AD/CESSNA 180/40 Amdt 1 - Main Gear Wheel Assemblies

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

Legislation au F2006B05053 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 180, 182 and Wren 460 Series Aeroplanes

 

AD/CESSNA 180/40

Amdt 1


Main Gear Wheel Assemblies 11/75

 

Applicability: All models 180 fitted with McCauley D-30063 wheel assemblies.

 

Requirement: Action in accordance with Cessna SL SE74-8 dated 17 May 1974 or later revisions. Compliance:               1. 1974 Models:              Within 25 hours time in service.

2. 1973 Models: At the next main wheel disassembly after 31 December 1975 or before 31 December 1976 whichever occurs first.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, specifically Part 39, establish various safety standards and directives to ensure the safety and airworthiness of aircraft operating in Australia. One such directive, AD/CESSNA 180/40 Amendment 1, addresses the issue of main gear wheel assemblies in Cessna 180, 182, and Wren 460 Series aeroplanes. This amendment was introduced to address potential safety concerns related to the main gear wheel assemblies in specified models, requiring compliance with the standards outlined by Cessna's Service Letter SE74-8 dated 17 May 1974 or later revisions. The directive aims to ensure that the specified aircraft models meet the necessary safety standards, with particular attention to the timing and conditions under which compliance must be achieved. This legislative instrument was enacted by the Australian Government under the authority of the Civil Aviation Act 1988, with the objective of enhancing aviation safety and maintaining the airworthiness of aircraft within the Australian aviation sector.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority Schedule of Airworthiness Directives for Cessna 180, 182, and Wren 460 series aeroplanes, sets out specific requirements for maintaining the airworthiness of certain aircraft models. This legislation applies to all models of Cessna 180 aeroplanes equipped with McCauley D-30063 wheel assemblies, necessitating compliance with Cessna Service Letter SE74-8 dated 17 May 1974 or any subsequent revisions. The geographic reach of this directive is nationwide, applying across all states and territories within Australia, ensuring a uniform standard of safety and maintenance for these aircraft. Compliance with these airworthiness directives is mandatory for the specified models, with particular timelines given for 1974 and 1973 models to ensure the maintenance of safety standards. The legislation does not specify any exclusions or exemptions, but compliance is enforced through subordinate instruments that may provide additional guidelines or clarifications.

Key Provisions

The primary sections of the Civil Aviation Regulations 1998, specifically Part 39 - 105, mandate that operators of Cessna 180, 182, and Wren 460 series aeroplanes comply with certain airworthiness directives. Section AD/CESSNA 180/40 Amendment 1 focuses on the main gear wheel assemblies. For models 180 equipped with McCauley D-30063 wheel assemblies, the directive requires adherence to Cessna Service Letter SE74-8 dated 17 May 1974 or any subsequent revisions. The directive applies to all 1974 models within 25 hours of time in service and to 1973 models at the next main wheel disassembly after 31 December 1975 or before 31 December 1976, whichever comes first. Operators and owners of the specified aircraft must ensure that the maintenance and inspection of the main gear wheel assemblies are carried out in accordance with the outlined directive. This includes following the procedures detailed in the Cessna Service Letter SE74-8 or any later revisions. The directive mandates timely actions to address potential safety issues related to the main gear wheel assemblies, ensuring that these components meet the required standards to maintain the airworthiness of the aircraft. Failure to comply with the airworthiness directives can result in serious safety concerns and legal repercussions. Under the Civil Aviation Regulations 1998, non-compliance with these directives may lead to enforcement actions by the Civil Aviation Safety Authority (CASA). This could include the issuance of fines, suspension or revocation of the aircraft's certificate of airworthiness, or other regulatory penalties. The exact consequences depend on the severity of the non-compliance and the potential risk posed to flight safety. In terms of penalties, the Civil Aviation Regulations 1998 do not specify maximum financial penalties for non-compliance with airworthiness directives. However, the severity of the penalties can vary significantly. Civil penalties may include fines up to $202,000 for corporations and $40,400 for individuals, as per the applicable administrative penalty provisions. Criminal penalties may also apply, with potential imprisonment terms, depending on the nature and extent of the breach. The regulations emphasise the importance of adhering to these directives to ensure the safety of all aviation operations.

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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.