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 206/26 Engine Firewall Seal - Modification 8/70 Applicability: All model 206A and AB-206A with S/Nos. referenced in requirement documents. Document: 1. Bell SB 206A-142; or
2. FAA AD 70-14-6; or
3. Agusta SB BT206-43.
Compliance: Within 300 hours time in service after 31 August 1970. Background: AD/Agusta 206/18 equivalent.
Overview
The Civil Aviation Regulations 1998, which were enacted by the Australian Parliament, form a crucial component of Australia's aviation safety framework. Specifically, Part 39 - 105 of these regulations addresses Airworthiness Directives (ADs) that are essential for ensuring the continued airworthiness of aircraft. One such directive is AD/BELL 206/26, introduced to address the need for modifying the engine firewall seal of Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters. This directive was issued to mitigate potential safety risks associated with the engine firewall seal, aiming to enhance the overall safety and reliability of these aircraft models.
The AD/BELL 206/26 directive mandates compliance within 300 hours of time in service after 31 August 1970 for all model 206A and AB-206A helicopters with specific serial numbers. This regulatory measure aligns with equivalent directives such as AD/Agusta 206/18 and FAA AD 70-14-6, ensuring a standardised approach to addressing this safety concern. The directive references specific documentation, including Bell SB 206A-142, FAA AD 70-14-6, and Agusta SB BT206-43, to guide operators in complying with the required modifications. The overarching policy objective is to maintain the highest safety standards in civil aviation by addressing potential hazards through timely and specific regulatory interventions.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to the modification of the engine firewall seal for Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters. This legislation mandates that all model 206A and AB-206A helicopters with specific serial numbers, as referenced in requirement documents, must comply with the directive. The requirement documents include Bell SB 206A-142, FAA AD 70-14-6, or Agusta SB BT206-43. The modification must be completed within 300 hours of time in service after 31 August 1970. This directive is equivalent to AD/Agusta 206/18. The legislation's geographic and jurisdictional reach is national, as it is a Commonwealth regulation, affecting all operators of the specified helicopters within Australia. There are no stated exclusions, exemptions, or thresholds in this directive, and its application may be extended or restricted through subordinate instruments as necessary.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, introduces AD/BELL 206/26, which addresses the modification of the engine firewall seal for Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters. This directive (AD/BELL 206/26) applies to all model 206A and AB-206A helicopters with serial numbers as detailed in the requirement documents. The compliance requirement is set for these aircraft to be modified within 300 hours of time in service after 31 August 1970, as detailed in either Bell SB 206A-142, FAA AD 70-14-6, or Agusta SB BT206-43.
The primary obligation imposed by this directive is the modification of the engine firewall seal. Owners or operators of affected aircraft must ensure that these modifications are made in accordance with the specified documentation. This requirement is critical to maintaining the airworthiness of the aircraft and ensuring safety standards are upheld. Compliance with this directive is mandatory and must be achieved within the stipulated timeframe, which is 300 hours of time in service after the specified date.
Failure to comply with AD/BELL 206/26 can result in serious consequences. Under the Civil Aviation Regulations, non-compliance may lead to enforcement actions by the Civil Aviation Safety Authority (CASA). The potential civil penalties for non-compliance with airworthiness directives include fines and other regulatory actions. The specific penalties are detailed within the broader regulatory framework but can be substantial, reflecting the importance of adhering to safety directives to prevent potential hazards and ensure the safety of aviation operations.