COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 55, 58 and 95-55 (Baron) Series Aeroplanes
AD/BEECH 55/31 Fuel Vent System 6/73
Applicability: Model 58 with S/Nos. TH-1 to TH-340.
Requirement: Action in accordance with Beechcraft SI No. 0568-281, Part II. Compliance: Within 100 hours’ time in service after 31 July 1973.
Overview
The Civil Aviation Regulations 1998 were enacted by the Parliament of Australia to provide a comprehensive regulatory framework governing all aspects of civil aviation within Australia. This legislation plays a crucial role in ensuring the safety, efficiency and orderly growth of civil aviation in the country, addressing the need for a cohesive set of rules and standards to be applied uniformly across the nation. One of the key objectives of these regulations is to facilitate the operation of aircraft in a manner that protects the public, while also allowing for the safe and efficient use of the nation's airspace.
One particular aspect of these regulations, covered in PART 39 - 105, addresses Airworthiness Directives for specific aircraft models, including the Beechcraft 55, 58 and 95-55 (Baron) Series Aeroplanes. The legislation mandates compliance with certain safety directives, such as the AD/BEECH 55/31 Fuel Vent System, to ensure the continued airworthiness of these aircraft and mitigate any potential risks associated with their operation. The Civil Aviation Safety Authority (CASA) is responsible for issuing and enforcing these directives, with the overarching policy objective being the protection of public safety and the promotion of efficient air travel within Australia.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, pertains to the maintenance and safety standards for certain Beechcraft aeroplane models, namely the 55, 58, and 95-55 (Baron) series. This legislation applies to aeroplanes of the Model 58 with serial numbers ranging from TH-1 to TH-340. The directive mandates compliance with Beechcraft Service Instruction No. 0568-281, Part II, focusing on the fuel vent system. Operators of these aeroplanes must ensure that the specified maintenance action is carried out within 100 hours of the aeroplane's time in service following 31 July 1973. The regulations cover all operations within the Commonwealth of Australia and are enforced by the Civil Aviation Safety Authority. No specific exclusions, exemptions, or thresholds are mentioned in this directive; however, the application and enforcement of the regulations may be further detailed through subordinate instruments or additional civil aviation safety directives.
Key Provisions
The primary sections of AD/BEECH 55/31 (section 39-105 of the Civil Aviation Regulations 1998) pertain specifically to the fuel vent system of the Beechcraft 55, 58, and 95-55 (Baron) Series Aeroplanes. This directive applies to Model 58 aircraft with serial numbers TH-1 to TH-340. The requirement is that these aircraft must comply with the action specified in Beechcraft Service Information No. 0568-281, Part II, within a timeframe of 100 hours of their time in service after 31 July 1973.
This legislation imposes a clear obligation on the owners and operators of the specified Beechcraft models to ensure that the modifications or actions prescribed by Beechcraft SI No. 0568-281, Part II, are carried out within the stipulated period. The directive is intended to maintain or enhance the airworthiness of the aircraft by addressing a specific issue related to the fuel vent system. The compliance must be verified by the relevant authorities and documented appropriately to demonstrate adherence to the regulatory requirements.
Failure to comply with AD/BEECH 55/31 can lead to significant consequences. Although specific penalties are not detailed in the provided text, under the Civil Aviation Regulations 1998, non-compliance with airworthiness directives can result in serious civil and criminal penalties. These may include fines, suspension or revocation of aircraft certificates, and potential criminal charges against the responsible individuals, depending on the severity of the non-compliance and its impact on safety. The exact penalties would be determined by the Civil Aviation Safety Authority and may vary based on the circumstances of the breach.