AD/HU 369/31 Amdt 2 - Overrunning Clutch Assembly - Rework and Inspection

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Legislation au F2006B10693 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 369/31

Amdt 2


Overrunning Clutch Assembly - Rework and Inspection


2/79

 

Applicability: Models 369D, MD, H, HE, HM and HS.

 

Document: For models 369D and MD: Hughes SIN No. DN-9.2.

 

For models 369H, HE, HM and HS: Hughes SIN No. HN-118.2.

 

Compliance: As detailed in the requirement document.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998 were enacted to ensure the safety and efficiency of civil aviation in Australia. Part 39 - 105 of these regulations addresses airworthiness directives which are critical for maintaining the safety standards of aircraft. The legislative instrument F2006B10693, specifically AD/HU 369/31 Amendment 2, pertains to the McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters. This directive was introduced to address the specific issue of the overrunning clutch assembly in these helicopter models, mandating rework and inspection to prevent potential safety hazards. The objective of this legislation, enacted by the Parliament of the Commonwealth of Australia, is to ensure compliance with airworthiness standards, thereby protecting public safety and maintaining the integrity of civil aviation operations. The policy objective is clearly stated in the directive, which is to enhance the safety of flight operations by requiring specific maintenance actions on the overrunning clutch assembly of the affected helicopter models. The Civil Aviation Safety Authority is the enforcing body responsible for ensuring that these safety directives are adhered to, thereby safeguarding the aviation industry and the public it serves. The regulations apply to models 369D, MD, H, HE, HM and HS, as specified in the Hughes Service Information Notices (SIN) DN-9.2 for models 369D and MD, and HN-118.2 for models 369H, HE, HM and HS. Compliance with these directives is mandatory and must be carried out as detailed in the requirement document to maintain the airworthiness of the helicopters.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, apply to the McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters through the Civil Aviation Safety Authority’s Airworthiness Directive (AD) concerning the overrunning clutch assembly rework and inspection. This regulation applies to models 369D, MD, H, HE, HM, and HS and mandates compliance with the specified Hughes Serial Numbers (SIN) for each model series, such as DN-9.2 for models 369D and MD, and HN-118.2 for models 369H, HE, HM, and HS. These requirements are detailed in the associated requirement document and must be strictly adhered to ensure the airworthiness of these helicopters. The regulations operate within the jurisdiction of the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority. While the document does not explicitly mention any exclusions, exemptions, or thresholds, the specific compliance criteria outlined in the requirement document are integral to the regulatory framework. Subordinate instruments may further extend or detail the application of these regulations.

Key Provisions

The main operative sections of this legislative instrument, particularly AD/HU 369/31 Amendment 2, pertain to the overrunning clutch assembly of specific McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters, including models 369D, MD, H, HE, HM, and HS. Section (2) specifies the applicability of this directive, ensuring that it applies to the aforementioned helicopter models. For models 369D and MD, Hughes Serial Numbers (SIN) DN-9.2 are detailed, and for models 369H, HE, HM, and HS, the relevant SIN is HN-118.2. Section (3) outlines the compliance requirements, which must be met as specified in the requirement document, ensuring that the helicopter's overrunning clutch assembly is reworked and inspected to maintain airworthiness standards. The obligations imposed by this Act on the parties or entities it governs primarily involve ensuring the safety and compliance of the specified helicopter models. Operators and maintainers of these helicopters must adhere to the detailed requirements in the requirement document to rework and inspect the overrunning clutch assembly. This includes following specific procedures and standards to ensure that the helicopters meet the necessary airworthiness criteria. Non-compliance can result in significant safety risks and potential grounding of the aircraft, highlighting the importance of strict adherence to the stipulated directives. Failure to comply with the provisions of AD/HU 369/31 Amendment 2 can lead to serious civil and criminal consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce penalties for non-compliance with airworthiness directives. The severity of the penalties can vary, but they may include substantial fines and potential criminal charges. The maximum penalties for non-compliance can be significant, reflecting the critical nature of ensuring the safety of aviation operations. This underscores the importance of prompt and thorough compliance with the specified directives to avoid severe legal and financial repercussions.

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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.