060 as the document containing the necessary modifications.
In terms of obligations and requirements, the AD/FA-200/15 mandates that the specified Fuji FA-200 Series Aeroplanes must undergo a modification to the nose landing gear piston stop NK plate screws as outlined in Fuji SB No. FAS-060. Operators and owners of the affected aircraft must ensure that the modifications are carried out by qualified personnel within the stipulated timeframe to maintain compliance with the Civil Aviation Regulations (subsection 39.105(3)). This requirement is crucial for ensuring the structural integrity and safety of the nose landing gear, which is a vital component during aircraft landing operations.
Failure to comply with the provisions of AD/FA-200/15 can result in serious consequences. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement actions against non-compliance. In cases of breach, the penalties can include fines and other sanctions as outlined in the Civil Aviation Act 1988 and the Civil Aviation Regulations 1998. The specific penalties for non-compliance with ADs can vary but may include substantial financial penalties. The severity of the penalty is dependent on factors such as the seriousness of the breach and the extent of non-compliance. Operators and owners must therefore ensure strict adherence to the directive to avoid any legal repercussions.