AD/CESSNA 205/10 Amdt 2 - Aft Tailcone Assembly

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Legislation au F2006B05194 In force Legislative Instrument

Legislation content

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 205/10

Amdt 2

Applicability: All 205 Series.


Aft Tailcone Assembly 11/72

 

Requirement: Action in accordance with Cessna SL SE72-29. Compliance: As detailed in the Requirement Document.

Note: Inspections carried out in accordance with the previous issue of this Directive may be taken as meeting the requirements of Cessna SL SE 72-3.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as amended through the legislative instrument F2006B05194, address the ongoing need for stringent safety measures within the aviation industry, particularly focusing on the maintenance and airworthiness of aircraft. This legislative instrument was introduced to ensure that all aircraft, including the Cessna 205 (210-5) series aeroplanes, meet specific safety standards. Enacted by the Parliament of the Commonwealth of Australia, the primary objective of this regulation is to mandate compliance with safety directives to prevent incidents and accidents, thereby safeguarding the public and enhancing the overall safety of civil aviation. The policy objective underpinning these regulations is to maintain and improve the airworthiness of aircraft through rigorous and regular inspections and maintenance actions as specified by the Civil Aviation Safety Authority.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, establish the requirements for the airworthiness directives concerning aircraft safety, including the Cessna 205 (210-5) Series Aeroplanes. This regulation applies to all aircraft within the 205 Series, mandating compliance with the aft tailcone assembly directive issued on 11/72. The directive stipulates actions in accordance with Cessna Service Letter SL SE72-29, ensuring that inspections and compliance are meticulously detailed in the Requirement Document. Furthermore, inspections conducted in alignment with the previous issue of this directive may be recognised as fulfilling the requirements of Cessna Service Letter SE 72-3. This regulatory framework is applicable nationally across the Commonwealth of Australia, governing the aviation industry to maintain the highest safety standards. While the regulations broadly apply to all entities involved in the operation of 205 Series aircraft, certain exclusions or exemptions may be specified through subordinate instruments. The overarching aim of these regulations is to ensure that the safety and airworthiness of the aircraft are consistently upheld, thereby protecting both the aviation industry and the public. The regulations are enforced by the Civil Aviation Safety Authority, ensuring compliance and safety throughout the Commonwealth.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes detailed provisions for ensuring the airworthiness of aircraft, and within this, the Civil Aviation Safety Authority (CASA) has issued Airworthiness Directives (AD) for various aircraft models. For the Cessna 205 (210-5) series aeroplanes, one such AD is AD/CESSNA 205/10 Amendment 2 (paragraph 1). This amendment applies to all aircraft in the 205 series and pertains to the aft tailcone assembly. The directive requires compliance with Cessna Service Letter SE72-29 (paragraph 2), with further details available in the Requirement Document. Importantly, inspections conducted under the previous version of this directive, Cessna SL SE 72-3, are considered to meet the current requirements (paragraph 3). Under this directive, the primary obligation is to ensure the aft tailcone assembly of the Cessna 205 series aeroplanes meets the specified standards outlined in the referenced documents. Operators of these aircraft must ensure that the necessary inspections and actions are carried out in accordance with Cessna SL SE72-29, as detailed in the Requirement Document. This includes conducting any required maintenance or modifications to the aft tailcone assembly to comply with the directive. Compliance with these standards is crucial for maintaining the airworthiness and safety of the aircraft. Failure to comply with the requirements of the AD/CESSNA 205/10 Amendment 2 may result in significant legal and safety repercussions. CASA enforces these directives to ensure that aircraft meet safety standards, and non-compliance can lead to penalties. While the specific penalties are not detailed in the legislative instrument, non-compliance with CASA directives can generally result in fines, enforcement actions, and potentially the grounding of non-compliant aircraft. Such outcomes can have severe consequences for the safety of passengers and crew, as well as the reputation and operations of the aircraft operator. Therefore, it is imperative that operators adhere strictly to the requirements of this directive.

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Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
Airworthiness Directives

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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.