|
SAE ARP 4493 : 2013
|
AEROSPACE - DIRECT DRIVE SERVOVALVES |
|
MIL-DTL-32480 Base Document:2014
|
Adapter, Hydraulic and Pneumatic, Flareless Tube Fitting to ORFS Connectors, 1500 to 3000 PSI and Minus 65 Degrees Fahrenheit to Plus 250 Degrees Fahrenheit, General Specification for |
|
MIL-DTL-5515 Revision F:2013
|
PUMP, HYDRAULIC, RAM, HAND DRIVEN |
|
MIL-PRF-32104 Base Document:2010
|
MOBILE HYDRAULIC OIL DISPENSER |
|
MIL-STD-290 Revision H:2013
|
PACKAGING AND MARKING OF PETROLEUM AND RELATED PRODUCTS |
|
MIL-DTL-8815-31 Base Document:2009
|
FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 3,000 PSI, 5 MICRON ABSOLUTE, -65 DEGREES F TO 275 DEGREES F |
|
MIL-DTL-32372 Revision A:2016
|
Fitting, Adapter, Hydraulic and Pneumatic, NPTF to ORFS Connectors, 1500 to 3000 PSI and -65°F to 250°F |
|
MIL-PRF-22750 Revision G:2011
|
COATING, EPOXY, HIGH-SOLIDS |
|
MIL-DTL-32554 Base Document:2016
|
STRAPS, TIE-DOWN, ADJUSTABLE, NON-METALLIC, CABLE BUNDLING, GENERAL SPECIFICATION FOR |
|
SAE AMS 3400 : 2017
|
FLUID, REFERENCE FOR TESTING POLYALPHAOLEFIN (PAO) RESISTANT MATERIAL |
|
MIL-PRF-32177 Revision A:2012
|
CLEANING COMPOUND, NONSKID |
|
MIL-DTL-25038 Revision J:2012
|
WIRE, ELECTRICAL, HIGH TEMPERATURE, FIRE RESISTANT, AND FLIGHT CRITICAL |
|
SAE ARP 5632 : 2016
|
ROTORCRAFT: APPLICATION OF EXISTING AIRCRAFT DESIGNED TIRES, WHEELS AND BRAKES |
|
SAE AIR 810 : 2013
|
DEGRADATION LIMITS OF HYDROCARBON-BASED HYDRAULIC FLUIDS, MIL-PRF-5606, MIL-PRF-83282, AND MIL-PRF-87257 USED IN HYDRAULIC TEST STANDS |
|
SAE AS 83461/2 : 2016
|
STRAIGHT THREAD TUBE FITTING BOSS O-RING MOLDED FROM AMS-P-83461 RUBBER |
|
SAE AS 83485 : 2016
|
O-RING MOLDED FROM AMS7287 MATERIAL |
|
SAE AIR 5693 : 2014
|
COMPATIBILITY OF PTFE HOSE ASSEMBLIES WITH TYPICAL FLUIDS FOUND IN AEROSPACE APPLICATIONS |
|
MIL-DTL-83797 Revision C:2008
|
HOSE, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
|
MIL-DTL-8790 Revision F:2007
|
Hose Assemblies, Rubber, Hydraulic, High Pressure 3,000 PSI, Operating Temperature Range -65 Degrees F to +275 Degrees F, Field Attachable |
|
MIL-DTL-24640 Revision C:2011
|
CABLES, LIGHTWEIGHT, LOW SMOKE, ELECTRIC, FOR SHIPBOARD USE, GENERAL SPECIFICATION FOR |
|
MIL-DTL-83796 Revision B:2008
|
HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
|
MIL-DTL-5523 Revision E:2011
|
VALVE; RELIEF, HYDRAULIC PRESSURE |
|
MIL-DTL-32330 Revision A:2015
|
Hose Assembly, Conductive Polytetrafluoroethylene Tube, Smooth Bore, Flared and Flareless, Tube to Hose, with Swivel Nut |
|
MIL-DTL-25579 Revision H:2014
|
Hose Assembly, Polytetrafluoroethylene, High Temperature, Medium Pressure, General Specification for |
|
MIL-DTL-8788 Revision G:2015
|
Hose, Rubber, Hydraulic, High Pressure 3,000 PSI, Operating Temperature Range -65 Degrees F to +160 Degrees F |
|
MIL-DTL-27267 Revision D:2012
|
Hose, Cres Wire Reinforced, Polytetrafluoroethylene, Four Hundred Fifty Degree Fahrenheit, Medium Pressure |
|
SAE AS 83461/1 : 2016
|
M83461 O-RING MOLDED FROM AMS-P-83461 RUBBER |
|
A-A-59935 Base Document:2013
|
Conical Seal, Crush, 37 Degree Flared Tube Fitting, General Requirements for |
|
