COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 60 (Duke) Series Aeroplanes
AD/BEECH 60/29 Current Limiter Terminal Block Assemblies 10/76
Applicability: All models B60, S/Nos. P-272 thru P-307, P-309 thru P-326, P-328 thru P-330. Requirement: Action in accordance with Beechcraft SI No. 0754-350.
Note: FAA AD 76-13-05 refers.
Compliance: Within 100 hours’ time in service after 29 October 1976.
Overview
The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, were introduced to address the need for comprehensive regulation of civil aviation within Australia. These regulations are designed to ensure the safety, efficiency, and orderly growth of civil aviation in Australia. Part 39 of these regulations includes various airworthiness directives, such as AD/BEECH 60/29, which pertain specifically to the maintenance and operational standards of certain aircraft models to mitigate safety risks. This legislative instrument is overseen by the Civil Aviation Safety Authority (CASA) and aims to align with international safety standards and practices, ensuring the highest level of safety for all air operations within Australia.
The particular directive AD/BEECH 60/29 focuses on the Beechcraft 60 (Duke) series aeroplanes, mandating specific actions regarding the current limiter terminal block assemblies to address identified safety issues. The directive requires compliance within a specified timeframe to ensure that the identified risks are mitigated effectively. This measure is crucial in maintaining the integrity and safety of the aircraft in question, reflecting the overarching policy objective of the Civil Aviation Regulations to safeguard all aspects of civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, specifically PART 39 - 105, applies to all Beechcraft 60 (Duke) Series Aeroplanes with specific serial numbers, namely models B60, serial numbers P-272 through P-307, P-309 through P-326, and P-328 through P-330. These regulations are mandated by the Civil Aviation Safety Authority (CASA) and are enforced throughout the Commonwealth of Australia, ensuring that the specified aircraft meet the necessary safety standards. Compliance with AD/BEECH 60/29 is required within 100 hours of time in service after 29 October 1976, as directed by Beechcraft Service Instruction No. 0754-350. The regulations align with Federal Aviation Administration Advisory Directive 76-13-05, emphasising the importance of maintaining the current limiter terminal block assemblies to ensure airworthiness. The regulations do not specify any exclusions or exemptions but require adherence to the prescribed timeframe and actions to maintain compliance with safety standards.
Key Provisions
The Civil Aviation Regulations 1998, specifically within Part 39 - 105, pertain to airworthiness directives concerning the Beechcraft 60 (Duke) Series Aeroplanes, and are outlined in AD/BEECH 60/29. This regulation requires action regarding the current limiter terminal block assemblies, as detailed in Beechcraft Service Instruction (SI) No. 0754-350, with reference to the Federal Aviation Administration (FAA) AD 76-13-05 (Section 10/76). The directive applies to all models B60 within specified serial numbers, namely P-272 through P-307, P-309 through P-326, and P-328 through P-330. Compliance with these requirements must be achieved within 100 hours of time in service following 29 October 1976.
Under these regulations, operators of the affected Beechcraft 60 series aeroplanes must adhere to the specified maintenance and inspection procedures outlined in the referenced service instruction. This includes ensuring that the current limiter terminal block assemblies are addressed to maintain the airworthiness of the aircraft. Such compliance is critical for the safety and operational integrity of the aircraft in question. Operators must ensure that all personnel involved in the maintenance and inspection processes are adequately trained and qualified to perform the required tasks to the standards specified by the Civil Aviation Safety Authority (CASA).
Failure to comply with these airworthiness directives can lead to significant legal and operational consequences. The regulations do not explicitly detail specific penalties for non-compliance, but violations of airworthiness directives can result in serious repercussions under the broader framework of the Civil Aviation Act 1988 and related regulations. These consequences can include the grounding of the aircraft, fines, and potential criminal charges for those responsible for the oversight or execution of the maintenance and inspection activities. In extreme cases, non-compliance may lead to the suspension or revocation of the operator's licence, thereby affecting the ability to legally operate the aircraft.