AD/BELL 412/14 Amdt 1 - Emergency Flotation System and Squib Valve

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Legislation au F2006B04649 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Bell Helicopter Textron 412 Series Helicopters

 

AD/BELL 412/14

Amdt 1


Emergency Flotation System and Squib Valve 5/87

 

Applicability: All model 412 helicopters S/No 33001 to 33134 fitted with Emergency Flotation Kit P/N 412-706-004-101, -119, -121, -123 and -125.

 

Requirement: Action in accordance with Bell Alert Service Bulletin No. 412- 87-29 Rev. A.

 

Compliance: Within 500 hours time in service after 7 May 1987 or before 31 July 1987 whichever occurs first.

 

Note: Compliance with the previous issue of this Directive does not constitute compliance with this issue.

 

Background: The failure of an emergency flotation squib valve assembly has shown the possibility of a valve assembly failure during the pressure reservoir discharge. This Directive has been amended to conform with the latest Bell Alert Service Bulletin.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, particularly within Part 39, was enacted to establish stringent safety standards and procedures governing the operation of civil aircraft in Australia. The inclusion of AD/BELL 412/14 Amendment 1, issued in 1987, addresses a critical safety concern involving the emergency flotation system and squib valve in Bell Helicopter Textron 412 Series helicopters, specifically those with serial numbers 33001 to 33134 and equipped with certain Emergency Flotation Kit part numbers. This legislative instrument was introduced by the Commonwealth of Australia, administered by the Civil Aviation Safety Authority, to ensure that the identified helicopters meet updated safety requirements, thereby preventing potential failures that could compromise flight safety. The policy objective is to mandate compliance with the latest safety directives issued by the manufacturer, Bell, to mitigate risks associated with the emergency flotation system.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, which includes the regulations governing the maintenance and operation of specific aircraft models. In this instance, the regulations apply to all Bell Helicopter Textron 412 series helicopters with serial numbers ranging from 33001 to 33134 that are equipped with particular Emergency Flotation Kits. This regulatory framework is designed to ensure that these aircraft meet safety standards by mandating compliance with the latest Bell Alert Service Bulletin No. 412-87-29 Rev. A. The directive requires actions to be taken within 500 hours of time in service after 7 May 1987 or before 31 July 1987, whichever comes first. It is imperative to note that compliance with previous issues of this directive does not suffice; adherence to the current directive is mandatory. This regulation underscores the importance of addressing potential failures in the emergency flotation squib valve assembly to prevent incidents during pressure reservoir discharge.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, includes specific Airworthiness Directives (AD) pertaining to certain aircraft models, including the Bell Helicopter Textron 412 Series. One such directive, AD/BELL 412/14 Amendment 1, focuses on the Emergency Flotation System and Squib Valve for model 412 helicopters with serial numbers ranging from 33001 to 33134 that are equipped with specific Emergency Flotation Kit part numbers (s/n 412-706-004-101, -119, -121, -123, and -125). This directive requires compliance with Bell Alert Service Bulletin No. 412-87-29 Rev. A, ensuring that any necessary actions are taken to address potential failures within the emergency flotation system. Specifically, compliance with the directive must be achieved within 500 hours of the helicopter's time in service after 7 May 1987, or by 31 July 1987, whichever comes first. Entities governed by these regulations must adhere to strict timelines and procedural requirements to ensure safety compliance. For the Bell Helicopter Textron 412 Series, this means that operators need to review and implement the actions specified in the Bell Alert Service Bulletin No. 412-87-29 Rev. A. This likely involves inspecting, repairing, or replacing parts of the emergency flotation system to prevent potential failures of the squib valve assembly. It is crucial that these actions are completed within the stipulated timeframes to maintain the airworthiness of the aircraft and ensure the safety of all personnel involved. Failure to comply with these directives can result in significant consequences. Under the Civil Aviation Regulations 1998, non-compliance may lead to enforcement actions by the Civil Aviation Safety Authority (CASA). The specific penalties for breaches are not detailed in the provided text, but generally, the penalties for non-compliance with airworthiness directives can be severe. They may include fines, operational restrictions, or even the grounding of the aircraft until the required actions are completed. Such actions are taken to uphold the highest safety standards in the aviation industry and to mitigate any risks associated with non-compliance.

Legal classification tags

Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
Emergency Flotation System

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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.