AD/B-2/22 - Seat Back Adjustment Wire - Removal

Overview

The Civil Aviation Safety Authority (CASA) is responsible for implementing the Civil Aviation Regulations 1998, which encompass various aspects of aviation safety in Australia. One such regulation, established to address specific safety concerns in the aviation industry, is Part 39 – 105. This particular part of the regulation, AD/B-2/22, targets the Brantly B-2 Series Helicopters, specifically addressing an issue with the seat back adjustment wire. The regulation was introduced to mitigate potential risks associated with the seat back adjustment wire part number B2-334-32, by requiring its removal from the left and right seat backs. This directive aligns with FAA AD 62-6-1 and mandates compliance without delay. The overarching policy objective is to ensure the highest safety standards are maintained in the aviation sector, thereby protecting both passengers and crew.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, mandate that the Airworthiness Directive AD/B-2/22 applies to all Brantly B-2 series helicopters that are fitted with the seat back adjustment wire P/N B2-334-32. This regulation is issued by the Civil Aviation Safety Authority and is in alignment with the FAA AD 62-6-1. The directive requires the immediate removal of the specified seat back adjustment wire from both the left and right seat backs to ensure compliance. This legislation encompasses entities operating Brantly B-2 helicopters within Australia, enforcing a safety measure that is crucial for the continued airworthiness of these aircraft. The directive applies across the Commonwealth and ensures that all operators adhere to the specified safety requirements without delay. There are no stated exclusions or exemptions in this directive, meaning that all applicable aircraft must comply immediately. The scope of this regulation is limited to the specified aircraft and issue, and any broader application would be managed through additional subordinate instruments as necessary.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically address the airworthiness directives for the Brantly B-2 Series Helicopters. The pertinent section in question is AD/B-2/22, which pertains to the seat back adjustment wire, P/N B2-334-32. This directive applies to all model B-2 helicopters that are fitted with the specified seat back adjustment wire. The requirement set forth in this directive is the removal of the seat back adjustment wire from the left and right seat backs of the aircraft, or compliance with the FAA AD 62-6-1 directive. The compliance with this directive must be carried out forthwith, ensuring that the necessary modifications are made without undue delay. The obligations imposed by this directive are clear and straightforward. Operators of the Brantly B-2 Series Helicopters must ensure that the seat back adjustment wire, P/N B2-334-32, is removed from the specified locations on the aircraft. This requirement is non-negotiable and must be met to maintain the airworthiness of the aircraft. The directive does not provide for any alternative methods of compliance, leaving no room for interpretation; the wire must be removed, or the FAA directive must be adhered to in its entirety. Failure to comply with the requirements of AD/B-2/22 can have significant consequences. While the Civil Aviation Regulations 1998 do not specify a particular offence or penalty within the directive itself, non-compliance with airworthiness directives generally can lead to severe repercussions. These can include the grounding of the aircraft, fines, and potential criminal charges for those responsible. In the context of aviation safety, non-compliance is taken very seriously, and the potential penalties reflect the importance of adhering to these safety standards. The overarching goal is to ensure that all aircraft meet the necessary safety standards to protect passengers and crew, and to maintain the integrity of the aviation system as a whole.