MIL-PRF-5503 Revision G:2013
|
ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
|
MIL-PRF-6083 Revision G:2013
|
HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION |
|
MIL-DTL-25427 Revision B:2009
|
COUPLING ASSEMBLY, HYDRAULIC, SELF SEALING, QUICK DISCONNECT, GENERAL SPECIFICATION FOR |
|
MIL-DTL-32435 Base Document:2013
|
Hose, Polytetrafluoroethylene, Convoluted, 450 Degrees F, Medium Pressure |
|
MIL-PRF-8932 Revision B:1998
|
SWITCHES, PRESSURE, BULKHEAD MOUNTED, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL-DTL-83296 Revision B:2009
|
Fittings, Corrosion Resistant Steel, High Temperature, High Pressure (3000 PSI), Hydraulic and Pneumatic, General Specification for |
|
16/30354036 DC : 0
|
BS EN 4854-3 - AEROSPACE SERIES - BEARINGS, SPHERICAL PLAIN, IN CORROSION RESISTING STEEL WITH SELF-LUBRICATING LINER, LOW STARTING TORQUE AND LOW FRICTION COEFFICIENT, ELEVATED DUTY CYCLES UNDER LOW OSCILLATIONS AT DIFFERENT OPERATING CONDITIONS - PART 3: TECHNICAL SPECIFICATION |
|
MIL-DTL-83298 Revision C:2009
|
Hose, Conductive Polytetrafluoroethylene Tube, High Temperature, High Pressure (3000 PSI), Hydraulicand Pneumatic |
|
MIL-DTL-8815-32 Base Document:2010
|
FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 3000 PSI, 5 MICRON ABSOLUTE, -65 DEGREES F TO 275 DEGREES F, H-60 AIRCRAFT |
|
SAE AIR 5358 : 2016
|
LANDING GEAR SHOCK STRUT HYDRAULIC FLUID |
|
MIL-DTL-81381 Revision C:2005
|
WIRE, ELECTRIC, POLYIMIDE-INSULATED, COPPER OR COPPER ALLOY |
|
SAE AS 83248/1 : 2016
|
O-RING MOLDED FROM AMS7276 MATERIAL |
|
MIL-PRF-27601 Revision C:1998
|
HYDRAULIC FLUID, FIRE RESISTANT, HYDROGENATED POLYALPHAOLEFIN BASE, HIGH TEMPERATURE, FLIGHT VEHICLE, METRIC |
|
MIL-DTL-32464 Revision A:2017
|
FITTINGS, ADAPTER, HYDRAULIC AND PNEUMATIC, 37 DEGREES SPHERICAL TO ANPT CONNECTORS, 1500 TO 3000 PSI, GENERAL SPECIFICATION FOR |
|
SAE AS 5960 : 2013
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC BRAID REINFORCED, 5080 PSI (35000 KPA), 400 DEGREES F (204 DEGREES C), AIRCRAFT HYDRAULIC SYSTEMS |
|
MIL-DTL-32371 Base Document:2012
|
Fittings, Adapter, Hydraulic and Pneumatic, Spherical to ORFS Connectors, 1500 to 3000 PSI, General Specification for |
|
MIL-DTL-64154 Revision B:2008
|
LAMINATE: FIBERGLASS-FABRIC-REINFORCED, PHENOLIC |
|
SAE AIR 1362 : 2016
|
AEROSPACE HYDRAULIC FLUIDS PHYSICAL PROPERTIES |
|
SAE AS 5466 : 2012
|
AEROSPACE - GENERAL REQUIREMENTS FOR HYDRAULIC FUSE - QUANTITY MEASURING |
|
SAE AS 620 : 2012
|
HOSE ASSEMBLIES, CONVOLUTED POLYTETRAFLUOROETHYLENE METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT |
|
SAE AIR 81 : 2016
|
IMPORTANCE OF PHYSICAL AND CHEMICAL PROPERTIES OF AIRCRAFT HYDRAULIC FLUIDS |
|
SAE ARP 4945 : 2013
|
AEROSPACE-SOLENOID VALVE, HYDRAULIC, THREE WAY, TWO POSITION, DIRECT ACTING |
|
SAE AS 83248/2 : 2016
|
O-RING MOLDED FROM AMS7259 MATERIAL |
|
SAE AS 683 : 2012
|
INSTALLATION PROCEDURES AND TORQUES FOR FLUID CONNECTIONS |
|
SAE AIR 786 : 2014
|
ELASTOMER COMPATIBILITY CONSIDERATIONS RELATIVE TO ELASTOMERIC SEALANT SELECTION |
|
SAE AS 614 : 2017
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 4000 PSI, 400 DEGREES F, HEAVY DUTY, HYDRAULIC AND PNEUMATIC |
