AD/BEECH 60/3 - Retract Cable Actuator Arm Shear Rivet

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, were established to regulate the safety and efficiency of civil aviation within Australia. The regulations form a comprehensive framework that addresses various aspects of aviation operations, including the airworthiness of aircraft. One specific legislative instrument under these regulations, F2006B04090, pertains to the safety directive for the Beechcraft 60 (Duke) series aeroplanes, specifically targeting the retract cable actuator arm shear rivet issue as outlined in AD/BEECH 60/3. This safety directive was introduced to address a critical safety concern regarding the potential failure of the retract cable actuator arm shear rivet, which could compromise the aircraft's structural integrity and operational safety. The policy objective is to ensure that all affected aircraft meet stringent safety standards before being issued a Certificate of Airworthiness, thereby safeguarding the public and maintaining high safety standards in the aviation industry.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, mandates the implementation of Airworthiness Directives (ADs) to ensure the safety and airworthiness of aircraft. AD/BEECH 60/3 pertains to Beechcraft 60 (Duke) Series Aeroplanes, applying to specific models with serial numbers P-1 to P-42, P-44 to P-49, P-51, P-52, P-54, and P-55. The directive requires compliance with Beechcraft Service Instruction No. 0186-112, mandating specific action before a Certificate of Airworthiness can be issued. The scope of this regulation extends to ensuring that the retract cable actuator arm shear rivet is addressed to maintain the structural integrity and safety of the aircraft. This legislation applies on a Commonwealth level, ensuring uniform standards across Australia. There are no stated exclusions or exemptions within the provided text, and compliance is mandatory for the specified aircraft models. The regulation’s reach is limited to the specific aircraft models and the condition outlined, with no indication of broader application through subordinate instruments in this excerpt.

Key Provisions

The key provisions of the Civil Aviation Regulations 1998, specifically in relation to the Beechcraft 60 (Duke) Series Aeroplanes, are outlined in Part 39 - 105 (Sections 39.105). These provisions concern the Airworthiness Directives (AD) issued by the Civil Aviation Safety Authority (CASA). One such directive, AD/BEECH 60/3, pertains to the retract cable actuator arm shear rivet of certain models of the Beechcraft 60 series. This directive applies to aircraft with serial numbers (S/Nos.) P-1 to P-42, P-44 to P-49, P-51, P-52, P-54, and P-55. The requirement, as stated in this directive, is that action must be taken in accordance with Beechcraft Service Instruction (SI) No. 0186-112. The obligations imposed by this Act on the parties or entities it governs are quite specific. Owners or operators of the affected Beechcraft 60 series aircraft must ensure that the specified action is taken as per the referenced service instruction. This involves inspecting and potentially replacing or repairing the retract cable actuator arm shear rivet to ensure compliance with airworthiness standards. Compliance with these directives is mandatory and must be achieved before a Certificate of Airworthiness can be issued or maintained for these aircraft. The Civil Aviation Regulations 1998 also detail the potential consequences for non-compliance with these directives. Failure to adhere to the requirements set forth in the AD/BEECH 60/3 could result in severe civil or criminal penalties. Under the Act, non-compliance with airworthiness directives can lead to the issuance of penalties, with maximum fines and potential imprisonment for serious breaches. Specifically, the Act may impose financial penalties for each instance of non-compliance, and in more severe cases, criminal charges could be brought against the responsible parties, leading to imprisonment. These provisions underscore the importance of adhering to the specified airworthiness directives to ensure the safety and compliance of the aircraft in operation.