SAE AS 4941 : 2015
Current
The latest, up-to-date edition.
AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS
Hardcopy , PDF
English
03-09-2015
1. SCOPE
2. REFERENCES
3. REQUIREMENTS
4. QUALITY ASSURANCE REQUIREMENTS
5. ACCEPTANCE TESTS
6. QUALIFICATION TESTS
7. NOTES
APPENDIX A - PROCUREMENT SPECIFICATION FOR COMMERCIAL
AIRCRAFT HYDRAULIC COMPONENTS
APPENDIX B - COMPONENT DESIGN CHECKLIST
This SAE Aerospace Standard (AS) provides general requirements for components that are used in commercial aircraft hydraulic systems.
Committee |
A-6A1
|
DocumentType |
Revision
|
Pages |
53
|
PublisherName |
SAE International
|
Status |
Current
|
SupersededBy | |
Supersedes |
SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
SAE ARP 4493 : 2013 | AEROSPACE - DIRECT DRIVE SERVOVALVES |
SAE AS 595 : 2015 | AEROSPACE - CIVIL TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED, HYDRAULIC PUMP |
SAE ARP 994 : 2016 | DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS |
SAE ARP 1311 : 2015 | LANDING GEAR STRUCTURES AND MECHANISMS |
SAE ARP 4378 : 2017 | ACCUMULATOR, HYDRAULIC, WELDED BELLOWS, FACTORY PRE-CHARGED |
SAE ARP 5812 : 2017 | ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE |
SAE AS 5466 : 2012 | AEROSPACE - GENERAL REQUIREMENTS FOR HYDRAULIC FUSE - QUANTITY MEASURING |
14/30310862 DC : 0 | BS EN 4832 - AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION |
SAE AS 5586 : 2005 | GENERAL REQUIREMENTS FOR HYDRAULIC SYSTEM RESERVOIRS |
SAE AS 5000 : 2010 | FITTING, PLUG-IN UNION, RING LOCKED, 24 DEGREE CONE, FLUID CONNECTION, 5080 PSI (35000 KPA), SPECIFICATION FOR |
SAE ARP 6154 : 2017 | AEROSPACE FLUID POWER ELECTROHYDROSTATIC MODULE, DESIGN, PERFORMANCE AND TEST RECOMMENDATIONS |
SAE ARP 4752 : 2013 | AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS |
SAE ARP 4763 : 2017 | AEROSPACE - GENERAL REQUIREMENTS FOR HYDRAULIC RELIEF VALVES |
SAE AS 5467 : 2016 | GENERAL REQUIREMENTS FOR HYDRAULIC FUSE - FLOW RATE |
SAE ARP 4925 : 2014 | AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS |
SAE ARP 4379 : 2016 | AEROSPACE - ACCUMULATOR, HYDRAULIC, CYLINDRICAL, PISTON SEPARATED |
SAE ARP 988 : 2016 | ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |
SAE AS3129C : 2014(S2019) | PLUG, EXPANSION - CRES, 303, LONG; STD AND .010 OVERSIZE DIAMETERS, UNS S30300 |
SAE AS 4716 : 2011 | GLAND DESIGN, O-RING AND OTHER SEALS |
SAE AMS 2447 : 2012 | COATING, THERMAL SPRAY, HIGH VELOCITY OXYGEN/FUEL PROCESS |
SAE ARP 1288 : 2012 | PLACARDING OF AIRCRAFT HYDRAULIC EQUIPMENT TO IDENTIFY PHOSPHATE ESTER FLUID COMPATIBILITY |
SAE AMS 2412 : 2015 | PLATING, SILVER, COPPER STRIKE, LOW BAKE |
SAE AMS 2424 : 2010 | PLATING, NICKEL LOW-STRESSED DEPOSIT |
MIL-DTL-5002 Revision E:2011 | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
SAE AS 3123B : 2014 | PLUG, EXPANSION - ALUMINUM, 2024-T4 AND 2024-T351, SHORT; STD AND .010 OVERSIZE DIAMETERS, UNS A92024 |
SAE AMS 2404 : 2013 | PLATING, ELECTROLESS NICKEL |
SAE AS 567 : 2015 | SAFETY CABLE, SAFETY WIRE, KEY WASHERS, AND COTTER PINS FOR PROPULSION SYSTEMS, GENERAL PRACTICES FOR USE OF |
SAE AMS QQ P 416 : 2016 | PLATING, CADMIUM (ELECTRODEPOSITED) |
SAE AMS A 8625 : 2000 | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
ASTM B 339 : 2012 : REDLINE | Standard Specification for Pig Tin |
SAE AS 3127 : 2014 | PLUG, EXPANSION - CRES, 416 OR 416SE, SHORT; STD AND .010 OVERSIZE DIAMETERS, UNS S41600/UNS S41623 |
