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Fire Testing of Fluid Handling Components for Aircraft Engines and Aircraft Engine Installations
- Aerospace Standard
Published February 15, 2007 by SAE International in United States
Downloadable datasets availableAnnotation ability available
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.
This SAE Aerospace Standard (AS) presents an improved fire test procedure sequence and changes to meet the new FAA requirements specified in AC 33.17 and AC 20-135.
|Aerospace Standard||Guide for Qualification Testing of Aircraft Air Valves|
|Aerospace Standard||Fire Test Equipment for Flexible Hose and Tube Assemblies|
|Ground Vehicle Standard||Fire Prevention on Forestry Machinery|
Data Sets - Support Documents
|Unnamed Dataset 1|
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