Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, are a comprehensive set of rules and regulations governing civil aviation in Australia, established to ensure safety and compliance within the industry. Within this expansive regulatory framework, Part 39 - 105 specifically addresses the Airworthiness Directives for various aircraft types, including the Beechcraft 90 and 65-90 (King Air) Series Aeroplanes. This particular legislation, identified as F2006B04230, was introduced to address safety concerns related to the landing gear actuators of these aircraft models. The policy objective is to mandate regular inspections of the landing gear actuators, ensuring they meet specific safety standards to prevent potential failures and enhance overall aviation safety. The directive is designed to be enforced through compliance with documented requirements, as outlined in the referenced Beechcraft SB 66-50, Rev. 1.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all models of Beechcraft 90 and 65-90 (King Air) series aeroplanes, establishing mandatory airworthiness directives that ensure safety and compliance within the Australian aviation industry. These regulations apply to aircraft operators, maintenance personnel, and other relevant entities involved in the operation and maintenance of these aircraft models. The geographic reach of these regulations is national, encompassing the entire Commonwealth of Australia, thereby ensuring uniform safety standards across the country. The regulations detail specific requirements for inspecting landing gear actuators, as outlined in the relevant documents such as Beechcraft SB 66-50, Rev. 1, with compliance necessary to meet the stipulated safety standards. While these regulations provide comprehensive coverage, any exclusions or exemptions are not specified within the text provided, and further details may be found in subordinate instruments or related documentation.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically address the airworthiness directives concerning Beechcraft 90 and 65-90 (King Air) series aeroplanes. Section 4/72 of this legislative instrument mandates that all models of the specified aircraft series must undergo a detailed inspection of the landing gear actuators (AD/BEECH 90/4 Amendment 3). The compliance requirement is outlined in Beechcraft Service Bulletin 66-50, Revision 1, which provides the necessary procedures and standards to ensure that the inspection is conducted appropriately. Entities and operators of the Beechcraft 90 and 65-90 series aeroplanes must adhere to the stipulated inspection requirements set forth in the Civil Aviation Regulations. This includes ensuring that the landing gear actuators are inspected in accordance with the detailed specifications provided in the referenced service bulletin. Operators are obligated to maintain records of all inspections and any resultant actions taken, ensuring that the aircraft remains in a state of airworthiness. Failure to comply with these airworthiness directives can result in significant legal and operational consequences. If an operator fails to conduct the required inspections or does not adhere to the specifications provided in Beechcraft Service Bulletin 66-50, Revision 1, they may face enforcement actions. Under the Civil Aviation Act 1988, non-compliance can lead to penalties, including fines and potential grounding of the aircraft. The specific maximum penalties for breaches of these regulations are detailed in the Civil Aviation Regulations and can vary depending on the severity and frequency of the non-compliance. It is crucial for operators to understand and comply with these directives to avoid legal repercussions and ensure the safety of their operations.