AD/BEECH 200/30 Amdt 3 - Wing Panel to Centre Section, Attach Fittings, Bolts and Nuts

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, are an extensive set of rules aimed at ensuring the safety and efficiency of civil aviation within the country. Within this framework, Part 39 outlines specific directives to maintain the airworthiness of aircraft. The legislative instrument F2006B03687 addresses the maintenance and safety standards for Beechcraft 200 (Super King Air) Series Aeroplanes. It was introduced to address the specific safety concerns associated with the attachment fittings, bolts, and nuts of the wing panels to the centre section of these aircraft. The policy objective is to ensure that the Beechcraft 200 series aeroplanes remain airworthy and compliant with safety standards by updating and cancelling outdated directives, as seen in the transition from AD/BEECH 200/30 Amendment 3 to AD/BEECH 200/39. The responsibility for enacting such regulations lies with the Parliament of Australia, reflecting a commitment to maintaining high safety standards in the nation's aviation sector.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, establish the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, which includes the Beechcraft 200 (Super King Air) Series Aeroplanes. These regulations apply to all aircraft operators, maintenance providers, and relevant aviation personnel who are responsible for ensuring compliance with airworthiness directives concerning these aircraft. The geographic reach of these regulations is national, as they are governed by the Commonwealth of Australia and apply across all states and territories. The regulations specify the requirements for the attachment fittings, bolts, and nuts of the wing panel to the centre section of the Beechcraft 200 series aeroplanes, and any failure to comply with these directives can result in serious safety risks. The mentioned amendment, AD/BEECH 200/30 Amendment 3, has been cancelled, with its intent now incorporated in the newer AD/BEECH 200/39. These directives are designed to ensure that the aircraft meet the necessary safety standards, and failure to adhere to them can lead to penalties or grounding of the aircraft.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, include specific airworthiness directives for various aircraft, such as the Beechcraft 200 (Super King Air) series aeroplanes. One such directive is AD/BEECH 200/30 Amendment 3 (sections referenced within the text). This directive concerns the attachment of fittings, bolts, and nuts for the wing panel to the centre section. Specifically, section 3/83 outlines the requirement for these attachments to be properly secured, ensuring the structural integrity and safety of the aircraft during flight. The obligations imposed by this directive on the operators and maintenance personnel of Beechcraft 200 series aeroplanes are clear and detailed. They must ensure that the wing panel to centre section fittings, bolts, and nuts are correctly installed and maintained according to the specifications provided in the directive. This involves regular inspections and adherence to the maintenance schedules outlined in the aircraft's maintenance manual. Any deviations from the specified procedures could compromise the aircraft's airworthiness and lead to regulatory non-compliance. Non-compliance with the requirements set forth in AD/BEECH 200/30 Amendment 3 can result in severe consequences. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement actions against operators who fail to adhere to the airworthiness directives. The potential penalties include fines, suspension or revocation of air operator certificates, and other administrative measures. In extreme cases, failure to comply with these directives could also lead to criminal charges against individuals or corporations responsible for the oversight of the aircraft, potentially resulting in substantial fines and imprisonment. The directive also emphasises the importance of using approved methods and materials for the installation and maintenance of the wing panel to centre section fittings, bolts, and nuts. This ensures that all work performed meets the highest safety standards and complies with the regulatory requirements. Operators must maintain records of all inspections, maintenance activities, and repairs related to these components to demonstrate compliance with the directive. These records are crucial for audits and inspections by CASA and must be readily available for review. In summary, AD/BEECH 200/30 Amendment 3 is a critical directive that mandates specific maintenance procedures for the wing panel to centre section fittings, bolts, and nuts on Beechcraft 200 series aeroplanes. Operators must ensure strict adherence to the directive's requirements to maintain the aircraft's airworthiness. Failure to comply can result in significant penalties, including fines and potential criminal charges. Keeping detailed records of all related maintenance activities is essential for demonstrating compliance and ensuring safety.