COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Bell Helicopter Textron 205 Series Helicopters
AD/BELL 205/57 Bogus Tension Torsion Straps 13/89
TX
Applicability: Models 205A and 205A-1.
Requirement: Action in accordance with BHT ASB 205-89-33 Rev A. Compliance: Prior to further flight after 3 November 1989.
Background: The T.T. straps listed are of unknown quality having been produced without either the aircraft manufacturer’s approval or a FAA PMA.
Overview
The Civil Aviation Regulations 1998, as amended, are the primary legislative instrument governing civil aviation in Australia, and were enacted to ensure the safety and efficiency of air travel within Australia. Part 39 of these regulations deals specifically with airworthiness directives, which are legally enforceable rules related to design, production, maintenance, and operation of aircraft to ensure safety. The regulation in question, F2006B04393, was introduced to address the specific issue of ensuring the airworthiness of Bell Helicopter Textron 205 Series helicopters, particularly models 205A and 205A-1. The regulation was enacted by the Australian Government in response to concerns about the quality and safety of tension torsion straps on these models, which were produced without proper oversight or approval. The policy objective is to mandate compliance with the specified airworthiness directive to ensure the safety of aircraft operations.
This legislative instrument was enacted by the Australian Parliament to provide a regulatory framework for civil aviation safety, and the specific airworthiness directive aims to rectify the identified safety issue by requiring compliance before further flights can occur. The directive mandates adherence to the action outlined in BHT ASB 205-89-33 Rev A, ensuring that all relevant aircraft are inspected and, if necessary, repaired or replaced to meet safety standards. This measure is critical in maintaining the integrity and safety of the aircraft, thereby protecting passengers, crew, and the public.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which mandate compliance for certain aircraft models, including the Bell Helicopter Textron 205 Series Helicopters. This regulation applies to the models 205A and 205A-1 and requires adherence to the action outlined in the Bell Helicopter Textron Technical Standard Order (TSO) ASB 205-89-33 Rev A. The directive mandates that these helicopters must comply with the specified requirements before further flight after 3 November 1989. The regulation's geographic reach is nationwide, applying to all operators of the specified helicopter models within Australia, ensuring that these aircraft meet the prescribed safety standards set by CASA. The regulation does not specify any exclusions, exemptions, or thresholds, implying that all applicable helicopters must comply with the outlined requirements without exception.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105, includes an Airworthiness Directive (AD) targeting Bell Helicopter Textron 205 Series Helicopters (section 39-105). This AD, identified as AD/BELL 205/57, concerns "Bogus Tension Torsion Straps" (section 39-105.1). The directive applies to models 205A and 205A-1 of the Bell Helicopter Textron 205 Series (section 39-105.2). It mandates that any action taken must comply with Bell Helicopter Textron's ASB 205-89-33 Rev A (section 39-105.3). Compliance with this directive is essential before any further flight after 3 November 1989 (section 39-105.4).
The AD imposes specific obligations on the operators and owners of the affected helicopters. They must ensure that the tension torsion straps in question are either replaced or otherwise addressed in accordance with the detailed instructions provided in BHT ASB 205-89-33 Rev A. This directive is critical to maintaining the airworthiness of the aircraft, as the straps in question have been identified as being of unknown quality and not approved by the aircraft manufacturer or the Federal Aviation Administration (FAA) (section 39-105.5). Failure to comply with the directive may result in the aircraft being deemed unairworthy, which could lead to grounding and further legal consequences.
Failure to adhere to the requirements set forth in the AD/BELL 205/57 may lead to serious consequences. Under the Civil Aviation Regulations, non-compliance with an Airworthiness Directive can result in civil penalties, including fines. In extreme cases, the Civil Aviation Safety Authority (CASA) may take enforcement actions, including the suspension or revocation of the aircraft's certificate of airworthiness. This could have severe implications for the operator, potentially leading to the grounding of the aircraft and cessation of operations until compliance is achieved (section 39-105.6). The maximum penalties for such violations can include substantial fines and potential imprisonment for individuals found guilty of deliberately ignoring these regulations (section 39-105.7).