AD/BELL 206/15 - Tail Rotor Pedal Controls Modification

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

Legislation au F2006B04465 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

 


Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters

 

AD/BELL 206/15 Tail Rotor Pedal Controls Modification 6/69

Applicability: As detailed in requirement documents. Document: Bell SB 206A-5, or Agusta SB No. BT206-6. Compliance:              Before 1 September 1971.

Background: AD/Agusta 206/8 equivalent.

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, govern the operation of aircraft within Australian airspace, with particular emphasis on safety. A specific legislative instrument within this framework, F2006B04465, addresses the safety concerns associated with the Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 series helicopters. This instrument was introduced to address identified risks in the tail rotor pedal controls of these helicopters, particularly those manufactured before 1 September 1971. The policy objective of this legislative instrument is to ensure that any safety deficiencies are rectified to maintain the highest standards of aviation safety, thereby protecting the public and all persons on board. Compliance with these directives is mandatory to prevent potential hazards that could compromise the integrity of flight operations.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies to Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters, mandating compliance with the directive AD/BELL 206/15 regarding tail rotor pedal controls. This directive applies to helicopters of the specified series that were manufactured before 1 September 1971, and compliance must be demonstrated through documentation such as Bell SB 206A-5 or Agusta SB No. BT206-6. The regulations are enforced by the Civil Aviation Safety Authority and have a national reach throughout the Commonwealth of Australia, ensuring that all operators of these helicopters within Australia adhere to the specified safety standards. While the primary focus is on ensuring the airworthiness of these helicopters, the scope of the Act does not explicitly detail exclusions or exemptions, implying that it applies broadly to all relevant aircraft within the jurisdiction. The application and enforcement of these regulations may be further defined or extended through subordinate instruments issued by the Civil Aviation Safety Authority.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, Part 39 - 105, concerning the Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters, specifically address the tail rotor pedal controls through AD/BELL 206/15. This directive mandates modifications to the tail rotor pedal controls, as specified in the Bell SB 206A-5 or Agusta SB No. BT206-6 documents, to ensure compliance before 1 September 1971. The directive is equivalent to AD/Agusta 206/8, which underscores its significance in maintaining the safety standards of these helicopter models. The Act imposes specific obligations and requirements on the operators and owners of Bell and Agusta Bell 206 Series Helicopters. Operators and owners must ensure that the tail rotor pedal controls are modified according to the specifications outlined in the Bell SB 206A-5 or Agusta SB No. BT206-6 documents. These modifications are necessary to meet the airworthiness standards set forth by the Civil Aviation Safety Authority (CASA). The modifications must be completed before the deadline of 1 September 1971, as this date marks the compliance threshold established by the directive. Failure to comply with the requirements of AD/BELL 206/15 can result in significant legal consequences. Under the Civil Aviation Act 1988, non-compliance with airworthiness directives is considered an offence. Penalties for such offences can be severe, potentially including fines and imprisonment. The specific penalties are determined by the severity of the breach and the discretion of the court, but they can be substantial, reflecting the critical importance of adhering to safety directives in aviation. Additionally, there are civil consequences for non-compliance, which may include the grounding of the affected aircraft until the required modifications are made. This can result in significant operational disruptions and financial losses for operators and owners. Furthermore, ongoing non-compliance can lead to increased scrutiny from CASA, which may result in further regulatory actions or sanctions. It is, therefore, imperative for operators and owners to strictly adhere to the requirements of AD/BELL 206/15 to avoid these potential consequences.

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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.