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SAE AS5467

General Requirements for Hydraulic Fuse - Flow Rate

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Organization: SAE
Publication Date: 1 January 2016
Status: active
Page Count: 12
scope:

This specification establishes the design, performance, and test requirements for hydraulic flow rate fuses intended to be used for hydraulic circuit protection on aircraft.

Product Classification

Types

Type 1 Self-Resetting without manual bypass

Type 2 Self-Resetting with manual bypass

Type 3 Non Self-Resetting

Classes

Class 1500 1500 psi (10345 kPa) nominal system pressure

Class 3000 3000 psi (20690 kPa) nominal system pressure

Class 4000 4000 psi (27580 kPa) nominal system pressure

Class 5000 5000 psi (34475 kPa) nominal system pressure

Document History

SAE AS5467
January 1, 2016
General Requirements for Hydraulic Fuse - Flow Rate
This specification establishes the design, performance, and test requirements for hydraulic flow rate fuses intended to be used for hydraulic circuit protection on aircraft. Product Classification...

References

This document references:
MIL-PRF-5606 - HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE
Published by NPFC on March 5, 2018
This specification describes the characteristics and provides the requirements for a petroleum base hydraulic fluid for use in the -54 °C to +135 °C temperature range . This fluid is identified by...
This document references:
MIL-PRF-83282 - HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537
Published by NPFC on September 30, 1997
This specification covers the requirements for a synthetic hydrocarbon-base hydraulic fluid for use in the temperature range of −40° to +205°C. This hydraulic fluid is identified by NATO Code Number...
This document references:
MIL-PRF-87257D - HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE
Published by AIR FORCE on February 15, 2022
Scope. This specification describes the characteristics and provides the requirements for a synthetic hydrocarbon base hydraulic fluid for use in the -54 °C to +200 °C temperature range in aircraft...
This document references:
MIL-STD-810 - ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
Published by NPFC on January 31, 2019
Purpose. This Standard contains materiel acquisition program planning and engineering direction for considering the influences that environmental stresses have on materiel throughout all phases of...
This document references:
RTCA DO-160 - Environmental Conditions and Test Procedures for Airborne Equipment
Published by RTCA on December 16, 2014
FOREWORD This report was prepared by RTCA Special Committee 135 (SC-135) and approved by the RTCA Program Management Committee (PMC) on December 16, 2014. RTCA, Incorporated is a not-for-profit...
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