AD/HU 369/10 - Main Transmission P/N 369A5100 Series - Modification

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Legislation au F2006B10659 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

 


McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters

 

AD/HU 369/10 Main Transmission P/N 369A5100

Series - Modification

Applicability: As detailed in the requirement document. Document: Hughes SIN No. HN-56.

Compliance: Within 300 hours time in service after 1 November 1973.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


7/73

Overview

The Civil Aviation Safety Authority (CASA) has introduced Airworthiness Directives (ADs) under the Civil Aviation Act 1988 to ensure that all aircraft operating in Australia meet safety standards. This particular directive, AD/HU 369/10, targets the McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters to address safety concerns with the main transmission, specifically for parts number 369A5100 series. The directive was enacted to ensure that these helicopters maintain airworthiness and safety standards by requiring modifications within 300 hours of time in service after 1 November 1973, as detailed in Hughes SIN No. HN-56. The policy objective of these ADs is to mitigate risks associated with identified safety issues, thereby protecting the public and maintaining high safety standards within the aviation industry.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning Airworthiness Directives for McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters, pertains to the modification of the Main Transmission P/N 369A5100 series. This regulation applies to all persons and entities involved in the operation, maintenance, and modification of these specific helicopter models within the Commonwealth of Australia. The directive is aimed at ensuring that the specified component of the helicopters meets required safety standards, thereby enhancing aviation safety across the nation. The geographic reach of this Act is national, extending to all states and territories within Australia. Compliance with the directive must be achieved within 300 hours of time in service after 1 November 1973, as stipulated in the requirement document Hughes SIN No. HN-56. While the primary focus is on ensuring the specified modifications are made, the Act does not explicitly mention any exclusions, exemptions, or thresholds, though adherence to the compliance timeframe is mandatory. The application and enforcement of this directive may also be extended or refined through subordinate instruments issued by the Civil Aviation Safety Authority.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 – 105, address the airworthiness directives issued by the Civil Aviation Safety Authority (CASA) concerning specific aircraft. Under this legislative instrument, Section 39.105 sets out the Airworthiness Directives (AD) applicable to the McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters, specifically referencing the modification of the Main Transmission P/N 369A5100 Series, as detailed in Hughes Service Information Notice (SIN) No. HN-56. This directive mandates the compliance within 300 hours of time in service after 1 November 1973. Under the AD/HU 369/10, the key requirement is that the Main Transmission P/N 369A5100 Series must be modified as specified in the Hughes SIN No. HN-56. This directive is binding on all operators and owners of the specified helicopters to ensure that the necessary modifications are made to maintain the aircraft's airworthiness. Compliance with this directive is essential to avoid any potential safety risks associated with the unmodified transmission. The obligations imposed by this directive include ensuring that the modifications are performed by authorised personnel and that all work is properly documented and logged. Operators and owners must ensure that the helicopter is grounded until the modifications are completed and that the aircraft is inspected to confirm compliance with the directive. Failure to adhere to these obligations could result in severe safety implications and regulatory penalties. Should an operator or owner fail to comply with the AD/HU 369/10, they may be subject to enforcement actions by CASA. The breach of these airworthiness directives can lead to civil penalties under Section 94 of the Civil Aviation Act 1988, which includes fines up to $1,650,000 for corporations and $330,000 for individuals, depending on the severity of the non-compliance. Additionally, CASA may issue a Notice of Unauthorized Change, suspend or revoke an airworthiness certificate, or take other enforcement actions as deemed necessary to ensure compliance and safety.

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Aviation Law
Instrument
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Definitions & Interpretation
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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.