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.
| Committee |
A-6A1
|
| DocumentType |
Standard
|
| Pages |
58
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| SAE AIR 5451 : 2017 | A GUIDE TO LANDING GEAR SYSTEM INTEGRATION |
| SAE ARP4945A | AEROSPACE-SOLENOID VALVE, HYDRAULIC, THREE WAY, TWO POSITION, DIRECT ACTING |
| SAE AIR 5992 : 2015 | DESCRIPTIONS OF SYSTEMS INTEGRATION TEST RIGS (IRON BIRDS) FOR AEROSPACE APPLICATIONS |
| SAE AIR 4922A : 2015 | PRIMARY FLIGHT CONTROL HYDRAULIC ACTUATION SYSTEM INTERFACE DEFINITION |
| SAE ARP994B | DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS |
| SAE ARP4378C | ACCUMULATOR, HYDRAULIC, WELDED BELLOWS, FACTORY PRE-CHARGED |
| SAE AIR 1922 : 2017 | AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
| SAE ARP584D | COILED TUBING - CORROSION RESISTANT STEEL, HYDRAULIC APPLICATIONS, AEROSPACE |
| SAE AIR 5829 : 2008 | AIR IN AIRCRAFT HYDRAULIC SYSTEMS |
| SAE AIR 5699 : 2013 | A GUIDE FOR THE DAMAGING EFFECTS OF TIRE AND WHEEL FAILURES |
| SAE ARP 5555 : 2016 | RECOMMENDATIONS FOR INSTALLATION OF SEALS IN STANDARD GLANDS |
| SAE ARP 5812 : 2017 | ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE |
| SAE AS595D | AEROSPACE - CIVIL TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED, HYDRAULIC PUMP |
| SAE AIR 6464 : 2013 | EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES |
| SAE ARP4146C | COILED TUBING - TITANIUM ALLOY, HYDRAULIC APPLICATIONS, AEROSPACE |
| SAE AIR 5696 : 2013 | AEROSPACE FLUID POWER - FAA REGULATORY HISTORY - TRANSPORT AIRPLANE HYDRAULIC SYSTEMS |
| SAE ARP 5891 : 2014 | ACHIEVING CLEANLINESS STANDARDS FOR AIRCRAFT HYDRAULIC SYSTEMS DURING MANUFACTURE |
| SAE AIR737F | AEROSPACE HYDRAULIC AND PNEUMATIC SPECIFICATIONS, STANDARDS, RECOMMENDED PRACTICES, AND INFORMATION REPORTS |
| SAE AS 5586 : 2005 | GENERAL REQUIREMENTS FOR HYDRAULIC SYSTEM RESERVOIRS |
| SAE ARP 4379 : 2016 | AEROSPACE - ACCUMULATOR, HYDRAULIC, CYLINDRICAL, PISTON SEPARATED |
| SAE AIR5992:2009(R2023) | Descriptions of Systems Integration Test Rigs (Iron Birds) for Aerospace Applications |
| SAE AS3129C : 2014(S2019) | PLUG, EXPANSION - CRES, 303, LONG; STD AND .010 OVERSIZE DIAMETERS, UNS S30300 |
| SAE AS5994A | PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY |
| SAE AS4396B | FITTING END, BULKHEAD, FLARED TUBE CONNECTION, DESIGN STANDARD |
| SAE AIR 1569 : 1993 | HANDLING AND INSTALLATION PRACTICE FOR AEROSPACE HOSE ASSEMBLIES |
| MIL V 81940 : B | VALVE, SAMPLING AND BLEED, HYDRAULIC, TYPE LI SYSTEMS |
| SAE ARP1288B | PLACARDING OF AIRCRAFT HYDRAULIC EQUIPMENT TO IDENTIFY PHOSPHATE ESTER FLUID COMPATIBILITY |
| SAE AS3123B:2009(R2014) | PLUG, EXPANSION - ALUMINUM, 2024-T4 AND 2024-T351, SHORT; STD AND .010 OVERSIZE DIAMETERS, UNS A92024 |
| SAE AS620G | HOSE ASSEMBLIES, CONVOLUTED POLYTETRAFLUOROETHYLENE METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT |
| SAE ARP603G | IMPULSE TESTING OF HYDRAULIC HOSE, TUBING, AND FITTING ASSEMBLIES |
| SAE ARP5376B | METHODS, LOCATIONS AND CRITERIA FOR SYSTEM SAMPLING AND MEASURING THE SOLID PARTICLE CONTAMINATION OF HYDRAULIC FLUIDS |
| SAE ARP 1897 : 2013 | CLAMP SELECTION AND INSTALLATION GUIDE |
