AD/CESSNA 210/13 - Control Systems - Modification

Overview

The Civil Aviation Regulations 1998 were enacted by the Parliament of the Commonwealth of Australia to regulate civil aviation safety, ensuring the safety and efficiency of aviation activities within Australia. One of the key components of this regulation is the schedule of airworthiness directives, which includes specific directives for various aircraft models to ensure they meet safety standards. The legislative instrument F2006B08064, under PART 39 - 105, focuses on Cessna 210 Series Aeroplanes, particularly addressing modifications to control systems. This directive was introduced to address specific safety concerns identified with certain serial numbers of these aircraft models. The objective is to mandate compliance with safety standards to prevent potential risks associated with these aircraft, thereby protecting passengers, crew, and the general public. The Civil Aviation Safety Authority is the enforcing body responsible for implementing these directives, ensuring that all specified modifications are carried out within the stipulated timeframe. This regulatory approach underscores the commitment to maintaining high safety standards in civil aviation, reflecting the policy objective of minimising risks and ensuring the reliability of aircraft operations.

Scope and Application

The Civil Aviation Regulations 1998, as amended, are central to ensuring the safety and airworthiness of aircraft operating within Australia. Specifically, Part 39 - 105 of the Civil Aviation Regulations pertains to the Airworthiness Directives issued by the Civil Aviation Safety Authority. This particular legislative instrument, AD/CESSNA 210/13, applies to Cessna 210 Series Aeroplanes with specific serial numbers: all models with serial numbers from 21059138 to 21059211 and T210-0434 to T210-0454. The directive mandates modifications to the control systems of these aircraft to ensure compliance with safety standards within 100 hours of time in service after 29 April 1970. The directive is enforced under Commonwealth jurisdiction, ensuring a uniform application across the country. The scope of the directive is specifically tailored to the identified models and serial numbers, and there are no stated exclusions or exemptions within the text provided. The regulatory framework extends its reach through subordinate instruments, which provide detailed guidance and implementation specifics for the modifications required by the directive.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39, Section 105, outlines the requirements for maintaining the airworthiness of aircraft, with particular attention to the Cessna 210 Series Aeroplanes. Section AD/CESSNA 210/13 details a modification directive for control systems, applicable to all models with specific serial numbers ranging from 21059138 to 21059211 and T210-0434 to T210-0454. This directive is applicable within 100 hours of time in service after 29 April 1970. The key operative sections of this directive require that the specified Cessna 210 models undergo a modification to their control systems. This modification is intended to address identified safety concerns, ensuring the aircraft maintain the required standards of airworthiness. Compliance with this directive necessitates following the procedures outlined in the Cessna SL SE69-28 document, which provides the technical details and instructions necessary to complete the required modifications. Entities and parties governed by these regulations must ensure that the specified Cessna 210 models are inspected and, if necessary, modified according to the AD/CESSNA 210/13 directive. This includes conducting the required maintenance within the specified timeframe of 100 hours of time in service after 29 April 1970. Operators must keep detailed records of any modifications performed to demonstrate compliance with the directive. Failure to comply with the airworthiness directive could lead to serious consequences. Non-compliance may result in the aircraft being deemed unairworthy, which could lead to enforcement actions by the Civil Aviation Safety Authority (CASA). The potential penalties for breaching these regulations include fines and possible grounding of the aircraft until the required modifications are completed. The severity of the penalties reflects the importance of adhering to these directives to ensure the safety of air travel.