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