AD/SM-205/7 - Right Main Landing Gear Control Rod - Replacement

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B07065 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


SIAI Marchetti S205 and S208 Series Aeroplanes

 

AD/SM-205/7 Right Main Landing Gear Control Rod - Replacement

Applicability: Models S205-18/R, S205-20/R and S205-22/R with S/Nos. 106 to 238. Document:  SIAI Marchetti SB 205B11.

Compliance: Before 31 March 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


3/71

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, were introduced to regulate the safety of civil aviation within Australia and to ensure compliance with international safety standards. Specifically, Part 39 of these Regulations, which includes the Airworthiness Directives, serves to address safety issues through mandatory directives that must be followed by operators of aircraft. The 1998 Regulations were established to address the need for a comprehensive legal framework that ensures the safety and airworthiness of all aircraft operating in Australian airspace, thereby protecting the public and maintaining high safety standards in civil aviation. This legislative instrument, F2006B07065, focuses on SIAI Marchetti S205 and S208 Series Aeroplanes, specifically targeting the right main landing gear control rod replacement for models S205-18/R, S205-20/R, and S205-22/R with serial numbers ranging from 106 to 238. The policy objective of this directive is to ensure that these aircraft meet necessary safety standards, particularly before 31 March 1971, as stipulated in the document SIAI Marchetti SB 205B11. The directive aims to mitigate potential risks associated with the specified component, thereby enhancing the overall safety of these aircraft in operation.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, establishes the Airworthiness Directives for certain aircraft types, including the SIAI Marchetti S205 and S208 series aeroplanes. This legislation mandates the replacement of the right main landing gear control rod for specified models, namely the S205-18/R, S205-20/R, and S205-22/R, with serial numbers ranging from 106 to 238. The directive applies to all operators of these aircraft models within the Commonwealth of Australia, ensuring adherence to safety standards set forth by the Civil Aviation Safety Authority. This regulation extends to any entity or individual operating these aircraft, thereby imposing a compliance requirement that must be met before 31 March 1971 as per the document SIAI Marchetti SB 205B11. The scope of this regulation is limited to the specified aircraft models and serial numbers, with no stated exclusions or exemptions in the provided text.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, Part 39 - 105, specifically in the context of Airworthiness Directives for the SIAI Marchetti S205 and S208 series aeroplanes, are crucial for ensuring the safety and compliance of these aircraft models. Section 39-105 mandates that for models S205-18/R, S205-20/R, and S205-22/R with serial numbers ranging from 106 to 238, compliance must be achieved before 31 March 1971. This directive is encapsulated in the document SIAI Marchetti SB 205B11, which specifies that a replacement of the right main landing gear control rod is required. This directive is crucial for maintaining the airworthiness of the specified aircraft models. The obligations and requirements imposed by this Act on the relevant parties, such as aircraft owners and operators, are stringent and clear. They must ensure that the right main landing gear control rod of the affected SIAI Marchetti S205 and S208 series aeroplanes is replaced in accordance with the specifications provided in the directive. This includes adhering to the compliance date of 31 March 1971, ensuring that all work is completed and documented appropriately. Failure to comply with these requirements can result in the aircraft being deemed unairworthy, which would prevent it from being operated legally. In terms of the consequences for breach, the Civil Aviation Regulations 1998 do not explicitly state penalties within this specific directive. However, the overarching regulations imply severe civil and criminal penalties for non-compliance. These can include substantial fines and, in more severe cases, criminal charges against the responsible parties. The potential for aircraft accidents or safety incidents resulting from non-compliance underscores the seriousness of these regulations. Therefore, it is imperative for all parties governed by these directives to take the necessary steps to ensure compliance in a timely and effective manner.

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Area of Law
Administrative Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
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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.