COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fokker F27 Series Aeroplanes
AD/F27/26 RPM Control System - Gustlock Interference System - Improvement
Document: Fokker SB F-9.
10/60
Overview
The Civil Aviation Regulations 1998, as amended by the Legislative Instrument F2006B09726, specifically address issues related to the airworthiness of Fokker F27 series aeroplanes. Enacted by the Commonwealth of Australia, this legislation aims to ensure that specific modifications and improvements are implemented to maintain the safety standards of these aircraft. The policy objective behind these regulations is to mitigate risks associated with the RPM control system and gustlock interference by mandating specific improvements as outlined in Fokker Service Bulletin F-9, dated 10/60. This legislative measure is crucial in safeguarding the operational integrity and safety of Fokker F27 series aeroplanes within the Australian aviation industry.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to the Fokker F27 Series Aeroplanes and governs the requirements for their airworthiness. This regulation mandates the implementation of Airworthiness Directives (ADs) to ensure safety standards are met. The legislation applies to all aircraft operators and maintenance providers who are responsible for ensuring compliance with these directives, particularly concerning the RPM control system and the gustlock interference system. The scope of this regulation is national, extending across the Commonwealth of Australia, and it applies to any Fokker F27 aeroplanes operating within Australian airspace. There are no specified exclusions or exemptions outlined in this directive, and compliance is mandatory for all relevant parties. The regulation may also extend its application through subordinate instruments, which provide further detail and clarification on the implementation and enforcement of the ADs.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, which governs the maintenance and operational standards of various aircraft types, including Fokker F27 Series Aeroplanes. One such directive, AD/F27/26, pertains to the RPM Control System and the Gustlock Interference System (section 105). This directive mandates improvements to these systems to ensure the safety and reliability of the aircraft in operation. The directive references Fokker SB F-9, document number 10/60, which provides detailed specifications and instructions for compliance.
The AD/F27/26 directive imposes specific obligations on aircraft operators and maintenance personnel. Operators must ensure that all modifications and inspections are performed in accordance with the detailed specifications outlined in the referenced Fokker SB F-9 document (section 105). This includes adherence to the technical standards and procedures for the RPM Control System and the Gustlock Interference System. Maintenance personnel must be qualified and authorised to perform the required tasks, and all work must be logged and certified accordingly to demonstrate compliance with the directive.
Failure to comply with the AD/F27/26 directive can result in serious consequences. The Civil Aviation Safety Authority has the authority to enforce these regulations, and non-compliance may lead to the grounding of the aircraft until the required modifications and inspections are completed (section 105). Additionally, operators and maintenance personnel found in breach of these requirements may face penalties, which could include fines and other sanctions. The exact penalties depend on the severity of the breach and the circumstances surrounding it, but they are intended to ensure that the safety standards are upheld rigorously.