COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 200 (Super King Air) Series Aeroplanes
AD/BEECH 200/31
Amdt 1
Elevator Control Horn Attachment 5/81
Applicability: All models 200 with S/Nos BB-3 to BB-674. All models 200C with S/Nos BL-1 to BL-8. All models 200T with S/Nos BT-1 to BT-16.
Requirement: Action in accordance with Beechcraft SI No 1111 Rev 1.
Compliance: Unless already accomplished, within 100 hours time in service after 31 May 1981.
Background: The installation of additional rivets in the elevator control horn attachment has been found necessary under service conditions to prevent looseness developing in this control connection. This amendment adds additional aeroplanes and revises accomplishment instructions.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, provide the framework for ensuring the safety and efficiency of civil aviation within the country. Part 39 of these regulations includes specific safety directives that aircraft manufacturers and operators must comply with. The Legislative Instrument F2006B03688, amending the Airworthiness Directives for the Beechcraft 200 (Super King Air) Series Aeroplanes, was introduced to address a particular safety concern identified in these aircraft models. The problem it was designed to resolve involved the potential for looseness in the elevator control horn attachment, which could compromise flight safety. The policy objective of this directive is to mandate corrective actions, as specified in Beechcraft Service Instruction No 1111 Revision 1, to ensure the integrity of the elevator control connection, thereby maintaining the overall airworthiness of the affected aircraft. Compliance with this directive is mandatory within 100 hours of time in service after 31 May 1981, ensuring that all specified aircraft models receive the necessary modifications to prevent any safety issues arising from this specific component.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, applies to all Beechcraft 200 (Super King Air) Series Aeroplanes, including specific serial number ranges for various models: all models 200 with serial numbers BB-3 to BB-674, all models 200C with serial numbers BL-1 to BL-8, and all models 200T with serial numbers BT-1 to BT-16. This legislation is designed to ensure the safety of these aircraft by mandating compliance with specified maintenance requirements. The requirement, as detailed in Beechcraft Service Information (SI) No 1111 Revision 1, mandates that action must be taken to reinforce the elevator control horn attachment unless this has already been completed, within 100 hours of time in service after 31 May 1981. This is crucial to prevent the development of looseness in the control connection, which could potentially compromise the safety of the aircraft during operation. The regulations are applicable across the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority, and no specific exclusions or exemptions are noted within the specified scope of the directive.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes a schedule of airworthiness directives that pertain to various aircraft types, including the Beechcraft 200 series. One such directive is AD/BEECH 200/31 Amendment 1, which addresses the elevator control horn attachment for specific models of the Beechcraft 200 (Super King Air) aeroplanes (Section 39-105). The directive applies to all Beechcraft 200 models with serial numbers within the specified ranges, as well as all Beechcraft 200C and 200T models within their respective serial number ranges. The directive requires action to be taken in accordance with Beechcraft Service Instruction (SI) No 1111, Revision 1 (Section 39-105).
The obligation under this directive is for the relevant parties, typically the aircraft operators or maintenance providers, to ensure that the specified action is taken on the affected aircraft. The action must be completed within 100 hours of time in service following the date of 31 May 1981. This directive mandates that additional rivets be installed in the elevator control horn attachment to prevent looseness in the control connection, a critical safety measure identified through service experience (Section 39-105).
Failure to comply with the airworthiness directive can result in serious safety implications, as the directive is aimed at addressing a known issue that could affect the aircraft's controllability. While the Civil Aviation Regulations 1998 do not specify a particular penalty for non-compliance with airworthiness directives, enforcement actions can be taken by the Civil Aviation Safety Authority (CASA). Such actions may include the issuance of compliance orders, fines, or in severe cases, grounding of the aircraft until the required actions are completed. The potential consequences underscore the importance of adhering to the stipulated requirements and timelines.
In summary, the directive outlines the need for specific action on the elevator control horn attachment of Beechcraft 200 series aeroplanes to ensure safety, sets forth the compliance timeline, and implies the serious consequences of non-compliance through regulatory enforcement mechanisms.