AD/HILLER 12/13 Amdt 2 - Transmission Gear - Inspection

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Legislation au F2006B10345 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Hiller UH-12 Series Helicopters

 

AD/HILLER 12/13

Amdt 2

Applicability: All model UH-12E.


Transmission Gear - Inspection 6/64

 

Document: Hiller SIL No. 3036C.

 

Compliance: As detailed in the requirement document.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, under Part 39 - 105, was enacted by the Parliament of Australia to provide comprehensive regulations governing civil aviation safety, ensuring the protection of the public and the integrity of the aviation system. Specifically, the Hiller UH-12 Series Helicopters Airworthiness Directives were introduced to address identified safety issues with the model UH-12E, particularly focusing on the transmission gear inspection as outlined in the amendments. The policy objective behind these regulations is to maintain and enhance aviation safety standards by mandating specific compliance protocols and regular inspections to mitigate potential risks associated with the aircraft's operation. These directives are enforced by the Civil Aviation Safety Authority, reflecting the commitment to safeguarding lives and property within the civil aviation sector.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, which pertains to the Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies to all model UH-12E helicopters. These regulations are instrumental in ensuring that the specified aircraft comply with the prescribed standards of airworthiness, which are critical for safety in civil aviation. The geographic and jurisdictional reach of these regulations is national, as they are issued under the authority of the Commonwealth of Australia, thereby binding all operators and owners of the affected aircraft within Australia. The regulations provide explicit instructions regarding the inspection of the transmission gear as detailed in the requirement document, Hiller SIL No. 3036C, and compliance is mandatory as stipulated. There are no exclusions, exemptions, or specific thresholds mentioned within the scope of this directive, and its application extends to all relevant entities and individuals operating or maintaining these helicopters. The regulations may be further refined or expanded through subordinate instruments issued by the Civil Aviation Safety Authority.

Key Provisions

The Civil Aviation Regulations 1998 (Cth), specifically Part 39 - 105, include detailed provisions for the Hiller UH-12 Series Helicopters, with particular focus on airworthiness directives under the Civil Aviation Safety Authority (CASA) (section 39.105). This legislation mandates that all model UH-12E helicopters undergo a specific inspection of the transmission gear as outlined in AD/HILLER 12/13 Amendment 2. The directive applies universally to all UH-12E models and necessitates compliance with the inspection requirements detailed in Hiller SIL No. 3036C. The compliance document provides the necessary procedures and standards that must be adhered to during the inspection process. The obligations imposed by these regulations are clear and comprehensive. Operators of UH-12E helicopters must ensure that the transmission gear is inspected according to the specifications and standards set forth in the Hiller SIL No. 3036C document (section 39.105). This includes conducting thorough checks and maintenance as required to maintain airworthiness and safety. Operators must also maintain records of all inspections and any subsequent repairs or modifications, ensuring that these records are readily available for review by CASA inspectors or other authorised officials. Failure to comply with the airworthiness directives outlined in the Civil Aviation Regulations can result in significant consequences. Violations of these regulations may be considered offences under the Civil Aviation Act 1988 (Cth) and can lead to penalties. The maximum penalty for non-compliance with airworthiness directives can include substantial fines and, in severe cases, imprisonment. Additionally, operators may face civil actions from affected parties if their failure to comply results in accidents or other safety incidents. CASA has the authority to impose further administrative penalties, including grounding of the aircraft, until compliance is achieved.

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Aviation Law
Instrument
Legislative Instrument
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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.