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 200/23
Amdt 1
Inboard Aileron Hinge Arms 6/78
Applicability: All model 200 with S/Nos. BB-2 to BB-185, BB-187 to BB-202, BB-204 to BB-232.
All model 200T with S/Nos. BT-1 and BT-2.
Requirement: Action in accordance with Beechcraft SI No 0915, Rev 1.
Compliance: Unless already accomplished, within 100 hours time in service after 30 June 1978.
Overview
The Civil Aviation Regulations 1998 were enacted by the Australian Government to ensure the safety and efficiency of civil aviation within Australia, and this legislation is administered by the Civil Aviation Safety Authority (CASA). Part 39 - 105 of the Civil Aviation Regulations 1998 includes specific airworthiness directives aimed at addressing safety issues for certain aircraft models. One such directive is AD/BEECH 200/23 Amendment 1, which pertains to the Beechcraft 200 (Super King Air) series aeroplanes. This directive was introduced to address a potential safety issue with the inboard aileron hinge arms of specified models. The policy objective is to ensure that all aircraft of the specified serial numbers comply with the required safety measures to maintain airworthiness. Compliance with this directive is mandatory, with actions to be taken in accordance with Beechcraft Service Instruction No 0915, Revision 1, within 100 hours of time in service after 30 June 1978, unless already completed.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39 – 105, applies to all Beechcraft 200 (Super King Air) series aeroplanes with specified serial numbers, including both model 200 and model 200T variants. This legislation mandates adherence to the Airworthiness Directives (AD) concerning the inboard aileron hinge arms, with compliance required within 100 hours of time in service following 30 June 1978. The regulation ensures that all affected aircraft undergo action in accordance with Beechcraft Service Information No 0915, Revision 1, to maintain safety standards. The scope of this legislation is geographically broad, extending to all civil aviation activities within Australia, as regulated by the Civil Aviation Safety Authority (CASA). Subordinate instruments may further detail or expand upon these requirements, ensuring comprehensive oversight and adherence to safety standards.
Key Provisions
The Civil Aviation Regulations 1998, specifically in PART 39 - 105, outlines the Civil Aviation Safety Authority (CASA) schedule of airworthiness directives. For the Beechcraft 200 (Super King Air) Series Aeroplanes, AD/BEECH 200/23 Amendment 1 addresses the inboard aileron hinge arms (section 6/78). This directive applies to all model 200 with serial numbers (S/Nos.) BB-2 to BB-185, BB-187 to BB-202, and BB-204 to BB-20232, as well as all model 200T with S/Nos. BT-1 and BT-2. The directive mandates compliance with the action stipulated in Beechcraft Service Instruction (SI) No 0915, Revision 1. Operators must implement this action within 100 hours of time in service following 30 June 1978, unless the action has already been performed.
The Act imposes specific obligations on the parties or entities it governs. Firstly, operators of the specified Beechcraft 200 series aeroplanes must ensure that the inboard aileron hinge arms are addressed in accordance with the Beechcraft SI No 0915, Rev 1. This directive requires detailed inspection, repair, or replacement of the hinge arms to maintain the aircraft's airworthiness. The compliance timeline is critical, with the mandated actions to be completed within 100 hours of time in service following the specified date. Secondly, the aircraft maintenance records must be updated to reflect the completion of these actions, thereby ensuring ongoing compliance with airworthiness standards.
Failure to comply with the provisions outlined in AD/BEECH 200/23 Amendment 1 can result in significant consequences. Firstly, civil penalties may apply, including fines and sanctions, as stipulated by the Civil Aviation Regulations. Additionally, non-compliance could lead to the aircraft being grounded until the necessary actions are completed, which could disrupt operations and potentially endanger safety. Furthermore, criminal charges could be brought against individuals or companies that deliberately or negligently fail to adhere to the directive, resulting in fines or imprisonment. The exact penalties depend on the severity of the breach and are determined in accordance with the relevant Australian laws.