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 65/16
Amdt 1
Engine Mount Bolt Nuts 3/89
Applicability: Models A65-8200, 65-B80 & 65-88 with S/Nos LC-295 and subs LD-385 & subs and LP-47 and subsequent. Models 70 with S/Nos LB-1 and subsequent.
Requirement: Action in accordance with Beechcraft SI No 0396-241. Compliance: Within 25 hours’ time in service after 21 August 1970. Background: Amendment 1 consolidates Queen Air series 65 and 70 aircraft.
Overview
The Civil Aviation Regulations 1998, amended by the Civil Aviation (Airworthiness) Regulations 2006, were enacted to ensure the safety and regulation of civil aviation in Australia. This legislative instrument aims to fill the gap in maintaining aircraft airworthiness standards and ensuring the safety of operations. The regulations are overseen by the Civil Aviation Safety Authority (CASA) under the authority granted by the Civil Aviation Act 1988. The overarching policy objective of these regulations is to ensure the highest possible standards of safety in civil aviation, thereby protecting the public, aircraft, and crew. The specific directive in this legislative instrument concerns the Beechcraft 65 and 70 (Queen Air) series aeroplanes, addressing the requirement for action on engine mount bolt nuts to ensure compliance with safety standards within a specified timeframe.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority’s Schedule of Airworthiness Directives, focusing on Beechcraft 65 and 70 (Queen Air) series aeroplanes. This legislation applies to the specified models of Beechcraft 65 and 70 aircraft, including those with particular serial numbers, and mandates compliance with specific maintenance and safety directives. The directive is applicable to the geographic and jurisdictional reach of the Commonwealth of Australia, ensuring that the safety and airworthiness standards set forth are adhered to within the national airspace. The regulation requires compliance within a defined period of time in service after a specific date, with particular emphasis on the maintenance of engine mount bolt nuts as per Beechcraft Service Instruction No 0396-241. The legislation does not explicitly state any exclusions or exemptions, implying that all applicable aircraft must comply with the stipulated directives. The scope of the Act can be further extended or clarified through subordinate instruments issued by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes Airworthiness Directives (ADs) that mandate certain safety measures for particular aircraft models to ensure operational safety. For instance, AD/BEECH 65/16 Amendment 1 pertains to the engine mount bolt nuts of Beechcraft 65 and 70 (Queen Air) series aeroplanes. The directive applies to models A65-8200, 65-B80, and 65-88 with specific serial numbers, as well as models 70 from a particular serial number onward. The action required by this directive is to comply with Beechcraft Service Information (SI) No 0396-241, and this compliance must be achieved within 25 hours of time in service after 21 August 1970. The directive consolidates previous requirements for these aircraft models to streamline and enhance safety protocols.
The AD imposes specific obligations on the owners and operators of the affected aircraft. They are required to ensure that the engine mount bolt nuts are inspected, maintained, or replaced according to the specified Beechcraft SI. This involves adhering to the timeline stipulated in the AD, which mandates that the necessary actions must be completed within 25 hours of the aircraft being in service post the date mentioned in the directive. This ensures that the aircraft meet the safety standards set by the Civil Aviation Safety Authority (CASA).
Non-compliance with the requirements set out in the AD/BEECH 65/16 Amendment 1 could lead to significant legal and operational consequences. While the specific penalties are not detailed in the legislative instrument, generally, failure to comply with ADs can result in the aircraft being deemed unairworthy, leading to grounding and potential legal action. Operators may face fines, and in severe cases, criminal charges could be pursued, depending on the extent of the non-compliance and its impact on aviation safety. These penalties underscore the importance of adhering to ADs to maintain high safety standards in civil aviation.