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 65/13 Starter and Battery Relay Covers - Installation 10/69
Applicability: Models 65, and A65-8200 with S/Nos. L-1, L-2, L-6, LC-1 to LC-286. Models 65-80, 65-A80 and 65-B80 with S/Nos. LD-1 to LD-372.
Document: Beechcraft SI No. 0135-355, Rev. 1.
Compliance: Within 100 hours’ time in service after 24 October 1969.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, form a comprehensive framework for ensuring the safety and efficiency of civil aviation within Australia. One particular segment of this legislation, PART 39 - 105, focuses on the Authority Schedule of Airworthiness Directives, which mandates the implementation of specific directives to maintain the airworthiness of certain aircraft models. For instance, AD/BEECH 65/13 pertains to Beechcraft 65 and 70 (Queen Air) Series Aeroplanes, specifically addressing the installation of starter and battery relay covers. This directive was introduced to address potential safety risks associated with the aircraft's electrical systems, ensuring compliance with established safety standards. The overarching policy objective of these regulations is to safeguard the public by maintaining the highest possible standards of airworthiness and safety in civil aviation operations.
Scope and Application
The Civil Aviation Safety Authority Regulations of 1998, specifically under Part 39 - 105, mandate compliance with airworthiness directives issued by the Civil Aviation Safety Authority for various aircraft models, including the Beechcraft 65 and 70 (Queen Air) series aeroplanes. This regulation applies to specific models of these aircraft, namely Models 65, and A65-8200 with serial numbers ranging from L-1 to L-286, as well as Models 65-80, 65-A80, and 65-B80 with serial numbers LD-1 to LD-372. The directive requires the installation of starter and battery relay covers, as documented in Beechcraft SI No. 0135-355, Revision 1, to ensure compliance within 100 hours of time in service after 24 October 1969. This regulation is binding on the owners and operators of the specified aircraft models, ensuring adherence to safety standards within the Commonwealth of Australia.
Key Provisions
The Civil Aviation Regulations 1998 (Part 39 - 105) outline specific requirements for the maintenance and operation of certain aircraft models. Under AD/BEECH 65/13, these regulations mandate the installation of starter and battery relay covers on Beechcraft 65 and 70 (Queen Air) series aeroplanes. The directive applies to models 65 and A65-8200 with serial numbers L-1 to L-6 and LC-1 to LC-286, as well as models 65-80, 65-A80, and 65-B80 with serial numbers LD-1 to LD-372. Compliance must be achieved within 100 hours of time in service following the directive's issuance date of 24 October 1969, as per the document Beechcraft Service Instruction No. 0135-355, Revision 1.
The regulations impose clear obligations on the parties responsible for the maintenance of these aircraft. Specifically, they require that the starter and battery relay covers be installed according to the specifications provided by the referenced service instruction. This includes ensuring that all components are correctly fitted and that the aircraft is thoroughly inspected to verify compliance. It is the responsibility of the aircraft owner or operator to ensure that the maintenance is performed by qualified personnel and documented properly.
Failure to comply with these regulations can result in significant consequences. Civil Aviation Safety Authority (CASA) may impose penalties for non-compliance, which can include fines or other administrative actions. Additionally, operating an aircraft that does not meet the airworthiness standards set by these regulations can result in the aircraft being grounded until the required modifications are made. This not only affects the operational status of the aircraft but can also lead to delays and additional costs for the owner or operator.
The potential penalties for breaching these regulations are substantial. The Civil Aviation Regulations provide for maximum fines that can be imposed, depending on the severity and nature of the breach. For example, failure to adhere to an airworthiness directive can result in fines up to a certain amount as prescribed by the regulations. Furthermore, repeated or serious non-compliance may lead to more severe penalties, including potential criminal charges if the breach results in a safety hazard. Therefore, it is crucial for all parties involved to take these obligations seriously and ensure full compliance with the specified directives.