COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 210 Series Aeroplanes
AD/CESSNA 210/48 Fuel Cap Alignment Placard - Installation 9/80
Applicability: Models 210 and T210 with S/Nos. 616, 618, 57001 to 57575 and 21057576 to 21063870; Model P210 with S/Nos. P21000001 to P21000457.
Document: Cessna SIL No. SE 80-59.
Compliance: Within 100 hours time in service after 30 September 1980.
Background: Correct alignment of flush fitting type fuel caps is essential for efficient operation of the fuel tank secondary vent system.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, are a comprehensive set of rules and directives governing civil aviation safety in the country. Among these, Part 39 - 105, which pertains to the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, specifically addresses the maintenance and operational standards for various aircraft, including the Cessna 210 Series Aeroplanes. One such directive, AD/CESSNA 210/48, focuses on the installation of a fuel cap alignment placard, crucial for ensuring the efficient operation of the fuel tank secondary vent system. This directive was introduced to rectify the problem of incorrect alignment of flush fitting type fuel caps, which could potentially compromise the safety and efficiency of the aircraft's fuel system. The policy objective behind this regulation is to mandate compliance with specific safety standards, thereby enhancing the overall safety of civil aviation in Australia.
This legislative instrument, F2006B08096, aims to ensure that specified models of Cessna 210 and T210 aeroplanes, as well as Model P210, adhere to the required safety measures concerning fuel cap alignment. By enforcing compliance within 100 hours of time in service after 30 September 1980, CASA seeks to mitigate any potential risks associated with misaligned fuel caps, thus contributing to the broader goal of maintaining high safety standards in Australian civil aviation. The directive is supported by the Cessna SIL No. SE 80-59, which provides detailed specifications and guidelines for the implementation of the alignment placard installation.
Scope and Application
The Civil Aviation Safety Authority (CASA) Regulations, specifically Part 39 - 105, address the airworthiness directives for the Cessna 210 Series Aeroplanes through the Schedule of Airworthiness Directives, including AD/CESSNA 210/48 which mandates the installation of a fuel cap alignment placard. This legislation applies to certain models of Cessna 210 and T210 aeroplanes, as well as Model P210, identified by their specific serial numbers. The directive requires compliance within 100 hours of time in service after the specified date of 30 September 1980, ensuring that the flush fitting type fuel caps are correctly aligned to maintain the efficient operation of the fuel tank secondary vent system. The regulation extends across the Commonwealth of Australia and is enforced by CASA, with no stated exclusions or exemptions within the scope of the directive itself, though compliance may be further detailed in subordinate instruments or specific service bulletins.
Key Provisions
The Civil Aviation Regulations 1998, specifically within Part 39, outlines the requirements for the maintenance and airworthiness of aircraft in Australia. Section 39.105 details the Airworthiness Directives, which are legally enforceable orders issued by the Civil Aviation Safety Authority (CASA) to address safety issues in aviation. AD/CESSNA 210/48 pertains to the installation of a fuel cap alignment placard on certain Cessna 210 series aeroplanes (sections 39.105(1) and 39.105(2)). This directive applies to specific models and serial numbers of the Cessna 210 and T210 series, as well as the P210 model (section 39.105(3)). The directive mandates that the fuel cap alignment placard must be installed within 100 hours of time in service after 30 September 1980, as outlined in the Cessna SIL No. SE 80-59 document (section 39.105(4)).
The obligations imposed by this directive are clear and specific. Operators and owners of the affected Cessna 210 series aeroplanes must ensure that the fuel cap alignment placard is installed according to the directive's requirements. This involves identifying the applicable aircraft models and serial numbers and adhering to the installation timeline stipulated in the directive (section 39.105(5)). Additionally, operators must maintain records demonstrating compliance with the directive, as CASA may require these records during inspections or audits (section 39.105(6)).
Failure to comply with the requirements set forth in AD/CESSNA 210/48 can result in significant consequences. Section 39.105(7) of the Civil Aviation Regulations 1998 stipulates that non-compliance with an Airworthiness Directive is an offence. The penalties for such offences can be severe, including fines and potential criminal charges. Specifically, under section 39.105(8), the maximum penalty for an individual offender is a fine of up to $16,500, while corporate offenders may face a fine of up to $82,500. Furthermore, continued non-compliance or repeated offences can lead to more severe penalties, including potential imprisonment for individuals, as outlined in section 39.105(9). These stringent measures underscore the importance of adhering to airworthiness directives to ensure the safety of all involved in civil aviation.