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SAE International - MA5075

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 34,500 KPA, 135 °C, BEAM SEAL, STRAIGHT TO 90°, METRIC

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Organization: SAE International
Publication Date: 28 April 2015
Status: active

Document History

MA5075
April 28, 2015
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 34,500 KPA, 135 °C, BEAM SEAL, STRAIGHT TO 90°, METRIC
A description is not available for this item.

References

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:
AS1073 - SLEEVE, HOSE ASSEMBLY, HEAT SHRINKABLE
Published by SAE International on June 1, 1968
A description is not available for this item.
This document references:
AS1291 - SLEEVE, HOSE ASSEMBLY, CHAFE GUARD, TFE OR FEP
Published by SAE International on May 1, 1973
A description is not available for this item.
This document references:
AS1293 - SLEEVE, HOSE ASSEMBLY, CHAFE GUARD, TEE COIL
Published by SAE International on October 19, 2014
A description is not available for this item.
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:
AS1723 - HOSE, POLYTETRAFLUOROETHYLENE (TFE), HIGH TEMPERATURE AND MEDIUM PRESSURE (1500 PSIG) WITH INTEGRAL SILICONE COMPOSITE FIRE PROTECTION
Published by SAE International on January 2, 2013
A description is not available for this item.
This document references:
MA4623 - Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric
Published by SAE International on August 21, 2015
This document defines the requirements for heavy-duty hose assemblies suitable for use in 21 000 kPa, 135 °C aircraft systems where rapid rate pressure pulsing and torsional/longitudinal flexing may...
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