COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 150, F150, 152 & F152 Series Aeroplanes
AD/CESSNA 150/24 Beryl Aviation Filtrator Assembly 9/75
Applicability: Models 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K,
A150K, 150L, A150L series which have been modified in accordance with STC SA2219WE.
Requirement: For Cessna Models 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J,
150K, A150K, 150L and A150L Series Airplanes, remove the Beryl Aviation filtrator assembly P/N 1000-1 and install P/N B-1119-M, P/N B-1119-RN or P/N 1000-1-RM.
Note: FAA AD 75-15-08 refers.
Compliance: Within 100 hours time in service after 30 September 1975.
Overview
The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, aim to ensure the safety of civil aviation in the country. This legislation, administered by the Civil Aviation Safety Authority (CASA), was introduced to address the need for comprehensive regulations governing the airworthiness of aircraft. The regulations are designed to ensure that all civil aircraft operating in Australia meet specific safety standards, thereby protecting the public and enhancing the overall safety of the aviation industry. One particular legislative instrument, F2006B04922, focuses on issuing airworthiness directives for specific aircraft models, such as the Cessna 150, F150, 152 & F152 series aeroplanes, addressing issues like the installation of specific Beryl Aviation filtrator assemblies to enhance aircraft safety and compliance with international standards.
This specific legislative instrument, AD/CESSNA 150/24, pertains to the Beryl Aviation filtrator assembly for various Cessna 150 series aeroplanes. The policy objective here is to mandate the removal of certain Beryl Aviation filtrator assemblies and the installation of approved alternatives to ensure continued airworthiness and compliance with safety standards. The requirement must be met within 100 hours of the aircraft being in service after a specified date, reflecting CASA's commitment to maintaining stringent safety regulations and ensuring that all aircraft meet necessary safety criteria.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertain to the Civil Aviation Safety Authority’s schedule of airworthiness directives, with a focus on ensuring the safety of aircraft operations. One such directive, AD/CESSNA 150/24, addresses the Beryl Aviation filtrator assembly for various models of Cessna 150 and F150 series aeroplanes, including 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, A150K, 150L, and A150L series that have been modified in accordance with STC SA2219WE. The directive mandates the removal of the Beryl Aviation filtrator assembly P/N 1000-1 and the installation of P/N B-1119-M, P/N B-1119-RN, or P/N 1000-1-RM. Compliance with this directive must be achieved within 100 hours of time in service following 30 September 1975, ensuring that these aircraft meet specific safety standards. The regulation applies to all aircraft fitting the described models and modifications, overseen by the Civil Aviation Safety Authority within the Commonwealth of Australia, thereby ensuring the safety and airworthiness of these aircraft within Australia's airspace.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, outlines specific requirements for certain models of Cessna aeroplanes. The regulation in focus is AD/CESSNA 150/24, which pertains to the Beryl Aviation filtrator assembly for Cessna 150, F150, 152, and F152 series aeroplanes. This directive applies to models 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, A150K, 150L, and A150L series aeroplanes that have undergone modifications in accordance with STC SA2219WE (section 1).
The primary requirement under this directive is the removal of the Beryl Aviation filtrator assembly P/N 1000-1 and the installation of P/N B-1119-M, P/N B-1119-RN, or P/N 1000-1-RM (section 2). This requirement must be met within 100 hours of time in service after 30 September 1975. The directive references FAA AD 75-15-08 for additional information (section 3).
Operators and owners of the specified Cessna models are obligated to comply with this directive by ensuring the necessary modifications are made within the stipulated timeframe. Compliance involves removing the old Beryl Aviation filtrator assembly and replacing it with the specified parts to maintain airworthiness standards. Failure to comply with these requirements can result in civil and criminal consequences, including enforcement actions by the Civil Aviation Safety Authority. While specific penalties are not detailed in the excerpt, non-compliance with airworthiness directives generally can lead to severe penalties, including fines and potential grounding of the aircraft.
Breaches of airworthiness directives can result in enforcement actions by the Civil Aviation Safety Authority, which may include fines and other penalties. The seriousness of non-compliance can lead to significant repercussions, including the potential for criminal charges if the breach results in safety hazards or accidents. Therefore, it is crucial for operators and owners to adhere strictly to the requirements set forth in the AD/CESSNA 150/24 directive to ensure the continued safety and airworthiness of their aircraft.