COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 65 and 70 (Queen Air) Series Aeroplanes
AD/BEECH 65/59
Amdt 1
Elevators 3/89
Applicability: All models Queen Air 65, A65, A65-8200 and 70 with S/Nos referenced in Beechcraft Service Bulletin No. 2030.
Requirement: Action in accordance with Beechcraft S.B. No. 2030.
Compliance: Unless already accomplished per Beechcraft SI No. 1207, within 100 hours’ time in service after 31 December 1984.
Background: Elevators on certain aeroplanes or aeroplanes fitted with replacement elevators may have improperly bonded honeycomb stiffener strips installed. S.B. No. 2030 extends compliance to model, corrects part number errors and supersedes and cancels Service Instruction No. 1207. Amendment 1 consolidates Queen Air series 65 and 70, aircraft.
Overview
The Civil Aviation Regulations 1998, under PART 39 - 105, establish a comprehensive regulatory framework for civil aviation in Australia, addressing safety and operational standards. This legislation was enacted to ensure that civil aviation activities in Australia are conducted in a safe and orderly manner, aiming to protect the public and enhance the efficiency of the aviation industry. The problem this Act was introduced to address included the need for stringent safety protocols and the harmonisation of regulatory standards across the aviation sector to prevent accidents and ensure a high level of safety for passengers and crew.
The Civil Aviation Regulations 1998 are administered by the Civil Aviation Safety Authority (CASA), which is tasked with enforcing these regulations. The policy objective underlying this legislation is to maintain and enhance the safety of civil aviation through rigorous oversight and compliance measures. By issuing specific airworthiness directives, such as AD/BEECH 65/59 Amendment 1, CASA ensures that aircraft manufacturers and operators adhere to critical safety standards, thereby mitigating potential risks associated with aircraft operations.
Scope and Application
The Civil Aviation Safety Authority's Schedule of Airworthiness Directives, specifically AD/BEECH 65/59 Amendment 1, applies to all models within the Queen Air 65, A65, A65-8200, and 70 series aeroplanes with serial numbers as referenced in Beechcraft Service Bulletin No. 2030. This legislative instrument pertains to the maintenance and safety standards of these aircraft, particularly addressing the potential issue of improperly bonded honeycomb stiffener strips on the elevators. The requirement necessitates compliance with the actions outlined in Beechcraft Service Bulletin No. 2030. Compliance must be achieved unless it has already been fulfilled in accordance with Beechcraft Service Instruction No. 1207, and must be done within 100 hours of the aircraft being in service after 31 December 1984. This directive is part of a broader regulatory framework aimed at ensuring the safety and airworthiness of aircraft operating under Australian jurisdiction. The directive extends its reach to cover specific aircraft models, ensuring that any identified safety issues are rectified through adherence to the specified service bulletins and instructions.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39 - 105, impose specific safety directives for certain aircraft models, including the Beechcraft 65 and 70 (Queen Air) series aeroplanes. This regulation, AD/BEECH 65/59 Amendment 1, focuses on the elevators of these aircraft, specifying actions that must be taken to ensure airworthiness. According to section (3/89), the directive applies to all models Queen Air 65, A65, A65-8200, and 70 with specific serial numbers as referenced in Beechcraft Service Bulletin No. 2030. The primary requirement, as outlined in this section, is to undertake the actions detailed in Beechcraft Service Bulletin No. 2030, ensuring that the honeycomb stiffener strips on the elevators are properly bonded. This is a critical safety measure to prevent potential structural failures in the elevators, which could compromise the aircraft's safety.
The obligations imposed by this directive on the operators and owners of the affected aircraft are clear and specific. Operators must ensure that the required actions are completed in accordance with the guidelines set out in Beechcraft Service Bulletin No. 2030. This involves a thorough inspection and, if necessary, the replacement or repair of improperly bonded honeycomb stiffener strips on the elevators. Compliance must be achieved within 100 hours of the aircraft's time in service after 31 December 1984, unless the actions have already been completed as per Beechcraft Service Instruction No. 1207. This mandate is critical to maintaining the structural integrity and safety of the aircraft.
Failure to comply with the provisions of this directive can result in serious consequences. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement action against non-compliance, which could include fines, penalties, or even the grounding of the aircraft until the required actions are completed. While the specific penalties are not detailed in the provided text, non-compliance with aviation safety directives is generally considered a serious offence, potentially leading to criminal charges in severe cases. Ensuring adherence to these directives is essential to uphold the high safety standards required in civil aviation.