Airworthiness Directives 2004 - Revocation and Remaking - Bell Helicopter Textron 214 Series Helicopters

Overview

The Airworthiness Directives 2004 is a legislative instrument enacted by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, acting under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. This instrument was introduced to address the need for updated and consolidated airworthiness directives for specific helicopter models, ensuring that safety standards are uniformly enforced across the industry. The policy objective behind these directives is to maintain and enhance the safety of aviation operations by mandating specific actions or modifications on certain aircraft types, thereby closing any identified safety gaps. The enacting body, the Civil Aviation Safety Authority, aims to ensure that all aircraft meet the required airworthiness standards by issuing these directives. The Airworthiness Directives 2004 revokes previously issued directives and remakes them as separate instruments, as listed in the attached schedules. This process ensures that the latest safety requirements and modifications are accurately reflected and applied, maintaining the integrity and safety of the civil aviation sector. The re-made directives are identical to the latest published editions, ensuring consistency and reliability in the enforcement of aviation safety standards.

Scope and Application

The Airworthiness Directives 2004, enacted under the authority of the Civil Aviation Safety Authority (CASA), pertain to specific aircraft, namely the Bell Helicopter Textron 214 Series Helicopters, and aim to ensure their continued airworthiness. The directives apply to the entities or individuals who own, operate, or maintain these aircraft within Australia. Each directive addresses particular components of the helicopter, such as the main rotor tension-torsion strap, the main transmission upper planetary carrier, the main rotor outboard strap fitting assembly, and the tail rotor yoke, ensuring these components meet specific safety standards. The geographic reach of these directives is national, encompassing all operations within Australian territory. The application is precise, targeting the specified components and aircraft models, and does not extend to other aircraft or components not listed in the directives. The legislative instrument revokes previously issued directives and re-issues them to ensure they reflect the latest safety standards and regulatory requirements. Subordinate instruments may further refine or expand upon the directives, but the primary legislative instrument focuses on the revocation and remaking of the specified airworthiness directives for the mentioned helicopter models.

Key Provisions

The Airworthiness Directives 2004 (F2006B07759) are a legislative instrument that primarily focuses on the revocation and remaking of specific Airworthiness Directives (AD) related to certain Bell Helicopter Textron 214 Series Helicopters. The instrument, issued by David Alan Villiers as the delegate of the Civil Aviation Safety Authority (CASA), revokes and remakes several ADs, including AD/BELL 214/1, AD/BELL 214/2, AD/BELL 214/3, and AD/BELL 214/4 (Schedule 1). These ADs address specific components of the helicopters such as the Main Rotor Tension-Torsion Strap, Main Transmission Upper Planetary Carrier, Main Rotor Outboard Strap Fitting Assembly, and Tail Rotor Yoke. The operative sections of this legislative instrument mandate the revocation of the previously issued ADs listed in Schedule 1 and their simultaneous remaking in the same form as they appear in the latest published edition. This ensures that the ADs reflect the most current safety standards and regulatory requirements. By doing so, the legislation aims to maintain the airworthiness of the specified helicopter models and ensure compliance with safety regulations. The Act imposes several obligations and requirements on the parties and entities it governs. Primarily, aircraft operators and maintenance organisations must adhere to the specific ADs as re-made in this legislative instrument. This includes conducting necessary inspections, repairs, or modifications as outlined in each AD to ensure the continued airworthiness of the helicopters. Operators must keep detailed records of all actions taken in response to the ADs and ensure that all compliance measures are completed within the stipulated timeframes. Failure to comply with these requirements can lead to safety risks and potential non-compliance with aviation safety regulations. Furthermore, there are no explicit offences, penalties, or civil/criminal consequences outlined in this particular legislative instrument for non-compliance with the ADs. However, the broader framework under which CASA operates does include provisions for penalties, which can range from fines to more severe sanctions, depending on the nature and severity of the non-compliance. The Civil Aviation Safety Regulations 1998, under which this instrument is issued, provides for penalties that can include significant fines and potential criminal charges for serious breaches that result in endangering safety.