|
SAE AIR 1228 : 2009
|
STANDARD IMPULSE MACHINE EQUIPMENT AND OPERATION |
|
MIL-DTL-13444 Revision H:2006
|
Hose and Hose Assemblies, Rubber: Fuel and Oil |
|
MIL-DTL-26633 Revision F:2014
|
HOSE ASSEMBLY, NONCONDUCTIVE, POLYTETRAFLUOROETHYLENE, OXYGEN |
|
SAE ARP 994 : 2016
|
DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS |
|
MIL-DTL-8794 Revision F:2007
|
HOSE, SYNTHETIC RUBBER - HYDRAULIC FLUID, FUEL, AND OIL RESISTANT |
|
SAE AS 5258 : 2012
|
INSULATING COMPONENT, MOLDED, ELECTRICAL, HEAT SHRINKABLE, CONNECTOR AND CABLE ACCESSORY, SEALING STRAIN RELIEF, GENERAL SPECIFICATION FOR |
|
MIL-PRF-32058 Revision B:2017
|
CHOCK, WHEEL-TRACK - AVIATION, ADJUSTABLE ROPE TYPE |
|
MIL-DTL-19068 Revision B:2006
|
VALVES, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 2 SYSTEMS |
|
SAE AS 5958 : 2017
|
FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPARABLE, FLUID SYSTEM FOR OPERATING PRESSURES UP TO AND INCLUDING 5080 PSI (35 000 KPA), SPECIFICATION FOR |
|
MIL-DTL-5593 Revision E:2006
|
HOSE, AIRCRAFT, LOW PRESSURE AIR AND VACUUM, FLEXIBLE |
|
SAE AS 4459 : 2013
|
FITTINGS, TUBE, FLUID SYSTEM 3000 PSIG (21000 KPA) RATED PRESSURE, EXTERNALLY SWAGED, SPECIFICATION FOR |
|
SAE ARP 5311 : 2016
|
AEROSPACE-INTERFACE DEFINITION FOR MECHANICAL ACTUATION SUBSYSTEMS |
|
MIL-DTL-32234 Base Document:2007
|
CONNECTORS, ELECTRICAL, ULTRA HIGH DENSITY, MODULAR, BLADE AND FORK, EIGHT ROW, GENERAL SPECIFICATION FOR |
|
MIL-DTL-53030 Revision B Interim Revision:2003
|
Primer Coating, Epoxy, Water Based, Lead and Chromate Free |
|
MIL-PRF-83860 Revision D:2013
|
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 MICRON ABSOLUTE |
|
MIL-DTL-32460 Revision A:2017
|
ADAPTER, HYDRAULIC AND PNEUMATIC, 37 DEGREES FLARE TUBE FITTING TO ORFS CONNECTORS, 1500 TO 3000 PSI AND -65 DEGREES F TO 250 DEGREES F, GENERAL SPECIFICATION FOR |
|
MIL-DTL-83798 Revision D:2008
|
FITTING, RUBBER HOSE, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
|
MIL-DTL-8795 Revision G:2014
|
Hose Assemblies, Elastomeric, Hydraulic, Fuel, Coolant, and Oil Resistant, General Specification for |
|
MIL-DTL-53030 Revision D:2011
|
Primer Coating, Epoxy, Water Based, Lead and Chromate Free |
|
MIL-STD-3004 Revision D:2014
|
QUALITY ASSURANCE/SURVEILLANCE FOR FUELS, LUBRICANTS AND RELATED PRODUCTS |
|
SAE AS 604 : 2012
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, HEAVYWEIGHT, HYDRAULIC |
|
SAE AS 2078 : 2015
|
TEST METHODS, HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE (PTFE) |
|
PREN 4854-3 : 200P1
|
AEROSPACE SERIES - BEARINGS, SPHERICAL PLAIN, IN CORROSION RESISTING STEEL WITH SELF-LUBRICATING LINER, LOW STARTING TORQUE AND LOW FRICTION COEFFICIENT, ELEVATED DUTY CYCLES UNDER LOW OSCILLATIONS AT DIFFERENT OPERATING CONDITIONS - PART 3: TECHNICAL SPECIFICATION |
|
SAE MA 1339 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 21,000 KPA, 204 DEGREE C, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC, METRIC |
|
SAE ARP 1595 : 2013(R2019)
|
DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS |
|
SAE AIR 1922 : 2017
|
AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
