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 65/14
Amdt 4
Elevator Control Rods 3/89
Applicability: All models Queen Air 65, A65 and A65-8200 with S/Nos. L-1, L-2, L-6, LF-7, LF-8 and LC-1 to LC-335; All models 65-80, 65-A80 and 65-B80 with S/Nos. LD-1 to LD-511; All models 65-88 with S/Nos. LP-1 to LP-28, LP-30 to LP-47. Models Queen Air 70 with S/Nos LB-1 through LB-35.
Requirement: Action in accordance with Beechcraft SI No. 0334-152, Rev. III. Compliance: As per requirement document.
Background: Amendment 4 consolidates Queen Air series 65 and 70 aircraft.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, establish comprehensive regulations for the safety and operation of civil aviation within the country. These regulations form a crucial part of Australia's legislative framework to ensure the safety and efficiency of civil aviation. One specific legislative instrument, F2006B04119, pertains to Airworthiness Directives for the Beechcraft 65 and 70 (Queen Air) series aeroplanes, aiming to address safety concerns associated with these aircraft models. The policy objective of this directive is to enhance the airworthiness and operational safety of these specific aircraft by mandating compliance with detailed maintenance and inspection requirements, ensuring that any identified safety issues are promptly and effectively addressed.
The enactment of this Airworthiness Directive is a direct response to identified safety risks associated with the elevator control rods in Beechcraft 65 and 70 series aeroplanes. By specifying detailed action in accordance with Beechcraft Service Information Notice No. 0334-152, Rev. III, the directive provides a clear and authoritative framework for maintaining the safety standards of these aircraft. Compliance with this directive is essential for operators to ensure that their aircraft meet the necessary safety criteria, thereby protecting both the passengers and crew, and maintaining the integrity of Australia's civil aviation system.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 – 105, issued by the Civil Aviation Safety Authority, encompass detailed airworthiness directives which mandate compliance for certain aircraft models within Australian airspace. This particular legislative instrument, AD/BEECH 65/14 Amendment 4, pertains to the elevator control rods of all Beechcraft 65 and 70 (Queen Air) series aeroplanes. It applies to specific serial numbers of these aircraft, ensuring safety and airworthiness standards are met. The directive is applicable to all relevant aircraft operating within the Australian jurisdiction, and compliance must adhere to the requirements outlined in Beechcraft Service Instruction No. 0334-152, Revision III. This regulation does not extend to other aircraft models or serial numbers not specified in the directive, thereby establishing clear parameters for its application.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, detail the Civil Aviation Safety Authority's (CASA) schedule of airworthiness directives for various aircraft models, including the Beechcraft 65 and 70 (Queen Air) series aeroplanes. Section AD/BEECH 65/14 Amendment 4, concerning the elevator control rods, applies to all Queen Air 65 models with specific serial numbers, as well as Queen Air 70 models with their respective serial numbers. The requirement outlined in this directive mandates that the action taken must align with Beechcraft Service Instruction No. 0334-152, Revision III. Compliance with this directive is to be achieved in accordance with the specifications provided in the referenced requirement document.
The Civil Aviation Regulations impose clear obligations on the owners and operators of the specified Beechcraft 65 and 70 series aircraft. They must ensure that the elevator control rods of their aircraft are addressed in accordance with the detailed instructions provided in the Beechcraft Service Instruction No. 0334-152, Revision III. This involves following the outlined procedures for inspection, repair, or replacement of the elevator control rods as necessary to maintain the airworthiness of the aircraft. Failure to comply with these directives can lead to serious safety implications and potential regulatory consequences.
The legislation also outlines potential consequences for non-compliance with the airworthiness directives. Under the Civil Aviation Regulations, any breach of the specified directives can result in significant civil or criminal penalties. The severity of the penalties depends on the nature and extent of the non-compliance but can include fines, operational restrictions, or even the grounding of the aircraft until compliance is achieved. The exact penalties are stipulated in the broader Civil Aviation Act 1988, which provides for substantial fines and imprisonment for serious breaches of aviation safety regulations. Ensuring adherence to these directives is, therefore, critical for maintaining the safety and legality of operating these aircraft within Australia.