COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fokker F28 Series Aeroplanes
AD/F28/27 Liftdumper System - Wire Protection and
Segregation in Pedestal Modification
11/75
Applicability: For Part 1 - S/Nos. 11003 to 11032, 11034 to 11037, 11039 11071, and 11991 to 11993 unless either SB F28/27-101 or F28/27-111 has been accomplished.
For Part 2 - S/Nos. 11003 to 11083 and 11991 to 11993 unless SB F28/27-101 has been accomplished.
Document: 1. Fokker F28 SB No. F28/27-109; or
2. RLD AD No. 75-28-27 Fokker F28. Compliance: Before 1 January 1976.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, address the overarching regulation of civil aviation safety within the country. These regulations are instrumental in ensuring that aviation operations adhere to stringent safety standards, thereby protecting the public and maintaining the integrity of the national airspace. The specific legislative instrument F2006B09764 pertains to Airworthiness Directives, and it was introduced to address safety issues associated with specific aircraft models, such as the Fokker F28 Series Aeroplanes. This particular directive, AD/F28/27, targets the lift dumper system, focusing on wire protection and segregation in pedestal modifications. The directive mandates compliance before 1 January 1976, ensuring that identified Fokker F28 aircraft meet the specified safety criteria to mitigate risks associated with the lift dumper system. The policy objective is to enhance the safety and reliability of these aircraft by addressing potential wiring issues that could compromise flight safety.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, governs the safety directives concerning airworthiness, with the Airworthiness Directive AD/F28/27 focusing on Fokker F28 series aeroplanes. This directive mandates wire protection and segregation in the pedestal modification of the liftdumper system for specified serial numbers, unless certain service bulletins have been completed. For Part 1 of the directive, serial numbers 11003 to 11032, 11034 to 11037, 11039, 11071, and 11991 to 11993 are covered unless service bulletins F28/27-101 or F28/27-111 have been executed. For Part 2, the directive applies to serial numbers 11003 to 11083 and 11991 to 11993 unless service bulletin F28/27-101 has been accomplished. Compliance with these directives is required before 1 January 1976. The legislation applies to entities and individuals involved in the operation and maintenance of the specified Fokker F28 series aeroplanes within the Commonwealth of Australia, ensuring adherence to the stipulated safety standards.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes the Airworthiness Directives (AD) that are essential for maintaining the safety standards of aircraft in Australian airspace. One such directive, AD/F28/27, pertains to the Fokker F28 Series aeroplanes and mandates specific modifications to the liftdumper system, particularly focusing on wire protection and segregation in pedestal modifications (Section 11/75). The directive applies to certain serial numbers of the Fokker F28 aircraft, unless specific service bulletins (SB F28/27-101 or F28/27-111) have already been implemented (Section 11/75). The directive aims to ensure the safety of the aircraft by addressing potential hazards associated with the liftdumper system.
Under the Civil Aviation Regulations, the AD imposes several obligations on the parties involved. Aircraft operators and maintenance providers must ensure that the specified modifications are completed before 1 January 1976. This includes adhering to the instructions provided in Fokker F28 Service Bulletin No. F28/27-109 or the RLD AD No. 75-28-27 Fokker F28 (Section 11/75). These obligations ensure that the structural integrity and operational safety of the aircraft are maintained according to the prescribed safety standards.
Failure to comply with the provisions outlined in AD/F28/27 can result in serious consequences. The Civil Aviation Regulations stipulate that non-compliance may lead to the aircraft being considered non-airworthy, which can prevent it from operating until the required modifications are completed. There may also be legal repercussions, including fines and potential prosecution, as the regulations are designed to enforce strict adherence to safety standards to protect the public and maintain the integrity of civil aviation operations. The exact penalties are not specified in the provided text, but they can be severe, reflecting the critical nature of air safety.