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SAE International - AS4500B

HOSE ASSEMBLY, CONVOLUTED, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED CONDUCTIVE, FLARED, STRAIGHT TO 45°

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Organization: SAE International
Publication Date: 19 January 2007
Status: active

Document History

AS4500B
January 19, 2007
HOSE ASSEMBLY, CONVOLUTED, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED CONDUCTIVE, FLARED, STRAIGHT TO 45°
A description is not available for this item.

References

This document references:
AMSDTL23053/5 - Insulation Sleeving, Electrical, Heat Shrinkable, Polyolefin, Flexible, Crosslinked
Published by SAE International on July 1, 1999
A description is not available for this item.
This document references:
AS1072 - SLEEVE, HOSE ASSEMBLY, FIRE PROTECTION
Published by SAE International on January 1, 1976
This standard defines the requirements for bulk protective sleeve to provide fire resistance for aircraft hose assemblies, which will enable these assemblies to meet the requirements of ARP 1055.
This document references:
AS1294 - SLEEVE, HOSE ASSEMBLY, CHAFE GUARD, NYLON COIL
Published by SAE International on October 27, 2014
A description is not available for this item.
This document references:
AS150 - HOSE ASSEMBLY, TYPE CLASSIFICATIONS OF, BASIC PERFORMANCE AND FIRE RESISTANCE
Published by SAE International on January 1, 1994
This SAE Aerospace Standard (AS) establishes Type classification for those hose assemblies commonly used in aerospace fuel, lubricating oil, and hydraulic fluid systems.
This document references:
AS4370 - NUT - SWIVEL, WIRED ON
Published by SAE International on June 7, 1991
A description is not available for this item.
This document references:
AS4395 - FITTING END - FLARED TUBE CONNECTION, DESIGN STANDARD
Published by SAE International on October 18, 1991
A description is not available for this item.
This document references:
AS620 - HIGH TEMPERATURE HOSE ASSEMBLY, CONVOLUTED TETRAFLUOROETHYLENE-, FOR AIRCRAFT
Published by SAE International on January 1, 1980
This Aerospace Standard covers hose assemblies intended for use in aircraft high temperature fluid systems. The specified temperature range is -65°F (-54°C) to +400°F (204°C). Operating pressures are...
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