AD/CESSNA 210/8 - Fuel System Placard - Installation

Overview

The Civil Aviation Regulations 1998, as amended and updated through legislative instruments such as F2006B08124, provide a comprehensive framework governing the safety and operation of civil aviation in Australia. Enacted by the Commonwealth Parliament, these regulations aim to ensure the safe and efficient use of Australian airspace, thereby protecting the public and maintaining the integrity of the national aviation system. The 1998 Regulations have been supplemented by specific airworthiness directives, such as AD/CESSNA 210/8, which address particular safety concerns for certain aircraft models. This directive, for example, targets the Cessna 210 Series Aeroplanes, requiring the installation of a fuel system placard for specified serial numbers to mitigate identified safety risks. The overarching policy objective of these regulations is to maintain the highest standards of safety and reliability within Australia’s civil aviation sector.

Scope and Application

The Civil Aviation Safety Authority (CASA) Regulations, specifically Part 39 - 105, encompass the scope and application of Airworthiness Directives (AD) concerning the Cessna 210 series aeroplanes. The particular directive AD/CESSNA 210/8 mandates the installation of a fuel system placard for certain model 210 and 210A aeroplanes, targeting a specific range of serial numbers. This regulation applies to aircraft operators and maintenance personnel responsible for ensuring compliance with airworthiness standards. The directive applies nationally, adhering to the Civil Aviation Regulations 1998, which are overseen by CASA and have a broad jurisdictional reach across Australia. The directive does not specify any exclusions or exemptions; however, the scope is limited to the specified serial numbers, ensuring that only the affected aircraft are subject to the compliance requirements. Any further clarification or extension of the directive's application is governed by subordinate instruments issued by CASA.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, specifically under PART 39 - 105, pertain to airworthiness directives for the Cessna 210 series aeroplanes. Section AD/CESSNA 210/8 addresses the installation of a fuel system placard, detailed in document SL 65-39, and requires compliance before 1 September 1971 for all model 210 and 210A with specific serial numbers ranging from 616, 618 57001 to 57575 and 210 57576 to 210 57840. The regulation ensures that the specified models of Cessna aeroplanes are fitted with a fuel system placard to comply with airworthiness standards. The obligations imposed by this directive include the installation of the required placard in the designated Cessna 210 series aeroplanes, ensuring they meet the set airworthiness criteria. Aircraft owners, operators, and maintenance personnel must ensure that the fuel system placard is correctly installed and visible as per the specifications laid out in the AD/CESSNA 210/8 directive. The regulation mandates that these modifications be carried out before the specified compliance date, underscoring the importance of adhering to the timeline. Non-compliance with the airworthiness directive AD/CESSNA 210/8 can result in significant consequences. The Civil Aviation Regulations 1998 do not explicitly state penalties in this particular directive, but generally, failure to comply with airworthiness directives can lead to serious civil and criminal penalties. These can include fines, the grounding of the aircraft, or even more severe repercussions such as the revocation of airworthiness certificates. The severity of penalties may vary depending on the extent of non-compliance and the impact on aviation safety. It is imperative for all parties involved to ensure strict adherence to the specified requirements to avoid these potential consequences.