AD/L200/1 - Fire Resistant Hose Assemblies - Installation

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

Legislation au F2006B11051 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

 


Morava L200 Series Aeroplanes

 

AD/L200/1 Fire Resistant Hose Assemblies - Installation 3/63

Applicability: All models.

 

Requirement: Install approved fire-resistant hose assemblies in all flexible fuel, oil and hydraulic lines forward of the firewall.

 

Compliance: Forthwith.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, specifically within Part 39 - 105, address the need for stringent safety measures in civil aviation, including the installation of specific safety components such as fire-resistant hose assemblies. The Australian Parliament enacted these regulations to ensure that aircraft meet the highest safety standards, thereby protecting passengers and crew from potential hazards. One particular directive, AD/L200/1, targets Morava L200 Series Aeroplanes, mandating the installation of approved fire-resistant hose assemblies in all flexible fuel, oil, and hydraulic lines forward of the firewall. The directive emphasises compliance "forthwith," reflecting the policy objective to immediately implement critical safety measures to prevent fire-related incidents. This legislative instrument underscores the commitment to maintaining rigorous safety standards in the aviation industry, overseen by the Civil Aviation Safety Authority.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 – 105, pertains to the installation of fire-resistant hose assemblies for Morava L200 Series Aeroplanes, as stipulated by Airworthiness Directive AD/L200/1. This legislation applies to all models of Morava L200 Series Aeroplanes, mandating the installation of approved fire-resistant hose assemblies in all flexible fuel, oil, and hydraulic lines that are situated forward of the firewall. The directive requires compliance to be achieved forthwith, ensuring that these safety measures are implemented promptly to mitigate potential fire hazards. The scope of this regulation extends to all entities and individuals responsible for the maintenance and operation of these aircraft within the Commonwealth of Australia, thereby ensuring adherence to stringent aviation safety standards. The Act does not explicitly state any exclusions or exemptions, implying that all relevant aircraft must comply with the outlined requirements. Additionally, the application of this regulation may be further defined or extended through subordinate instruments issued by the Civil Aviation Safety Authority.

Key Provisions

The key provisions of the Civil Aviation Regulations 1998, specifically AD/L200/1 under Part 39, mandate the installation of approved fire-resistant hose assemblies in all flexible fuel, oil, and hydraulic lines forward of the firewall for Morava L200 Series Aeroplanes (section 105). This directive applies to all models within the specified aircraft series, underscoring the importance of fire safety in critical areas of the aircraft (section 3/63). Compliance with this directive is required immediately, ensuring that any existing installations are upgraded or replaced to meet the stipulated safety standards (section 3/63). To meet these requirements, operators and owners of Morava L200 Series Aeroplanes must ensure that the fire-resistant hose assemblies specified in the directive are correctly installed in the designated locations. This involves sourcing and fitting hose assemblies that have been approved by the Civil Aviation Safety Authority (CASA). Additionally, operators must ensure that all personnel involved in the installation process are adequately trained and that the installations are thoroughly inspected to confirm compliance with the regulations (section 105). Failure to comply with these provisions may result in serious consequences. Under the Civil Aviation Act 1988, non-compliance with airworthiness directives is an offence. Those found guilty of such an offence may face substantial penalties. For corporations, the maximum penalty can be up to $210,000, while for individuals, the penalty can be up to $42,000. Furthermore, ongoing non-compliance may result in the grounding of the aircraft, thereby affecting the operator's ability to conduct flights and potentially leading to further civil or criminal actions (section 105). The gravity of these penalties highlights the importance of adhering to the specified requirements to maintain the safety and airworthiness of the aircraft.

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Aviation Law
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Legislative Instrument
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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.