AD/AC-SNOW/3 - Main Landing Gear Axle - Inspection and Modification

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Legislation au F2006B02216 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Ayres Thrush (Snow) Commander Series Aeroplanes

 

AD/AC-SNOW/3 Main Landing Gear Axle - Inspection

and Modification Applicability: Models S-2C and S-2D with a wheel tread of 100 inches. Document:               Aero Commander - Olney Division SL No. 42.

Compliance: Forthwith.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


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Overview

The Civil Aviation Regulations 1998, specifically within Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, addresses the safety and operational standards of civil aircraft in Australia. This legislative instrument was enacted by the Commonwealth of Australia and aims to ensure that specific aircraft models meet the required safety standards, thereby enhancing the overall safety of civil aviation. The Airworthiness Directive AD/AC-SNOW/3 concerning the Ayres Thrush (Snow) Commander Series Aeroplanes, models S-2C and S-2D with a wheel tread of 100 inches, is a prime example of such regulatory measures. The policy objective behind these regulations is to mandate immediate compliance with specified inspection and modification requirements to prevent potential safety hazards associated with the main landing gear axle. This directive, issued by the Civil Aviation Safety Authority, underscores the commitment to maintaining the highest safety standards within the Australian aviation sector.

Scope and Application

The Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically AD/AC-SNOW/3, pertains to the Ayres Thrush (Snow) Commander Series aeroplanes, namely models S-2C and S-2D with a wheel tread of 100 inches. This directive applies to aircraft operators, maintenance personnel, and anyone involved in the upkeep and operation of these specific aircraft models. The directive mandates immediate compliance and outlines the necessity for thorough inspection and potential modification of the main landing gear axle to ensure continued airworthiness. Geographically, this directive is enforced within the Commonwealth of Australia, thereby affecting all relevant entities and persons operating within the nation's airspace. The directive does not specify exclusions or exemptions, implying that all applicable aircraft must adhere to the outlined safety measures. Subordinate instruments may further detail the implementation and compliance requirements, ensuring the safety and regulatory standards are consistently met.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically address the Airworthiness Directives (ADs) for certain aircraft models, including the Ayres Thrush (Snow) Commander Series Aeroplanes. The directive in question, AD/AC-SNOW/3, pertains to the inspection and modification of the main landing gear axle for Models S-2C and S-2D with a wheel tread of 100 inches. This directive is documented in Aero Commander - Olney Division SL No. 42. The directive mandates compliance forthwith, meaning that the specified inspections and modifications must be completed immediately (Section 39 - 105). The main operative sections of this directive require a thorough inspection of the main landing gear axle on the specified models. The inspection must identify any signs of wear, damage, or defects that could compromise the safety of the aircraft during landing. If any issues are found, the directive requires immediate modification of the affected parts to ensure they meet the safety standards set by the Civil Aviation Safety Authority (CASA). These modifications must be carried out by certified personnel to guarantee that the repairs are effective and compliant with the regulations (Section 39 - 105). The obligations imposed by this Act on the parties governed by it, such as aircraft owners, operators, and maintenance personnel, are significant. They must ensure that the specified inspections are conducted as soon as possible, and any identified issues must be addressed promptly. Aircraft owners and operators are required to maintain detailed records of all inspections and modifications carried out in compliance with the directive. Maintenance personnel must be qualified and authorised to perform the necessary work. Failure to comply with these obligations can result in serious safety risks and potential legal consequences (Section 39 - 105). In the event of non-compliance with the requirements set out in this directive, there can be serious consequences, both civil and criminal. The Civil Aviation Safety Authority has the authority to enforce the regulations and can impose penalties for breaches. Civil penalties may include fines, and in more severe cases, criminal charges could be brought against individuals or entities responsible for the non-compliance. The maximum penalties can vary, but they are designed to ensure that the safety standards are strictly adhered to. Ignoring these requirements can lead to severe repercussions, including the grounding of the aircraft until the issues are rectified, which can have significant operational and financial impacts (Section 39 - 105).

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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.