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 200/24 Fuselage Clip Installation 2/78
Applicability: All model 200 with S/Nos. BB-2, BB-6 to BB-185, BB-187 to BB-202 and BB-204 to BB-267. Model 200T with S/Nos. BT-1 and BT-2.
Requirement: Action in accordance with Beechcraft SI No 0946. Compliance: Within 100 hours time in service after 28 February 1978.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, were introduced to provide a comprehensive regulatory framework for civil aviation in the country. This legislative instrument plays a crucial role in ensuring the safety and efficiency of civil aviation operations. Part 39, in particular, pertains to airworthiness directives and safety regulations for specific aircraft types, including the Beechcraft 200 (Super King Air) series aeroplanes. One such directive, AD/BEECH 200/24, addresses the installation of fuselage clips for certain model numbers, aiming to rectify identified safety issues and maintain the airworthiness of these aircraft. The policy objective behind these regulations is to safeguard the highest standards of aviation safety, protecting both passengers and crew while fostering public confidence in the aviation industry.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, under the authority of the Civil Aviation Safety Authority, includes an Airworthiness Directive (AD) pertaining to the installation of fuselage clips on Beechcraft 200 (Super King Air) series aeroplanes. This directive applies to all Beechcraft 200 aeroplanes with specific serial numbers, as well as model 200T aeroplanes with particular serial numbers. The requirement for action in accordance with Beechcraft Service Instruction No 0946 must be met, and compliance must be achieved within 100 hours of time in service following 28 February 1978. This regulation is applicable to aircraft owners, operators, and maintenance providers who are responsible for ensuring that the specified Beechcraft 200 aeroplanes comply with the airworthiness directive. The geographic and jurisdictional reach of this regulation is national, as it is issued under the Commonwealth of Australia and applies across all states and territories. There are no stated exclusions or exemptions within the directive, and it does not specify thresholds. The application of the AD may be further detailed or extended through subordinate instruments issued by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, include the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives (ADs) concerning various aircraft. One such AD, AD/BEECH 200/24, applies to Beechcraft 200 (Super King Air) series aeroplanes. This directive mandates the installation of fuselage clips in specified serial number ranges of the Beechcraft 200 and Beechcraft 200T models. According to Section 2/78, the affected Beechcraft 200 series aeroplanes include those with serial numbers BB-2, BB-6 to BB-185, BB-187 to BB-202, and BB-204 to BB-267. For the Beechcraft 200T series, the directive applies to aeroplanes with serial numbers BT-1 and BT-2.
The AD/BEECH 200/24 requires compliance with Beechcraft Service Instruction (SI) No. 0946. Owners or operators of the specified Beechcraft 200 and 200T models must ensure the installation of the fuselage clips as outlined in this service instruction. The compliance must be achieved within 100 hours of time in service following 28 February 1978. This directive is crucial for maintaining the structural integrity and airworthiness of the specified aircraft, ensuring they meet safety standards set by CASA.
The obligations imposed by AD/BEECH 200/24 on the owners and operators of the affected Beechcraft 200 and 200T aeroplanes are clear and specific. They must adhere to the installation requirements detailed in Beechcraft SI No. 0946 and ensure these are completed within the stipulated timeframe of 100 hours of time in service after 28 February 1978. Failure to comply with these requirements could lead to significant consequences, including potential grounding of the aircraft until the required modifications are made.
In terms of penalties and consequences for non-compliance with AD/BEECH 200/24, the Civil Aviation Regulations 1998 provide for both civil and criminal penalties. Civil penalties can include fines and other monetary penalties imposed by CASA. Criminal penalties may apply in cases of serious non-compliance, potentially resulting in imprisonment. The exact penalties would depend on the severity of the breach and the discretion of the court. Ensuring compliance with AD/BEECH 200/24 is essential for maintaining the safety and airworthiness of the specified Beechcraft aeroplanes.