SAE ARP4752B
Current
Current
The latest, up-to-date edition.
Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
02-12-2013
Publisher
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1. SCOPE
2. REFERENCES
3. OVERALL HYDRAULIC SYSTEM REQUIREMENTS
4. GENERAL HYDRAULIC SYSTEM AIRWORTHINESS REQUIREMENTS
5. SPECIFIC HYDRAULIC SYSTEM AIRWORTHINESS REQUIREMENTS
6. DESIGN PRACTICES AND GUIDELINES
7. COMPONENTS
8. INSTALLATION PRACTICES AND GUIDELINES
9. NOTES
Gives guidance for the design and installation of a commercial aircraft hydraulic system to meet the applicable requirements, including the applicable airworthiness regulations that affect the hydraulic system design.
| DocumentType |
Standard
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| Pages |
58
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| PublisherName |
SAE International
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| Status |
Current
|
| Supersedes |
This SAE Aerospace Recommended Practice (ARP) provides guidance for the design and installation of a commercial aircraft hydraulic system to meet the applicable requirements, including the applicable airworthiness regulations that affect the hydraulic system design.This ARP also provides information and guidelines on the many factors that arise in the design process to provide cost effectiveness, reliability, maintainability and accepted design and installation practices.
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| SAE AIR310A | Fittings, Catalog of Flared, Flareless, Pipe Threaded, Port, Hose, and Other Type Tube Standard Connectors |
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| MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
| SAE AS5169A | FITTING, PORT PLUG AND BLEEDER |
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| SAE AS5586 | Aerospace - General Requirements for Hydraulic System Reservoirs |
| ISO 22072:2011 | Aerospace — Electrohydrostatic actuator (EHA) — Characteristics to be defined in procurement specifications |
| SAE AS1055D | Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings, and Similar System Components |
| ISO 12:1987 | Aerospace — Pipelines — Identification |
| SAE AS5440A | Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For |
| MIL-DTL-27272 Revision D:2015 | Fittings, Polytetrafluoroethylene Hose, High-Temperature, Medium-Pressure, General Specification for |
| SAE AMST7081A | Tube, Aluminum Alloy, Seamless, Round, Drawn, 6061, Aircraft Hydraulic Quality |
| SAE AS5960B | Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35 000 kPa), 400 °F (204 °C), Aircraft Hydraulic Systems |
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| SAE AS1709A | Coupling Assembly, Hydraulic Self Sealing, Quick Disconnect |
| SAE AIR797E | Hose Characteristics and Selection Chart |
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| SAE AS3132B | PIN, EXPANSION - CRES, 303, SHORT, UNS S30300 |
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| MIL-DTL-25579 Revision H:2014 | Hose Assembly, Polytetrafluoroethylene, High Temperature, Medium Pressure, General Specification for |
| SAE AIR4057B | Secondary Filters for Fluid System Reliability |
| SAE AS1241D | Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| SAE AS3121A | PLUG, EXPANSION, ALUMINUM, 2024-T4 AND 2024-T351, LONG; STD AND .010 OVERSIZE DIAMETERS (UNS A92024) |
| SAE AS3122A | PIN, EXPANSION - ALUMINUM, 2024-T4 AND 2024-T351, LONG (UNS A92024) |
| MIL F 8815 : D | FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
| ISO 7137:1995 | Aircraft — Environmental conditions and test procedures for airborne equipment |
| SAE AS1339G | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Lightweight, Hydraulic and Pneumatic |
| SAE AS1290B | Graphic Symbols for Aircraft Hydraulic and Pneumatic Systems |
| SAE ARP584C | Coiled Tubing - Corrosion Resistant Steel, Hydraulic Applications, Aerospace |
| SAE AIR4092A | Investigation of PTFE \"Melt\" Phenomenon for High Pressure Hoses |
| SAE AS 4059F : 2013 | AEROSPACE FLUID POWER - CONTAMINATION CLASSIFICATION FOR HYDRAULIC FLUIDS |
| SAE J1927_201406 | Cumulative Damage Analysis for Hydraulic Hose Assemblies |
| SAE ARP4386C | Terminology and Definitions for Aerospace Fluid Power, Actuation and Control Technologies |
| SAE AS4941B | Aerospace - General Requirements for Commercial Aircraft Hydraulic Components |
| SAE AS595D | Aerospace – Civil Type Variable Delivery, Pressure Compensated, Hydraulic Pump |
| SAE AMS4944L | Titanium Alloy Tubing, Seamless, Hydraulic 3.0Al - 2.5V Cold Worked, Stress Relieved |
| SAE AS3125C | PLUG, EXPANSION - CRES, 416 OR 416SE, LONG; STD AND .010 OVERSIZE DIAMETERS, UNS S41600/UNS S41623 |
| SAE AS3130B | PIN, EXPANSION - CRES, 303, LONG, UNS S30300 |
| SAE ARP 1383 : 2013 | AEROSPACE - IMPULSE TESTING OF HYDRAULIC COMPONENTS |
| SAE AS1227C | Hose Assembly, Convoluted Polytetrafluoroethylene, Metallic Reinforced, Low Pressure, Up to 400 °F, Aircraft |
| SAE AS604E | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Heavyweight, Hydraulic |
| SAE AS3124A | PIN, EXPANSION - ALUMINUM, 2024-T4 AND 2024-T351, SHORT, UNS A92024 |
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| SAE AS 5202 : 2005 | PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD |
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| MIL H 85800 : 0 | HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID FIBER REINFORCED, 5000 & 8000 PSI, GENERAL SPECIFICATION FOR |
| MIL-PRF-6164 Revision G:2012 | VALVE; AIRCRAFT, PNEUMATIC, HIGH-PRESSURE CHARGING |
| SAE ARP1280B | Aerospace - Application Guide for Hydraulic Power Transfer Units |
| SAE AS3131B | PLUG, EXPANSION - CRES, 303, SHORT; STD AND .010 OVERSIZE DIAMETERS, UNS S30300 |
| MIL-DTL-83296 Revision B:2009 | Fittings, Corrosion Resistant Steel, High Temperature, High Pressure (3000 PSI), Hydraulic and Pneumatic, General Specification for |
| SAE AS33611 | TUBE BEND RADII |
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