MIL-DTL-85052 Revision B:2005
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CLAMP, LOOP, CUSHION, GENERAL SPECIFICATION FOR |
ASTM F 2146 : 2013 : REDLINE
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Standard Specification for Wrought Titanium-3Aluminum-2.5Vanadium Alloy Seamless Tubing for Surgical Implant Applications (UNS R56320) |
SAE MA 2060 : 2015
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FITTINGS, WELDED, HYDRAULIC, TITANIUM AND CORROSION RESISTANT STEEL, 21 000 KPA, METRIC |
SAE AS 4076 : 2013
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CONTRACTILE STRAIN RATIO TESTING OF TITANIUM HYDRAULIC TUBING |
SAE AS 1946 : 2015
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HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, UP TO 1500 PSI AND 450 DEGREES F, HYDRAULIC AND PNEUMATIC |
SAE J 1779 : 2013
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SHIP SYSTEMS AND EQUIPMENT - HYDRAULIC SYSTEM DESIGN CRITERIA FOR MARINE VEHICLES |
SAE ARP 4698 : 2013
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GUIDE FOR CHOOSING A MINIMUM WALL THICKNESS OF TUBING FOR USE WITH WELD FITTINGS CODED FOR A RANGE OF WALL SIZES |
SAE AIR 1388 : 1992
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SERVICE DAMAGE LIMITS FOR AIRCRAFT HYDRAULIC TUBING |
SAE ARP 1185 : 2013
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FLEXURE TESTING OF HYDRAULIC TUBING JOINTS AND FITTINGS |
SAE AIR 5005 : 2015
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AEROSPACE - COMMERCIAL AIRCRAFT HYDRAULIC SYSTEMS |
SAE MA 2150 : 2015
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CLAMPS, LOOP OR P STYLE, SINGLE POINT MOUNT, MULTIPLE SHAPES, METRIC |
SAE AS 85052 : 2015
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CLAMP ASSEMBLY, LOOP TYPE, CUSHIONED, GENERAL SPECIFICATION FOR |
SAE ARP 4752 : 2013
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AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS |
NASA HDBK 6025 : 2014
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GUIDELINES FOR THE SPECIFICATION AND CERTIFICATION OF TITANIUM ALLOYS FOR NASA FLIGHT APPLICATIONS |
SAE AIR 1529 : 1989
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FLEXURE TESTING OF HYDRAULIC TUBING JOINTS AND FITTINGS BY PLANAR RESONANT VIBRATION (FREE-FREE BEAM) |
SAE AS 4510 : 2013
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FITTINGS, WELD, FLUID CONNECTION, 5000 PSI |
MIL H 85800 : 0
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HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID FIBER REINFORCED, 5000 & 8000 PSI, GENERAL SPECIFICATION FOR |
MIL-F-85720 Base Document:1985
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FITTING, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM, SEAL, GENERAL SPECIFICATION FOR |
SAE AS 1241 : 2016
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FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT |
SAE MA 2151 : 2015
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CLAMP ASSEMBLIES, SADDLE OR OMEGA STYLE, TWO POINT MOUNT, MULTIPLE SHAPES, METRIC |
SAE AS 4388 : 2013
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HOSE ASSEMBLY PTFE HEAVY DUTY, -65 TO 400 DEGREES F (-55 TO 204 DEGREES C) 8000 PSI (56000 KPA) HYDRAULIC AND PNEUMATIC |
SAE ARP 4925 : 2014
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AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS |