COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fokker F28 Series Aeroplanes
AD/F28/36 APU Enclosure Fuel Drain - Modification 11/77
Applicability: All models with S/Nos. 11003 to 11131 and 11991 to 11993. Document: 1. Fokker SB F28/49-25; or
2. RLD AD A102/77.
Compliance: Before 30 April 1978.
Overview
The Civil Aviation Regulations 1998 were enacted to regulate civil aviation activities in Australia, ensuring safety and efficiency within the industry. These regulations, which are part of a larger legislative framework aimed at maintaining high standards of airworthiness, were introduced to address the need for comprehensive and consistent rules governing civil aviation operations. The Civil Aviation Safety Authority, established under the Civil Aviation Act 1988, is the body responsible for enforcing these regulations, thereby ensuring compliance with safety directives and standards. The overarching policy objective of these regulations is to enhance the safety of civil aviation through rigorous oversight and the enforcement of airworthiness directives, such as those pertaining to the Fokker F28 Series Aeroplanes, which include modifications to the APU enclosure fuel drain to mitigate potential risks.
The specific legislative instrument F2006B09774 under the Civil Aviation Regulations 1998, pertaining to Fokker F28 Series Aeroplanes, was introduced to address the issue of the APU enclosure fuel drain. This directive mandates compliance by a specified date for certain models of the Fokker F28, aiming to prevent potential safety hazards associated with the fuel drain system. By establishing clear compliance requirements, the regulations ensure that all relevant aircraft are modified to meet the prescribed safety standards, thereby protecting both the passengers and the operational integrity of the aircraft.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, mandate the application of airworthiness directives issued by the Civil Aviation Safety Authority (CASA) to ensure the safety of aircraft operations. In this context, Airworthiness Directive (AD) F28/36 pertains to Fokker F28 Series aeroplanes, particularly those with serial numbers ranging from 11003 to 11131 and 11991 to 11993. This directive requires modifications to the Auxiliary Power Unit (APU) enclosure fuel drain to be completed by 30 April 1978. The directive applies to all Fokker F28 Series aircraft within the specified serial number range, ensuring that these aircraft meet specific safety standards as outlined in the CASA's regulatory framework. Compliance with these directives is mandatory for operators and owners of the affected aircraft to maintain their airworthiness certificates and ensure safe flight operations. This regulation underscores the Commonwealth's commitment to stringent safety measures in civil aviation.
Key Provisions
The Civil Aviation Regulations 1998 (Cth) under Part 39 - 105, specifically AD/F28/36, pertains to Fokker F28 Series aeroplanes, focusing on the Auxiliary Power Unit (APU) enclosure fuel drain modification. This directive applies to Fokker F28 aeroplanes with serial numbers ranging from 11003 to 11131 and 11991 to 11993. Compliance with this directive is mandated before 30 April 1978, as outlined in Fokker SB F28/49-25 or RLD AD A102/77. The key requirement is the modification of the APU enclosure fuel drain to ensure safety and compliance with regulatory standards.
Entities governed by these regulations must ensure that the specified Fokker F28 aeroplanes undergo the necessary modifications to the APU enclosure fuel drain. This obligation is crucial for maintaining airworthiness and adhering to the safety directives issued by the Civil Aviation Safety Authority (CASA). Compliance involves thorough inspection and, where necessary, modification of the aircraft to meet the standards set out in the referenced documents. Failure to comply with these directives could result in the aircraft being deemed non-airworthy, which in turn may prevent the aircraft from being operated legally.
Breach of these safety directives can result in significant consequences, both civil and criminal. The severity of the penalty may depend on the extent of non-compliance and the potential risk posed to aviation safety. Civil penalties can include fines, while criminal penalties may be imposed in cases of serious non-compliance, including imprisonment. The exact penalties are not specified in the text, but the overarching principle is that failure to adhere to the airworthiness directives can lead to substantial legal ramifications, impacting both the operators and the individuals responsible for compliance.