SAE AS 1300 : 2014 | PORT - RING LOCKED FLUID CONNECTION TYPE, STANDARD DIMENSIONS FOR |
MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
SAE AS 5729 : 2016 | O-RING MOLDED FROM AMS7379 (FLUOROCARBON) MATERIAL |
SAE AS 4273 : 2007 | FIRE TESTING OF FLUID HANDLING COMPONENTS FOR AIRCRAFT ENGINES AND AIRCRAFT ENGINE INSTALLATIONS |
SAE AS 3581 : 2012 | PACKING, PREFORMED - O-RING SEAL AMS 7259 |
MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
SAE AMS 2409 : 2016 | PLATING, IMMERSION TIN FOR ALUMINUM ALLOYS |
SAE AS 5169 : 2009 | FITTING, PORT PLUG AND BLEEDER |
SAE AMS 7276H : 2011 | RUBBER: FLUOROCARBON (FKM) HIGH-TEMPERATURE-FLUID RESISTANT LOW COMPRESSION SET FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
SAE AMS 2449 : 2004 | GRINDING OF HVOF SPRAYED TUNGSTEN CARBIDE COATINGS APPLIED TO HIGH STRENGTH STEELS |
NASM33547:2011 | PINS, SPRING, FUNCTIONAL LIMITATIONS OF |
SAE AS 3208 : 1976 | PACKING, PREFORMED - AMS 7276 - SEAL |
ASTM B 545 : 2013 : REDLINE | Standard Specification for Electrodeposited Coatings of Tin |
NAS 1613 : 2002 | PACKING, PREFORMED, ETHYLENE PROPYLENE RUBBER |
SAE AMS R 83485 : 2014 | RUBBER, FLUOROCARBON ELASTOMER, IMPROVED PERFORMANCE AT LOW TEMPERATURES |
SAE AMS P 83461 : 1998 | Packing, Preformed, Petroleum Hydraulic Fluid Resistant, Improved Performance at 275°F (135°C) |
SAE AS 568 : 2014 | AEROSPACE SIZE STANDARD FOR O-RINGS |
SAE AS 5857 : 2010 | GLAND DESIGN, O-RING AND OTHER ELASTOMERIC SEALS, STATIC APPLICATIONS |
SAE AMS 2448 : 2016 | APPLICATION OF TUNGSTEN CARBIDE COATINGS ON ULTRA HIGH STRENGTH STEELS HIGH VELOCITY OXYGEN/FUEL PROCESS |
MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
SAE AS 3126 : 2014 | PIN, EXPANSION - CRES, 416 OR 416SE, LONG, UNS S41600/UNS S41623 |
SAE AS 6235 : 2015 | FACE SEAL GLAND DESIGN, STATIC, O-RING AND OTHER SEALS FOR AEROSPACE HYDRAULIC AND PNEUMATIC APPLICATIONS |
SAE AS 3132 : 2014 | PIN, EXPANSION - CRES, 303, SHORT, UNS S30300 |
SAE AIR 4543 : 2017 | AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED |
MIL-PRF-87257 Revision C:2017 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
SAE AMS C 5541 : 2000 | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
SAE AMS 7287 : 2012 | FLUOROCARBON ELASTOMER (FKM) HIGH TEMPERATURE/HTS OIL RESISTANT/FUEL RESISTANT LOW COMPRESSION SET/70 TO 80 HARDNESS, LOW TEMPERATURE TG -22 DEGREES F (-30 DEGREES C) FOR SEALS IN OIL/FUEL/SPECIFIC HYDRAULIC SYSTEMS |
SAE AMS 2423 : 2015 | PLATING, NICKEL, HARD DEPOSIT |
SAE AS 83461/2 : 2016 | STRAIGHT THREAD TUBE FITTING BOSS O-RING MOLDED FROM AMS-P-83461 RUBBER |
SAE AMS 7259 : 2013 | RUBBER: FLOUROCARBON (FKM), HIGH TEMPERATURE/FLUID RESISTANT, LOW COMPRESSION SET/85 TO 95 HARDNESS, FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
SAE AMS 2413 : 2013 | PLATING, SILVER-RHODIUM |
SAE ARP1870A:1987(S2012) | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety(STABILIZED Aug 2012)<br> |
SAE ARP 4727 : 2004(S2013) | GLAND DESIGN, COMPUTATION OF SEAL SQUEEZE AND GLAND VOLUME |
SAE ARP 5935 : 2013 | USE OF HVOF THERMAL SPRAY COATINGS FOR HARD CHROME REPLACEMENT IN LANDING GEAR APPLICATIONS |
MIL-STD-276 Revision A:1992 | IMPREGNATION OF POROUS METAL CASTINGS AND POWDERED METAL COMPONENTS |
SAE AS3128C : 2014(S2019) | PIN, EXPANSION - CRES, 416 OR 416SE, SHORT, UNS S41600/UNS S41623 |
