AD/RES/20 - Eon Corporation E6000 Buckle Assemblies

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B06588 Not in force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Restraint Equipment

 

AD/RES/20 Eon Corporation E6000 Buckle Assemblies 6/87

Applicability: All seat belts.

 

Requirement: 1. Inspect all seat belts to determine if they have been manufactured by the EON Corporation under TSO C22. These are to include all seat belts supplied under an airframe manufacturers part number.

 

2.    If the seat belt assembly is an EON Corporation seat belt assembly determine if an E6000 buckle is fitted. If an E6000 buckle is fitted remove the seat belt assembly and replace with another item approved in accordance with ANO 108.42.

 

3.    The seat belts removed in compliance with this Directive are to be destroyed or have the TSO markings removed or totally obliterated.

 

Note: This type of buckle assembly has a front cover plate which is pivoted at one end and is pulled at the other end through an arc to release the latch from the buckle. The E6000 buckle assemblies can be identified by the type of catch they use. Figure 1 shows the configuration of the catch and how it is located within the buckle assembly.


 

Note: FAA AD 87-04-19 refers.

 

Compliance: Prior to the issue of the next Maintenance Release after 4 June 1987 and thereafter prior to the issue of a Certificate of Airworthiness.

 

Background: This Directive is prompted by reports of a buckle assembly that pulled apart under load and of other assemblies that could be pulled apart by manipulating the latch in the buckle. This could result in lack of restraint during either flight or crash loads.

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, represent a comprehensive framework designed to ensure the safety and efficiency of civil aviation within Australia. This legislative instrument, administered by the Civil Aviation Safety Authority, is intended to address critical safety concerns by issuing Airworthiness Directives, among other provisions. One such directive, AD/RES/20 concerning Eon Corporation E6000 Buckle Assemblies, was introduced to mitigate risks associated with buckle assemblies that could fail under load or be manipulated to release the latch, potentially leading to catastrophic outcomes during flight or in the event of a crash. The overarching policy objective of this directive is to mandate the inspection and replacement of potentially defective seat belt assemblies to uphold the highest safety standards in civil aviation. The specific directive mandates the inspection of all seat belts to ascertain their manufacturer, particularly those produced by the EON Corporation under TSO C22, and the identification and replacement of any E6000 buckle assemblies with approved alternatives. Additionally, it requires the destroyed or defaced marking of any removed assemblies to prevent their reuse. This directive underscores the commitment of the Civil Aviation Safety Authority to proactive safety measures, ensuring that aircraft remain compliant with stringent safety regulations and that passengers and crew are protected against potential hazards.

Scope and Application

The Airworthiness Directives (AD) issued by the Civil Aviation Safety Authority (CASA) under the Civil Aviation Regulations 1998 are designed to ensure the ongoing safety and airworthiness of aircraft operating in Australia. Specifically, AD/RES/20 pertains to seat belts manufactured by the EON Corporation, particularly those equipped with E6000 buckle assemblies. This directive applies to all seat belts in aircraft, irrespective of the aircraft type or operator, and is mandated to be implemented across the Commonwealth of Australia. The directive requires a thorough inspection of all seat belts to ascertain their compliance with TSO C22, and if an E6000 buckle is identified, the seat belt assembly must be replaced with an approved alternative in accordance with ANO 108.42. The removed assemblies must be destroyed or otherwise rendered unusable by obliterating the TSO markings. This directive must be adhered to before the issuance of the next Maintenance Release following 4 June 1987 and prior to the issuance of a Certificate of Airworthiness thereafter. The directive aims to address safety concerns related to the buckle assembly's structural integrity, which could otherwise compromise passenger safety during flight or in the event of a crash.

Key Provisions

The Civil Aviation Regulations 1998, specifically within Part 39 - 107, detail the Airworthiness Directives (AD) issued by the Civil Aviation Safety Authority (CASA). One such directive, AD/RES/20, pertains to the E6000 buckle assemblies manufactured by the Eon Corporation (section 1). This directive applies to all seat belts, as stated in the applicability clause (section 2). The main requirement is to inspect all seat belts to ascertain if they have been manufactured by the Eon Corporation under TSO C22, including those supplied under an airframe manufacturer's part number (section 1.1). If a seat belt assembly is confirmed to be an Eon Corporation assembly, it must be further checked to determine if it is fitted with an E6000 buckle. If such a buckle is present, the seat belt assembly must be removed and replaced with another item approved under ANO 108.42 (section 1.2). The removed seat belts must then be destroyed, or have their TSO markings removed or obliterated (section 1.3). The obligations imposed by this directive require all relevant parties, including airlines and maintenance providers, to conduct thorough inspections of seat belts to identify those manufactured by the Eon Corporation and equipped with an E6000 buckle. These inspections must be carried out meticulously to ensure compliance with the directive's requirements. Additionally, once identified, the affected seat belts must be replaced with approved alternatives and the removed assemblies must be appropriately destroyed or defaced to prevent any further use. This directive is crucial for maintaining airworthiness standards and ensuring passenger safety during flights. Failure to comply with AD/RES/20 can lead to significant consequences. The primary risk is the potential for seat belts to fail under load, which could result in severe safety hazards during flights or crashes. As per the legislation, non-compliance with these directives can lead to various offences and penalties. The maximum penalties for breaching these regulations can include substantial fines and, in severe cases, imprisonment. These measures underscore the importance of adhering to the directive to maintain the highest safety standards in civil aviation.

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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.