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SAE International - MA4624

HOSE ASSEMBLY, PTFE, PARA ARAMID REINFORCED, HEAVY-DUTY, 21 000 KPA, 135 ⁰C, FLARELESS, ITANIUM FITTINGS, JUMP SIZES, STRAIGHT TO STRAIGHT, METRIC

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

Document History

MA4624
April 28, 2015
HOSE ASSEMBLY, PTFE, PARA ARAMID REINFORCED, HEAVY-DUTY, 21 000 KPA, 135 ⁰C, FLARELESS, ITANIUM FITTINGS, JUMP SIZES, STRAIGHT TO STRAIGHT, 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:
MA2014 - FITTING END, FLARELESS ACDRN, METRIC
Published by SAE International on February 1, 1987
A description is not available for this item.
This document references:
MA2047 - NUT, SWIVEL, WIRED ON
Published by SAE International on March 1, 1986
A description is not available for this item.
This document references:
MA2096 - FITTING END, 24° CONE, BULKHEAD, STANDARD DIMENSIONS FOR
Published by SAE International on August 1, 1985
A description is not available for this item.
This document references:
MA2126 - Hose Assembly, Polytetrafluoroethylene (PTFE), up to 232°C and 10 500 kPa Procurement Specification, Metric (ISO/DIS 10502)
Published by SAE International on March 23, 2002
This Metric Aerospace Standard (MA) covers the requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aerospace hydraulic, fuel, and lubricating oil systems at temperatures...
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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