| SAE AIR 1922 : 2017 | AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
| SAE ARP4146C | COILED TUBING - TITANIUM ALLOY, HYDRAULIC APPLICATIONS, AEROSPACE |
| SAE ARP4553A | AEROSPACE - ACCUMULATOR, HYDRAULIC, SELF-DISPLACING |
| SAE ARP 4379 : 2016 | AEROSPACE - ACCUMULATOR, HYDRAULIC, CYLINDRICAL, PISTON SEPARATED |
| ISO 3323:1987 | Aircraft — Hydraulic components — Marking to indicate fluid for which component is approved |
| SAE AS 3127 : 2014 | PLUG, EXPANSION - CRES, 416 OR 416SE, SHORT; STD AND .010 OVERSIZE DIAMETERS, UNS S41600/UNS S41623 |
| SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL J 5513 : C | JOINT, HYDRAULIC SWIVEL |
| SAE AS1300D | PORT - RING LOCKED FLUID CONNECTION TYPE, STANDARD DIMENSIONS FOR |
| SAE AIR310A | FITTINGS, CATALOG OF FLARED. FLARELESS, PIPE THREADED, PORT, HOSE AND OTHER TYPE TUBE STANDARD CONNECTORS |
| SAE AIR787A | FILTER ELEMENT CLEANING METHODS |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| SAE AIR 887 : 2013 | LIQUID FILTER RATINGS, PARAMETERS AND TESTS |
| SAE ARP4754A | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
| ISO 2685:1998 | Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
| MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
| SAE AS 5169 : 2009 | FITTING, PORT PLUG AND BLEEDER |
| SAE AMS5561G | STEEL, CORROSION AND HEAT-RESISTANT, WELDED AND DRAWN OR SEAMLESS AND DRAWN TUBING, 9.0MN - 20CR - 6.5NI - 0.28N, HIGH-PRESSURE HYDRAULIC |
| SAE AS 5586 : 2005 | 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, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL-DTL-27272 Revision D:2015 | Fittings, Polytetrafluoroethylene Hose, High-Temperature, Medium-Pressure, General Specification for |
| SAE AMS T 7081 : 1999 | TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN, 6061, AIRCRAFT HYDRAULIC QUALITY |
| SAE AS 5960 : 2013 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC BRAID REINFORCED, 5080 PSI (35000 KPA), 400 DEGREES F (204 DEGREES C), AIRCRAFT HYDRAULIC SYSTEMS |
| ISO 9206:2016 | Aerospace series Constant displacement hydraulic motors General specifications |
| ISO 5859:2014 | Aerospace series — Graphic symbols for schematic drawings of hydraulic and pneumatic systems and components |
| SAE AIR5005A | AEROSPACE - COMMERCIAL AIRCRAFT HYDRAULIC SYSTEMS |
| SAE AS 3126 : 2014 | PIN, EXPANSION - CRES, 416 OR 416SE, LONG, UNS S41600/UNS S41623 |
| SAE AS1709A | COUPLING ASSEMBLY, HYDRAULIC SELF SEALING, QUICK DISCONNECT |
| SAE AIR797E | HOSE CHARACTERISTICS AND SELECTION CHART |
| MIL-DTL-83298 Revision C:2009 | Hose, Conductive Polytetrafluoroethylene Tube, High Temperature, High Pressure (3000 PSI), Hydraulicand Pneumatic |
| SAE AS 5951 : 2017 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 5080 PSI (35,000 KPA), 275 DEGREES F (135 DEGREES C), AIRCRAFT HYDRAULIC SYSTEMS |
| SAE AS 3132 : 2014 | PIN, EXPANSION - CRES, 303, SHORT, UNS S30300 |
| SAE AIR4543C | AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED |
| MIL-PRF-87257 Revision C:2017 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
| SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| ISO 22089:2009 | Aerospace Hydraulic power transfer units General specifications |
