AD/BEECH 200/12 Amdt 2 - Vertical Stabiliser

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, provide comprehensive regulations to ensure the safety and efficiency of civil aviation within the country. Within this legislative framework, Part 39 specifically addresses the safety of aircraft through Airworthiness Directives, aiming to address safety deficiencies and ensure that aircraft maintain an acceptable level of safety throughout their operational life. The policy objective of these regulations is to safeguard the public by mandating that aircraft meet specific safety standards and undergo regular inspections and maintenance. One such Airworthiness Directive pertains to the Beechcraft 200 (Super King Air) Series Aeroplanes, specifically addressing the vertical stabiliser. AD/BEECH 200/12 Amendment 2, issued in 1978, applies to certain models with specific serial numbers and mandates actions in accordance with Beechcraft Service Information No 0810-134, Revision 1. This directive requires compliance with the specified requirements to ensure the structural integrity of the vertical stabiliser, thereby maintaining the overall airworthiness of the aircraft. Ansett Airlines of Australia’s repair scheme, identified by ER No XB-55-30-1A, is recognised as an acceptable method of compliance.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105, pertains to the safety directives issued by the Civil Aviation Safety Authority (CASA) and applies to the Beechcraft 200 (Super King Air) series aeroplanes. The legislation mandates specific action concerning the vertical stabiliser of these aircraft and applies to all models with specific serial numbers, including BB-2 to BB-137, BB-138 to BB-185, BB-187 to BB-202, BB-204 to BB-269, BB-271 to BB-301, as well as BT-1, BT-2, and BT-3. Compliance with the directive necessitates adherence to the actions outlined in Beechcraft Service Information No 0810-134, Rev 1. Notably, Ansett Airlines of Australia's repair scheme, denoted as ER No XB-55-30-1A, is recognised as an acceptable method for achieving compliance. This regulation, administered by CASA, ensures the safety and airworthiness of the specified Beechcraft aeroplanes within the Australian jurisdiction.

Key Provisions

The Civil Aviation Regulations 1998, Part 39 - 105, specifically under Schedule of Airworthiness Directives, outlines key provisions concerning the Beechcraft 200 (Super King Air) Series Aeroplanes (AD/BEECH 200/12). This section mandates actions to be taken regarding the vertical stabiliser of the aircraft, particularly for models with serial numbers within the specified ranges (Sections 39-105). The directive requires operators to follow the instructions detailed in Beechcraft Service Instruction No 0810-134, Revision 1. It is also noted that the repair scheme used by Ansett Airlines of Australia, identified by Engineering Order Number XB-55-30-1A, is acceptable for compliance purposes. The Act imposes clear obligations on the entities that operate these aircraft. Specifically, they must ensure that all required actions concerning the vertical stabiliser are implemented in line with the specified service instruction. This includes conducting the necessary repairs or modifications as outlined in the directive to maintain the aircraft's airworthiness. Compliance with the directive is critical, and operators must document their adherence to the requirements set forth in the directive's accompanying documentation. Failure to comply with the provisions of this airworthiness directive can result in significant consequences. While the specific penalties are not detailed within the legislative instrument, non-compliance with airworthiness directives generally can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). These actions may include fines, operational restrictions, or even the grounding of the aircraft until the required actions are satisfactorily completed. The seriousness of the consequences underscores the importance of adhering to the specified requirements to ensure the safety and compliance of the aircraft in operation.