AD/B-2/6 - Overunning Clutch - Modification and Cockpit Placard Amendment

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Legislation au F2006B02607 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

 


Brantly B-2 Series Helicopters

 

AD/B-2/6 Overunning Clutch - Modification and Cockpit Placard Amendment


12/60

 

Applicability: All model B-2. Document: Brantly SL No. 1. Compliance:  Forthwith.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia and administered by the Civil Aviation Safety Authority, aims to address specific safety concerns within the aviation industry. One such regulation is Part 39 - 105, which includes the Schedule of Airworthiness Directives, specifically pertaining to the Brantly B-2 Series Helicopters. This legislative instrument, F2006B02607, was introduced to address issues related to the overrunning clutch and cockpit placards in the Brantly B-2 Series Helicopters. The policy objective is to ensure that all model B-2 helicopters comply with the specified modifications and placard requirements to maintain airworthiness and enhance safety. This regulation, denoted as AD/B-2/6, applies to all model B-2 helicopters and mandates compliance forthwith. It requires the modification of the overrunning clutch and the addition of a specific cockpit placard as outlined in Brantly Service Letter No. 1. The directive aims to mitigate safety risks associated with the overrunning clutch and ensure that cockpit placards provide adequate and necessary information to pilots, thereby contributing to the overall safety standards in civil aviation.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, pertains to the Airworthiness Directives that govern the safety standards for aircraft in Australia. This particular directive, AD/B-2/6, applies to all aircraft within the Brantly B-2 Series, ensuring that such aircraft meet specific safety criteria concerning the overrunning clutch modification and cockpit placard amendment. The regulation is applicable to all persons and entities involved in the operation, maintenance, and certification of Brantly B-2 Series helicopters in Australia, including operators, maintenance providers, and aviation authorities. The directive mandates compliance immediately, underscoring the importance of these safety measures. The scope of this directive extends across the Commonwealth of Australia, ensuring a uniform approach to the safety of Brantly B-2 Series helicopters nationwide. There are no exclusions or exemptions specified in the directive, meaning it applies universally to the identified aircraft models. However, the Civil Aviation Regulations 1998 may provide for further clarification or exceptions through subordinate instruments, which may detail specific conditions or exemptions in particular scenarios. This comprehensive approach ensures that all stakeholders are held to the same safety standards, thereby maintaining the integrity of civil aviation in Australia.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, contains a Schedule of Airworthiness Directives that mandates certain safety modifications and procedures for particular aircraft models, including the Brantly B-2 Series Helicopters. AD/B-2/6 pertains to the modification of the overrunning clutch and the addition of a cockpit placard. Section 12/60 of the directive states that it applies to all model B-2 helicopters (Section 12/60). Compliance with this directive is mandatory and must be achieved forthwith (Section 12/60). The obligations imposed by this directive include ensuring that all model B-2 helicopters undergo the specified modification to the overrunning clutch. This involves implementing the detailed technical procedures outlined in the directive to enhance the safety and reliability of the helicopter's clutch system. Furthermore, operators must ensure that a specific placard is installed in the cockpit, providing clear and visible information regarding the modified overrunning clutch to the flight crew (Section 12/60). These measures are essential to maintaining the airworthiness of the aircraft and ensuring the safety of all personnel on board. Failure to comply with the requirements set forth in AD/B-2/6 can result in significant legal consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce these regulations. Any breach of the directive may be subject to penalties under the Civil Aviation Act 1988. The specific penalties for non-compliance can include substantial fines, imprisonment, or both, depending on the severity of the breach and the discretion of the court. The maximum penalties for non-compliance with airworthiness directives can be severe, reflecting the critical importance of adhering to these safety measures to prevent accidents and ensure the safety of 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.