AD/BELL 205/32 - Main Beam Cap - Inspection and Repair

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Legislation au F2006B04370 Not in force Legislative Instrument

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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 205/32 Main Beam Cap - Inspection and Repair 7/76

Applicability: All model 205 with S/Nos. 30001 to 30228. Document:  Bell Tech. Bulletin No. 205-76-10.

Compliance: Inspect within 100 hours time in service after 30 July 1976 and thereafter at intervals not exceeding 100 hours time in service.

Overview

The Civil Aviation Regulations 1998, as amended, are fundamental in governing the safety and operational standards within the Australian civil aviation sector. Enacted by the Parliament of Australia, these regulations are administered by the Civil Aviation Safety Authority (CASA) and serve to ensure that aviation activities within the country meet stringent safety and airworthiness standards. One specific area of focus is the airworthiness directives, such as the one concerning the Bell Helicopter Textron 205 Series Helicopters. This directive, identified as AD/BELL 205/32, was introduced to address specific safety concerns related to the main beam cap of these helicopters, aiming to ensure that such components are regularly inspected and maintained to prevent potential failures that could compromise flight safety. The policy objective behind these regulations is to maintain a high level of safety in civil aviation by mandating regular inspections and repairs of critical components on aircraft, thereby reducing the risk of in-flight failures and enhancing overall aviation safety.

Scope and Application

The Civil Aviation Regulations 1998, under Part 39 - 105, pertains specifically to the Airworthiness Directives for Bell Helicopter Textron 205 Series Helicopters, with a particular focus on the AD/BELL 205/32 concerning the main beam cap. This directive applies to all Bell model 205 helicopters with serial numbers ranging from 30001 to 30228. The regulation mandates a specific inspection and, if necessary, repair of the main beam cap as outlined in Bell Tech. Bulletin No. 205-76-10. Compliance requires that these inspections be conducted within 100 hours of the helicopter's time in service after 30 July 1976, and subsequently at intervals not exceeding 100 hours of time in service. This regulation is enforceable across the Commonwealth of Australia, thereby ensuring uniformity in the maintenance and safety standards of the specified helicopter models within the national airspace.

Key Provisions

The Civil Aviation Regulations 1998 (Cth) under Part 39 - 105, within the Schedule of Airworthiness Directives, specifically address the maintenance requirements for the Bell Helicopter Textron 205 Series Helicopters. One such directive, AD/BELL 205/32, pertains to the inspection and repair of the Main Beam Cap. According to this directive, all model 205 helicopters with serial numbers (S/Nos.) ranging from 30001 to 30228 are subject to these specific maintenance requirements (Section 1). For these affected helicopters, the regulations mandate an inspection of the Main Beam Cap within 100 hours of time in service following 30 July 1976. This initial inspection must be carried out as per the guidance provided in Bell Tech. Bulletin No. 205-76-10. Subsequent inspections are required at intervals not exceeding 100 hours of time in service (Section 2). These periodic inspections ensure that the Main Beam Cap remains in a safe and operational condition, thereby maintaining the overall airworthiness of the aircraft. Compliance with these regulations is crucial for the operators and maintainers of the Bell Helicopter Textron 205 Series. They are required to adhere strictly to the prescribed inspection intervals and procedures as outlined in the technical bulletin. Failure to comply with these directives can lead to serious safety implications and potential non-compliance with aviation safety standards. Operators must ensure that their maintenance protocols include the timely and thorough inspection and, if necessary, repair of the Main Beam Cap to meet the specified regulatory requirements. In the event of non-compliance with the provisions outlined in the Civil Aviation Regulations 1998, there can be significant legal and safety repercussions. While the specific offences and penalties for breaches of these regulations are not detailed within the provided text, it is understood that failure to adhere to airworthiness directives can result in enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions may include fines, operational restrictions, or other regulatory penalties. It is imperative for operators to be fully aware of and comply with these regulations to avoid any adverse consequences and to ensure the continued safety and airworthiness of their aircraft.

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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.