AD/BELL 212/19 Amdt 1 - External Cargo Suspension Kit - Load Restriction and Modification

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Legislation au F2006B04551 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 212 Series Helicopters

 

AD/BELL 212/19

Amdt 1


External Cargo Suspension Kit - Load Restriction and Modification


7/78

 

Applicability: All model 212 with cargo suspension kit P/N 212-706-103- 1.

 

Requirement: 1. Restrict load on external cargo hook in accordance with Bell SB No. 212-78-2, until modified in accordance with Bell SB No. 212-78-6.

 

2. Modify external cargo suspension kit P/N 212-706-103-1 in accordance with Bell SB No. 212-78-6.

 

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

 

2. Before 1 September 1978.

Overview

The Civil Aviation Regulations 1998, as amended, play a crucial role in ensuring the safety and compliance of civil aviation operations within Australia. This legislation, overseen by the Civil Aviation Safety Authority (CASA), was enacted to address the need for a robust regulatory framework that maintains the highest standards of safety in the aviation industry. A key objective of the regulations is to ensure that aircraft and aviation operations meet stringent safety requirements to protect passengers, crew, and the general public. Part 39 of these regulations, specifically the Airworthiness Directives, focuses on the mandatory compliance measures for aircraft manufacturers and operators to follow, ensuring that any identified safety issues are addressed promptly and effectively. One such directive, AD/BELL 212/19, pertains to the Bell Helicopter Textron 212 Series Helicopters. This directive was introduced to address specific safety concerns related to the external cargo suspension kit of the Bell 212 helicopters, particularly focusing on load restrictions and necessary modifications. The directive mandates that operators of Bell 212 helicopters with the identified cargo suspension kit must adhere to the specified modifications and load restrictions to prevent potential safety hazards. Compliance with these directives is mandatory to ensure the continued airworthiness of the aircraft and to uphold the stringent safety standards set forth by CASA.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105, governs the airworthiness directives for aircraft registered in Australia, ensuring the safety of the aviation industry. This particular legislative instrument pertains to the Bell Helicopter Textron 212 Series Helicopters and mandates strict compliance with the specified directives to ensure operational safety. The directives include restricting the load on the external cargo hook as outlined in Bell SB No. 212-78-2 and modifying the external cargo suspension kit as detailed in Bell SB No. 212-78-6. This legislation applies to all model 212 helicopters equipped with the cargo suspension kit P/N 212-706-103-1, necessitating compliance with the stipulated requirements before any flight using the external cargo hook and by the specified deadline of 1 September 1978. The regulatory framework extends to all helicopter operators within the Commonwealth of Australia, underscoring the importance of adhering to these safety standards to mitigate risks associated with cargo operations.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, establish a Schedule of Airworthiness Directives that govern the safety of aircraft in Australia. Specifically, AD/BELL 212/19 Amendment 1 pertains to the Bell Helicopter Textron 212 Series Helicopters, focusing on the External Cargo Suspension Kit. The applicability of this directive is limited to all model 212 helicopters equipped with the cargo suspension kit P/N 212-706-103-1 (Section 39 - 105). The main requirements outlined in this directive are to restrict the load on the external cargo hook as specified in Bell SB No. 212-78-2 until modifications are made in accordance with Bell SB No. 212-78-6, and to modify the external cargo suspension kit as per the latter service bulletin (Section 39 - 105). Entities governed by this directive are obligated to adhere to the specified requirements to ensure the safety and airworthiness of the aircraft. This involves adhering to the load restrictions on the external cargo hook until the necessary modifications have been completed, which must be done before 1 September 1978 (Section 39 - 105). Compliance is mandatory on any flight that utilises the external cargo hook, ensuring that all operations are conducted within the safety parameters established by the Civil Aviation Regulations (Section 39 - 105). Failure to comply with the provisions of AD/BELL 212/19 Amendment 1 may result in significant civil or criminal consequences. Although the specific penalties are not detailed within the text provided, non-compliance with Civil Aviation Regulations can generally lead to enforcement actions, fines, and potential grounding of the aircraft. The seriousness of the consequences underscores the importance of adhering to these safety directives to maintain the integrity and safety of civil aviation operations in Australia.

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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.