MIL-DTL-38999 Revision M:2015 | Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect (Bayonet, Threaded or Breech Coupling), Environment Resistant with Crimp Removable Contacts or Hermetically Sealed with Fixed, Solderable Contacts, General Specification for |
SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
SAE AMS 2411 : 2013 | PLATING, SILVER FOR HIGH TEMPERATURE APPLICATIONS |
SAE AS 83461/1 : 2016 | M83461 O-RING MOLDED FROM AMS-P-83461 RUBBER |
SAE AMS 2406 : 2015 | PLATING, CHROMIUM, HARD DEPOSIT |
SAE MA 2010 : 2012 | PACKING, PREFORMED - O-RING SEAL, STANDARD SIZES & SIZE CODES, METRIC |
SAE ARP 210 : 2014 | DEFINITION OF COMMONLY USED DAY TYPES (ATMOSPHERIC AMBIENT TEMPERATURE CHARACTERISTICS VERSUS PRESSURE ALTITUDE) |
SAE AS 8775 : 1998 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
SAE AS 4088 : 2011 | AEROSPACE ROD SCRAPER GLAND DESIGN STANDARD |
SAE AS 1241 : 2016 | FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT |
SAE AMS 7379 : 2008 | RUBBER: FLUOROCARBON ELASTOMER (FKM) 70 TO 80 HARDNESS, LOW TEMPERATURE SEALING TG -40 DEGREES F (-40 DEGREES C) FOR ELASTOMERIC SEALS IN AIRCRAFT ENGINE OIL, FUEL AND HYDRAULICS SYSTEMS |
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 AMS R 83485/1 : 2015 | RUBBER, FLUOROCARBON ELASTOMER, IMPROVED PERFORMANCE AT LOW TEMPERATURES, O-RINGS, SIZES AND TOLERANCES |
SAE AS 3122 : 2014 | PIN, EXPANSION - ALUMINUM, 2024-T4 AND 2024-T351, LONG (UNS A92024) |
SAE AMS 2403 : 2015 | PLATING, NICKEL, GENERAL PURPOSE |
SAE AS 1290 : 2011 | GRAPHIC SYMBOLS FOR AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS |
SAE AS 4059F : 2013 | AEROSPACE FLUID POWER - CONTAMINATION CLASSIFICATION FOR HYDRAULIC FLUIDS |
SAE AMS 2410 : 2010 | PLATING, SILVER, NICKEL STRIKE, HIGH BAKE |
ISO 3601-1:2012 | Fluid power systems — O-rings — Part 1: Inside diameters, cross-sections, tolerances and designation codes |
SAE AS 3209 : 2013 | PACKING, PREFORMED - AMS 7276, 'O' RING |
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) |
ISO 16889:2008 | Hydraulic fluid power Filters Multi-pass method for evaluating filtration performance of a filter element |
SAE AS 3130 : 2014 | PIN, EXPANSION - CRES, 303, LONG, UNS S30300 |
SAE ARP 1383 : 2013 | AEROSPACE - IMPULSE TESTING OF HYDRAULIC COMPONENTS |
NAS1612:2005 | PACKING, ETHYLENE PROPYLENE PREFORMED, O-RING PHOSPHATE ESTER RESISTANT, STRAIGHT THREAD TUBE FITTING BOSS (-65 DEGREES F TO 250/300 DEGREES F) |
NAS1599:1980 | CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE CIRCULAR, ENVIRONMENT RESISTING, 200 DEG. C. MAXIMUM TEMPERATURE |
SAE AMS 2405E: 2013 | ELECTROLESS NICKEL PLATING, LOW PHOSPHORUS |
SAE AS 4052 : 2015 | GLAND DESIGN: SCRAPER, LANDING GEAR, INSTALLATION |
SAE AS 3124 : 2014 | PIN, EXPANSION - ALUMINUM, 2024-T4 AND 2024-T351, SHORT, UNS A92024 |
SAE AS 5202 : 2005 | PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD |
SAE AMS 2433 : 2004 | PLATING, NICKEL-THALLIUM-BORON OR NICKEL-BORON ELECTROLESS DEPOSITION |
SAE AS 33566 : 2013 | FITTINGS, INSTALLATION OF FLARELESS TUBE, STRAIGHT-THREADED CONNECTORS |
SAE AS 3131 : 2014 | PLUG, EXPANSION - CRES, 303, SHORT; STD AND .010 OVERSIZE DIAMETERS, UNS S30300 |
NASM 21209 : 2003 | INSERT, SCREW THREAD, COARSE AND FINE, SCREW LOCKING, HELICAL COIL, CRES |
NAS 1611:2005 | PACKING, ETHYLENE PROPYLENE, PREFORMED O-RING, PHOSPHATE ESTER RESISTANT (-65 DEGREES F TO 250/300 DEGREES F) |
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