AD/CESSNA 205/3 Amdt 1 - Plastic Control Wheel

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Legislation au F2006B05209 Not in force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Cessna 205 (210-5) Series Aeroplanes

 

AD/CESSNA 205/3

Amdt 1


Plastic Control Wheel 5/69

 

Applicability: All models fitted with plastic control wheels.

 

Requirement: Action in accordance with 1 (a) Cessna SL No. 62-44 and (b) Cessna SL No. 64-8.

 

Compliance: For document 1(a) at intervals not exceeding 100 hours time in service and for document 1(b) at intervals not exceeding 500 hours time in service.

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, serve as the primary legislation governing civil aviation in Australia. This comprehensive set of regulations was designed to address the need for stringent safety standards and efficient air traffic management. One specific area addressed by the regulations is the airworthiness of aircraft, with a focus on ensuring that all civil aircraft operating in Australian airspace meet the necessary safety requirements. The Civil Aviation Safety Authority (CASA) is the body responsible for enforcing these regulations and ensuring compliance. The policy objective behind these regulations is to protect public safety by maintaining the highest standards of airworthiness and operational safety in the civil aviation sector. A particular aspect of these regulations involves the issuance of airworthiness directives for specific aircraft types, such as the Cessna 205 (210-5) Series Aeroplanes. One such directive, AD/CESSNA 205/3, pertains to the replacement of plastic control wheels on these aircraft. The directive, identified as Amendment 1, requires that all models fitted with plastic control wheels comply with specific service intervals as outlined in Cessna Service Letters No. 62-44 and No. 64-8. The directive mandates that these actions be taken at intervals not exceeding 100 hours for one component and 500 hours for another, ensuring that the aircraft remain airworthy and safe for operation.

Scope and Application

The Civil Aviation Regulations 1998, as outlined in Part 39-105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically pertain to Cessna 205 (210-5) series aeroplanes, focusing on the AD/CESSNA 205/3 Amendment 1 concerning the plastic control wheel. This legislation applies to all models of Cessna 205 aeroplanes that are fitted with a plastic control wheel. The regulation mandates actions in accordance with two Service Letters: Cessna SL No. 62-44 and Cessna SL No. 64-8, which detail the necessary compliance requirements. The compliance intervals are set at not exceeding 100 hours for document 1(a) and 500 hours for document 1(b) in terms of time in service. The scope of this legislation extends to the Commonwealth of Australia, enforcing compliance within the national jurisdiction under the oversight of the Civil Aviation Safety Authority. There are no stated exclusions or exemptions in the provided text, meaning all applicable aircraft must adhere to the specified intervals for compliance checks. Additionally, the application of this Act may be extended or restricted through subordinate instruments as deemed necessary by the regulatory authorities.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, particularly Part 39 - 105, require compliance with Airworthiness Directives (ADs) that ensure the safety of aircraft operations. Specifically, AD/CESSNA 205/3 Amendment 1, which pertains to Cessna 205 (210-5) Series Aeroplanes, mandates actions concerning the plastic control wheels on these aircraft. According to section 1 of this AD, the action required must align with two specific Service Letters issued by Cessna: SL No. 62-44 and SL No. 64-8. These service letters outline the necessary modifications or inspections that must be carried out to maintain the airworthiness of the aircraft. The obligations imposed by the Act on the parties governed by these regulations include adhering to the specified compliance intervals. For instance, for the modifications outlined in Cessna SL No. 62-44, the compliance interval is not to exceed 100 hours of time in service. Similarly, for the actions detailed in Cessna SL No. 64-8, compliance must be achieved within intervals not exceeding 500 hours of time in service. These intervals ensure that the required inspections or modifications are performed regularly to maintain the safety standards of the aircraft. Failure to comply with the requirements set out in the AD/CESSNA 205/3 Amendment 1 can result in significant legal consequences. The Civil Aviation Safety Authority (CASA) may impose various penalties for non-compliance, including fines, suspension of airworthiness certificates, or other enforcement actions. The seriousness of the breach will determine the specific penalty imposed, with potential maximum penalties varying based on the nature and severity of the violation. It is imperative for operators and maintenance personnel to adhere strictly to the directives to avoid any legal repercussions and to ensure the ongoing airworthiness of the aircraft.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.