AD/BELL 205/41 Amdt 1 - External Cargo Suspension Kit - Load Restriction and Modification

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Legislation au F2006B04377 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 205/41

Amdt 1


External Cargo Suspension Kit - Load Restriction and Modification


7/78

 

Applicability: All model 205A-1 with external cargo suspension kit P/N 204-706-104-1.

 

Requirement: 1. Restrict load on external cargo hook in accordance with Bell SB No. 205-78-1 until modified in accordance with Bell SB No. 205-78-4.

 

2. Modify external cargo suspension kit P/N 204-706-104-1 in accordance with Bell SB No. 205-78-4.

 

Compliance: 1. On any flight utilising the external cargo hook.

 

2. Before 1 September 1978.

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, represent a comprehensive legal framework governing all aspects of civil aviation in the country. One particular part of these regulations, Part 39 - 105, addresses the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, which are critical in ensuring the safety standards of aircraft operations. This specific legislative instrument, F2006B04377, pertains to the Bell Helicopter Textron 205 Series Helicopters and mandates specific modifications to enhance safety. The problem or gap this directive addresses is the need to impose strict load restrictions and modifications on the external cargo suspension kit for certain model 205A-1 helicopters to prevent potential safety hazards. The policy objective is to ensure that all civil aviation activities within Australia comply with stringent safety standards, thus safeguarding both crew and passengers.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the safety directives issued by the Civil Aviation Safety Authority (CASA) for aircraft operation. This particular directive, AD/BELL 205/41 Amendment 1, applies to all Bell Helicopter Textron 205 Series helicopters, specifically model 205A-1 equipped with an external cargo suspension kit with part number 204-706-104-1. The regulation mandates compliance with the load restriction on the external cargo hook as outlined in Bell Service Bulletin (SB) No. 205-78-1 until the external cargo suspension kit is modified in accordance with Bell SB No. 205-78-4. Compliance with these directives is mandatory for any flight that utilises the external cargo hook and must be achieved before 1 September 1978. The directive falls under the Commonwealth of Australia's regulatory framework, ensuring that aviation safety standards are uniformly enforced across the country. This specific regulation is an extension of the overarching Civil Aviation Regulations 1998, which establish the legal requirements for aviation safety and operations within Australia.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, address the Airworthiness Directives for various aircraft, including the Bell Helicopter Textron 205 Series Helicopters. The section AD/BELL 205/41 Amendment 1, issued on 7/78, pertains to the external cargo suspension kit for Bell Helicopters model 205A-1. This directive applies to helicopters equipped with an external cargo suspension kit identified by part number 204-706-104-1. The primary requirement outlined in this directive is twofold: first, to restrict the load on the external cargo hook according to Bell Service Bulletin No. 205-78-1 until modifications are made; second, to modify the external cargo suspension kit as per Bell Service Bulletin No. 205-78-4. The obligations imposed by this Airworthiness Directive are clear and specific. Operators of the affected Bell Helicopters must adhere to the load restrictions specified in Bell SB No. 205-78-1 until the external cargo suspension kit is modified. This modification must be carried out in accordance with Bell SB No. 205-78-4. The compliance must be observed on any flight that utilises the external cargo hook, and the modifications must be completed before 1 September 1978. These requirements are designed to ensure the continued safety and airworthiness of the helicopters in question. Failure to comply with the provisions of this Airworthiness Directive could result in serious consequences. The Civil Aviation Regulations 1998 do not explicitly state the penalties for non-compliance within the text of this particular directive, but it is understood that breaches of airworthiness directives can lead to significant civil and criminal penalties. These may include fines, the grounding of the aircraft, and potential criminal charges for those responsible for the oversight or operation of the non-compliant aircraft. The severity of the penalties can vary depending on the nature and extent of the non-compliance, as well as any resulting safety incidents.

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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.