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AS4273B - Fire Testing of Fluid Handling Components for Aircraft Engines and Aircraft Engine Installations

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Document Number: AS4273B
Project Initiation: 2016-01-27 18:29:07.0
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Revision Number: B
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Title
Fire Testing of Fluid Handling Components for Aircraft Engines and Aircraft Engine Installations
Scope
This document establishes requirements, test procedures, and acceptance criteria for the fire testing of fluid handling components and materials used in aircraft fluid systems. It is applicable to fluid handling components other than those prescribed by AS1055 (e.g., hoses, tube assemblies, coils, and fittings). It also is applicable to materials, wiring, and components such as reservoirs, valves, gearboxes, pumps, filter assemblies, accumulators, fluid-cooled electrical/electronic components, in-flight fluid system instrumentation, hydromechanical controls, actuators, heat exchangers, and manifolds. These components may be used in fuel, lubrication, hydraulic, or pneumatic systems.
Rationale
Revise to bring in line with FAA AC 33.17.1A. Add average flame temperature & thermocouple information. Add test plan information
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