Overview

The Civil Aviation Regulations 1998, which were enacted by the Parliament of Australia, encompass a broad range of regulations designed to ensure safety and efficiency within Australia's civil aviation sector. One specific legislative instrument, F2006B09676, addresses safety concerns associated with Fokker F27 Series aeroplanes, particularly targeting issues related to the inboard aileron hinge bolt retention. This instrument was introduced to rectify a problem where restricted aileron movement was caused by the migration of the hinge bolt and bush, which could compromise the safety of the aircraft. The policy objective is to mandate inspections and replacements for affected aeroplanes, ensuring that the inboard aileron hinge bolts are retained securely, thus enhancing overall aircraft safety and compliance with aviation standards. The Civil Aviation Safety Authority, through this directive, aims to mitigate potential risks by requiring compliance with specific inspection and replacement protocols for Fokker F27 Series aeroplanes with serial numbers between 10105 and 10635. This proactive approach underscores the commitment to maintaining stringent safety measures within the civil aviation industry, ensuring that all aircraft meet the necessary safety standards to protect passengers and crew.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates the applicability of Airworthiness Directives (ADs) issued by the Civil Aviation Safety Authority (CASA) to ensure the safety and airworthiness of aircraft within Australian airspace. This legislative instrument applies to all Fokker F27 series aeroplanes with serial numbers (S/Nos.) ranging from 10105 to 10635, requiring these aircraft to undergo an inspection and, if necessary, the replacement of inboard aileron hinge bolt retentions as outlined in Fokker Service Bulletin F27/57-58. This directive aims to prevent restricted aileron movement caused by the migration of the hinge bolt and bush. The regulation mandates compliance with these directives before 1st January 1984, with additional context provided by Referenced Local Document AD BLA 83-20-57. This legislation applies broadly across the Commonwealth, ensuring that all relevant aircraft within the specified serial number range comply with the stipulated safety measures. The application of these regulations is not restricted by jurisdictional boundaries within Australia, thereby extending its reach to all operators and owners of the specified Fokker F27 aircraft, regardless of where they are based or operate. The legislation does not explicitly state any exclusions, exemptions, or thresholds, implying a broad application intended to enhance the safety standards of these aircraft. Furthermore, the application of these regulations can be extended or refined through subordinate instruments issued by CASA, ensuring that the safety directives remain up-to-date and effective in addressing any emerging issues.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, includes AD/F27/107 concerning the inspection and replacement of inboard aileron hinge bolt retention for Fokker F27 Series Aeroplanes. This directive applies to all model F27 aircraft with serial numbers ranging from 10105 to 10635 (Section 105). The required actions and documentation are detailed in Fokker SB F27/57-58, with a reference to RLD AD BLA 83-20-57. Compliance with this directive was mandated before 1st January 1984, following reports of restricted aileron movement due to hinge bolt and bush migration (Section 8/83). Under the Civil Aviation Regulations, the entities governed by AD/F27/107 must ensure that the specified inboard aileron hinge bolt retention is inspected and, if necessary, replaced to prevent restricted aileron movement. This inspection and replacement must be conducted in accordance with the procedures outlined in Fokker SB F27/57-58. It is imperative that these actions are completed to maintain the airworthiness of the aircraft as per the Civil Aviation Safety Authority's standards. The directive mandates that these steps are to be taken before the specified compliance date, ensuring that all affected aircraft meet the required safety standards. Failure to comply with the provisions of AD/F27/107 may result in significant legal and operational consequences. The Civil Aviation Regulations 1998 establish that non-compliance with airworthiness directives can lead to the grounding of aircraft, which can severely impact operations. Furthermore, operators who do not adhere to these directives may face enforcement actions by the Civil Aviation Safety Authority. While the specific penalties are not detailed in the provided text, non-compliance with airworthiness directives generally results in enforcement actions that could include fines, operational restrictions, or other regulatory penalties. It is therefore critical for operators to ensure full compliance to avoid any adverse outcomes.