Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, form a comprehensive legal framework governing all aspects of civil aviation within Australia. Part 39 of these regulations, specifically dealing with the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, outlines mandatory requirements to ensure that aircraft meet specific safety standards. This particular legislative instrument, F2006B09731, focuses on Fokker F27 Series Aeroplanes, addressing a recognised problem of potential failure in the autopilot servo rod, as stipulated in AD/F27/46. The policy objective of this directive is to enhance aviation safety by mandating regular inspection and maintenance of the autopilot servo rod to prevent any potential failure that could compromise flight safety.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, addresses the regulation of airworthiness directives for various types of aircraft, including the Fokker F27 Series Aeroplanes. This legislation applies to all operators and owners of Fokker F27 aircraft within the Commonwealth of Australia, ensuring that these aircraft meet the prescribed safety standards. The regulation mandates adherence to the specific airworthiness directive AD/F27/46 concerning the autopilot servo rod, as detailed in Fokker Service Bulletin 0-10. The directive ensures that any identified safety issues related to the autopilot servo rod are addressed to maintain the airworthiness of the aircraft. The regulation applies nationally across all states and territories of Australia, reinforcing the importance of compliance for the safety of all air passengers and crew. While the primary focus is on the safety and operational standards of the aircraft, there are no specific exclusions or exemptions outlined in this directive, although subordinate instruments may extend or clarify the application of these regulations.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, contains the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, with AD/F27/46 detailing requirements for the Fokker F27 Series Aeroplanes. Section 11/62 of this directive focuses on the autopilot servo rod. In plain terms, this section mandates specific actions to ensure the safety and airworthiness of Fokker F27 aircraft by addressing issues related to the autopilot servo rod. It requires aircraft operators to adhere to the instructions laid out in Fokker SB 0-10, a service bulletin that provides detailed guidance on inspection, maintenance, and repair procedures for the autopilot servo rod. The obligations under this directive are clear and specific. Operators of Fokker F27 aircraft must comply with the instructions provided in Fokker SB 0-10, which includes regular inspections and maintenance of the autopilot servo rod to prevent potential failures. This involves detailed checks for wear, corrosion, and any signs of damage or fatigue. If any issues are identified, operators must follow the repair or replacement procedures outlined in the service bulletin. Compliance with these obligations is crucial to maintain the airworthiness of the aircraft and ensure the safety of all passengers and crew. Failure to comply with the provisions outlined in AD/F27/46 and Fokker SB 0-10 can lead to significant consequences. Under the Civil Aviation Act 1988, non-compliance with airworthiness directives can result in enforcement actions by CASA. These actions may include fines, penalties, or even the grounding of the affected aircraft until the necessary repairs or inspections are completed. The specific penalties for non-compliance can vary, but they are designed to enforce adherence to safety standards and ensure that aircraft meet the required safety levels. The maximum penalties can include substantial financial fines and potential criminal charges for serious breaches, reflecting the seriousness of maintaining aviation safety standards.