AD/BEECH 60/4 - Elevator and Tab Controls

Overview

The Civil Aviation Regulations 1998 (Cth), as amended, are a comprehensive set of rules and standards governing civil aviation within Australia, administered by the Civil Aviation Safety Authority (CASA). The 1998 Regulations were enacted to provide a uniform framework for the safe operation of aircraft, ensuring that civil aviation activities are conducted in a manner that protects the public and promotes efficient and orderly air traffic management. A specific amendment to these regulations is AD/BEECH 60/4, which targets elevator and tab controls on Beechcraft 60 (Duke) series aeroplanes. This directive applies to aircraft with serial numbers P-1 to P-48, with the exceptions of P-43 and P-45, and requires compliance with Beechcraft Service Instruction No. 0187-152 before the issue of a Certificate of Airworthiness. The overarching policy objective is to ensure that aircraft maintain a high standard of airworthiness, thereby enhancing aviation safety.

Scope and Application

The Civil Aviation Regulations 1998, as outlined in Part 39 - 105 of the Commonwealth of Australia's legislative framework, mandate specific airworthiness directives for certain aircraft models, including the Beechcraft 60 (Duke) series aeroplanes. This particular directive, AD/BEECH 60/4, pertains to elevator and tab controls for Model 60 aircraft with serial numbers P-1 to P-48, excluding P-43 and P-45. The directive necessitates compliance with Beechcraft Service Instruction No. 0187-152, ensuring that all specified modifications are implemented prior to the issuance of a Certificate of Airworthiness. This regulatory requirement applies specifically to the affected aircraft models and serial numbers within the Australian jurisdiction, thereby ensuring that all applicable aircraft meet the requisite safety standards before they are allowed to operate. The directive does not explicitly extend its application through subordinate instruments, focusing solely on the specified aircraft models and the outlined modifications.

Key Provisions

The Civil Aviation Regulations 1998 (Cth), under Part 39, particularly section 105, mandates specific safety directives for certain types of aircraft, such as the Beechcraft 60 (Duke) Series Aeroplanes. Section AD/BEECH 60/4, which addresses elevator and tab controls, specifies the applicability of these directives to model 60 with serial numbers (S/Nos) ranging from P-1 to P-48, excluding P-43 and P-45. The requirement outlined in this section necessitates compliance with Beechcraft Service Instruction No. 0187-152, ensuring that these aircraft meet the necessary safety standards before a Certificate of Airworthiness is issued. The obligations imposed by this legislation are stringent, focusing on ensuring the safety and airworthiness of the specified aircraft models. Operators of these aircraft must adhere to the specific directives outlined in the service instruction, which likely involves inspecting, repairing, or replacing certain elevator and tab control components to meet safety standards. This compliance is critical before any Certificate of Airworthiness can be granted, which is necessary for the legal operation of the aircraft in Australian airspace. Failure to comply with the directives and requirements set forth in section AD/BEECH 60/4 could result in serious consequences. The regulations stipulate that any aircraft that does not meet the specified safety criteria will not be issued a Certificate of Airworthiness. This lack of certification means the aircraft cannot legally be operated, potentially leading to civil penalties for non-compliance. Additionally, the continued operation of a non-compliant aircraft poses significant safety risks, which could result in criminal charges if harm or fatalities occur. The potential penalties for these breaches can be severe, reflecting the importance of adhering to these safety directives.