COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 207 Series Aeroplanes
AD/CESSNA 207/3 Auxiliary Fuel Pump Electrical System 12/70
Applicability: All models 207 and T207 with S/Nos 207-0001 to 207-00192. Requirement: Action in accordance with Cessna SL SE70-25.
Compliance: Within 100 hours time in service after 31 December 1970.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, establish a comprehensive framework to ensure the safety and efficiency of civil aviation operations within Australia. The Regulations were introduced to address the need for stringent safety standards and regulatory oversight in the rapidly evolving aviation industry. The Regulations, as amended and updated, provide a critical safety net by imposing mandatory requirements on aircraft operations, maintenance, and airworthiness. In particular, Part 39 - 105 of the Civil Aviation Regulations addresses Airworthiness Directives, which are legally binding instructions issued by the Civil Aviation Safety Authority to ensure the continued airworthiness of specific aircraft types. These directives are crucial in mitigating safety risks and maintaining high standards of aviation safety. The policy objective of these regulations is to protect the public and aviation personnel by ensuring that all aircraft meet stringent safety and maintenance standards.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, establish the scope and application of the Civil Aviation Safety Authority's (CASA) Airworthiness Directives, which mandate safety requirements for particular types of aircraft. In this instance, AD/CESSNA 207/3 pertains to all models 207 and T207 within the Cessna 207 Series Aeroplanes with serial numbers ranging from 207-0001 to 207-00192. This directive is aimed at ensuring the safety of the auxiliary fuel pump electrical system, requiring compliance with Cessna Service Letter SE70-25. The directive applies to all relevant aircraft operators and mandates that the specified actions be taken within 100 hours of time in service after 31 December 1970. The geographic reach of this regulation is national, covering all aircraft registered and operated within Australia, thereby ensuring a uniform standard of safety across the Commonwealth. The regulations do not specify any exclusions or exemptions, and compliance is mandatory for the identified aircraft to maintain their airworthiness certification.
Key Provisions
The Civil Aviation Regulations 1998 (Cth), specifically in Part 39, Subpart 105, and under the schedule of Airworthiness Directives, addresses the maintenance and safety requirements for the Cessna 207 Series Aeroplanes. One such directive, AD/CESSNA 207/3, pertains to the auxiliary fuel pump electrical system. This directive applies to all models 207 and T207 with serial numbers ranging from 207-0001 to 207-00192 (AD/CESSNA 207/3, 12/70). According to the directive, compliance is mandatory and must be achieved by following the instructions detailed in Cessna SL SE70-25. The action required must be completed within 100 hours of time in service after 31 December 1970.
The primary obligation imposed by this directive is that the relevant parties, which include aircraft owners, operators, and maintenance personnel, must ensure that the specified maintenance action on the auxiliary fuel pump electrical system is carried out in a timely and appropriate manner. The directive is clear that the maintenance must be completed within the stipulated timeframe of 100 hours of time in service post-1970, as stated in the directive (AD/CESSNA 207/3, 12/70). Failure to adhere to this timeframe could result in the aircraft being deemed non-compliant with airworthiness standards.
In the event of non-compliance with the Airworthiness Directive, there are significant consequences. The breach of these requirements may lead to various civil and possibly criminal penalties. Under the Civil Aviation Act 1988 (Cth), non-compliance with an airworthiness directive can result in penalties, including fines and potential imprisonment. The specific penalties can vary, but for serious breaches, the maximum penalty under the Act can include fines of up to $21,000 for individuals and significantly higher amounts for corporations, alongside possible imprisonment terms that reflect the severity of the breach. It is critical for all involved parties to ensure adherence to these directives to avoid such severe consequences.