AD/CESSNA 210/12 Amdt 2 - Auxiliary Fuel Pump Electrical System - Modification

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, aim to regulate and ensure the safety of civil aviation in Australia. This legislation was introduced to address the need for consistent and stringent safety standards in the aviation industry, particularly in response to the growing number of aircraft and passengers. One specific piece of legislation within this framework is the Airworthiness Directive AD/CESSNA 210/12 Amendment 2, which applies to the Cessna 210 Series Aeroplanes with serial numbers within the specified range. This directive aims to ensure the safety of these aircraft by requiring modifications to the auxiliary fuel pump electrical system within a certain timeframe, thereby addressing potential safety issues identified in this model. The policy objective of this amendment is to maintain and enhance the airworthiness of these aircraft, ensuring the safety of passengers and crew, as well as the overall integrity of the Australian civil aviation system.

Scope and Application

The Civil Aviation Safety Authority's Airworthiness Directives, specifically AD/CESSNA 210/12 Amendment 2, pertains to the modification of the auxiliary fuel pump electrical system in Cessna 210 Series aeroplanes. This legislation applies to all models within specified serial number ranges, namely from S/Nos. 210-57841 to 210-59351 and T210-0001 to T210-0454. Compliance with the directive is mandatory for those aircraft models, requiring the modification to be completed within 100 hours of time in service following 29 August 1969. The directive is part of the broader Civil Aviation Regulations 1998, which governs civil aviation safety standards across Australia, thereby establishing a nationwide regulatory framework for ensuring aircraft airworthiness. The regulation does not explicitly state any exclusions or exemptions but requires compliance through the specified documentation, namely Cessna SL SE69-9 or Cessna SL SE70-25, ensuring that modifications are accurately and effectively implemented.

Key Provisions

The primary operative sections of the Civil Aviation Regulations 1998, specifically Part 39 - 105, address the issue of ensuring the airworthiness of aircraft through the issuance of airworthiness directives (ADs). Section 39.105 focuses on ADs concerning Cessna 210 Series Aeroplanes, with a particular emphasis on the Auxiliary Fuel Pump Electrical System as outlined in AD/CESSNA 210/12 Amendment 2 (Section 12/70). This directive applies to all models with specific serial numbers: 210-57841 to 210-59351 and T210-0001 to T210-0454. Compliance with these directives requires the aircraft to adhere to the technical specifications and modifications detailed in either the Cessna SL SE69-9 or Cessna SL SE70-25 documents (Section 1). The obligations imposed by the AD mandate that the affected Cessna 210 Series Aeroplanes must undergo necessary modifications to their Auxiliary Fuel Pump Electrical System. Compliance must be achieved within 100 hours of the aircraft's time in service following the directive's effective date of 29 August 1969. This requirement ensures that the electrical system meets the necessary safety standards to avoid potential malfunctions or failures that could compromise the aircraft's safety (Section 1). Failure to comply with the AD/CESSNA 210/12 Amendment 2 can result in severe consequences. Under Section 39.105, non-compliance with airworthiness directives can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). These actions may include penalties such as fines or legal proceedings against the aircraft operator or owner. Additionally, non-compliance can result in the aircraft being grounded until the necessary modifications are made, thereby affecting the operational status and airworthiness certification of the aircraft (Section 39.105).