| SAE AS 5550 : 2015 | FITTING ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSI |
| SAE AS 5958 : 2013 | FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPARABLE, FLUID SYSTEM FOR OPERATING PRESSURES UP TO AND INCLUDING 5080 PSI (35 000 KPA), SPECIFICATION FOR |
| SAE ARP1870A | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety(STABILIZED Aug 2012)<br> |
| SAE AS4098A | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HEAVY DUTY, METALLIC REINFORCED, 400 DEGREE F, 5000 PSI HYDRAULIC AND PNEUMATIC |
| SAE AS7997 | Motors, Aircraft Hydraulic, Constant Displacement General Specification For |
| SAE ARP994B | DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS |
| MIL-PRF-5503 Revision G:2013 | ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| SAE AS3128C : 2014(S2019) | PIN, EXPANSION - CRES, 416 OR 416SE, SHORT, UNS S41600/UNS S41623 |
| SAE AMS4945F | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3AL - 2.5V, CONTROLLED CONTRACTILE STRAIN RATIO COLD WORKED, STRESS RELIEVED |
| SAE ARP4378C | ACCUMULATOR, HYDRAULIC, WELDED BELLOWS, FACTORY PRE-CHARGED |
| ATA MSG 3 : 2011.1 | OPERATOR/MANUFACTURER SCHEDULED MAINTENANCE DEVELOPMENT |
| SAE AS18280E | FITTINGS, 24 DEGREES CONE FLARELESS, FLUID CONNECTION, 3000 PSI |
| SAE AS1896A | COUPLING ASSEMBLY, SELF-SEALING, ONE SIDE ONLY, HYDRAULIC |
| MIL-DTL-9395 Revision K:2016 | Switches, Pressure (Absolute, Gage and Differential) General Specification for |
| SAE AIR 4150 : 1993 | INSPECTION OF INSERVICE AIRBORNE ACCUMULATORS FOR CORROSION AND DAMAGE |
| MIL-DTL-27267 Revision D:2012 | Hose, Cres Wire Reinforced, Polytetrafluoroethylene, Four Hundred Fifty Degree Fahrenheit, Medium Pressure |
| SAE AMS 4946 : 2016 | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC, 3AL - 2.5V, TEXTURE CONTROLLED, COLD WORKED, STRESS RELIEVED |
| 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 AS 3121 : 2014 | PLUG, EXPANSION, ALUMINUM, 2024-T4 AND 2024-T351, LONG; STD AND .010 OVERSIZE DIAMETERS (UNS A92024) |
| SAE AS 3122 : 2014 | 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 DEGREES 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 AIR 4092 : 2013 | 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 AS 3125C : 2014(S 2019) | PLUG, EXPANSION - CRES, 416 OR 416SE, LONG; STD AND .010 OVERSIZE DIAMETERS, UNS S41600/UNS S41623(STABILIZED May 2019) |
| SAE AS 3130 : 2014 | 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 DEGREES F, AIRCRAFT |
| SAE AS604E | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, HEAVYWEIGHT, HYDRAULIC |
| SAE AS 3124 : 2014 | PIN, EXPANSION - ALUMINUM, 2024-T4 AND 2024-T351, SHORT, UNS A92024 |
| SAE ARP490F | ELECTROHYDRAULIC SERVOVALVES |
| ISO 8278:2016 | Aerospace series Hydraulic, pressure compensated, variable delivery pumps General requirements |
| SAE AS 5202 : 2005 | PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD |
| SAE AIR737F | AEROSPACE HYDRAULIC AND PNEUMATIC SPECIFICATIONS, STANDARDS, RECOMMENDED PRACTICES, AND INFORMATION REPORTS |
| 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 AS 3131 : 2014 | 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 AS 33611 : 2015 | TUBE BEND RADII |
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