|
SAE AIR 5005 : 2015
|
AEROSPACE - COMMERCIAL AIRCRAFT HYDRAULIC SYSTEMS |
|
SAE AS 1975 : 2016
|
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems |
|
SAE AS 1709 : 2014
|
COUPLING ASSEMBLY, HYDRAULIC SELF SEALING, QUICK DISCONNECT |
|
SAE AS 18280 : 2017
|
FITTINGS, 24 DEGREES CONE FLARELESS, FLUID CONNECTION, 3000 PSI |
|
SAE AS 6235 : 2015
|
FACE SEAL GLAND DESIGN, STATIC, O-RING AND OTHER SEALS FOR AEROSPACE HYDRAULIC AND PNEUMATIC APPLICATIONS |
|
MIL-PRF-6164 Revision G:2012
|
VALVE; AIRCRAFT, PNEUMATIC, HIGH-PRESSURE CHARGING |
|
SAE ARP 5796 : 2013
|
FLIGHT CRITICAL CONTROL VALVES, MILITARY AIRCRAFT |
|
MIL-DTL-32434 Base Document:2013
|
Hose Assembly, Polytetrafluoroethylene, Convoluted, High Temperature, Medium Pressure, General Specification for |
|
SAE ARP 1281 : 2002
|
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
|
MIL-DTL-5498 Revision G:2013
|
ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
|
SAE ARP 6154 : 2017
|
AEROSPACE FLUID POWER ELECTROHYDROSTATIC MODULE, DESIGN, PERFORMANCE AND TEST RECOMMENDATIONS |
|
SAE AIR 1083 : 2012
|
AIRBORNE HYDRAULIC AND CONTROL SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT |
|
SAE AIR 5829 : 2008
|
AIR IN AIRCRAFT HYDRAULIC SYSTEMS |
|
MIL-PRF-32287 Revision A:2011
|
PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT |
|
MIL-DTL-83733 Revision E:2006
|
CONNECTORS, ELECTRICAL MINIATURE, RECTANGULAR TYPE, RACK TO PANEL, ENVIRONMENT RESISTING, 200 DEGREES C TOTAL CONTINUOUS OPERATING TEMPERATURE, GENERAL SPECIFICATION FOR |
|
MIL-DTL-5070 Revision F:2006
|
ADAPTER, HOSE TO TUBE, PIPE AND FLANGE, REUSABLE - HYDRAULIC, FUEL, AND OIL LINES, GENERAL SPECIFICATION FOR |
|
MIL-PRF-83861 Revision D:2013
|
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE |
|
MIL-DTL-8789 Revision G:2015
|
FITTING END, ATTACHABLE, HYDRAULIC, HIGH PRESSURE (3,000 PSI), GENERAL SPECIFICATION FOR |
|
MIL-PRF-46170 Revision E:2013
|
HYDRAULIC FLUID, RUST INHIBITED, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, NATO CODE NO. H-544 |
|
MIL PRF 0032287 : 0
|
PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT |
|
MIL-PRF-5606 Revision H:2002
|
HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
|
SAE AS 595 : 2015
|
AEROSPACE - CIVIL TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED, HYDRAULIC PUMP |
|
SAE AS 1339 : 2017
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC |
|
SAE AS 5729 : 2016
|
O-RING MOLDED FROM AMS7379 (FLUOROCARBON) MATERIAL |
|
SAE AS 1227 : 2013
|
HOSE ASSEMBLY, CONVOLUTED POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, LOW PRESSURE, UP TO 400 DEGREES F, AIRCRAFT |
|
SAE ARP 5891 : 2014
|
ACHIEVING CLEANLINESS STANDARDS FOR AIRCRAFT HYDRAULIC SYSTEMS DURING MANUFACTURE |
|
SAE ARP 4763 : 2017
|
AEROSPACE - GENERAL REQUIREMENTS FOR HYDRAULIC RELIEF VALVES |
|
MIL-DTL-9129 Revision G:2014
|
Discharges, Electrostatic General Specification for |
|
SAE ARP 1311 : 2015
|
LANDING GEAR STRUCTURES AND MECHANISMS |
|
SAE AIR 4094 : 2016
|
AIRCRAFT FLIGHT CONTROL SYSTEMS DESCRIPTIONS |
|
JSSG-2009 Revision A:2013
|
Air Vehicle Subsystems |
|
MIL-DTL-28804 Revision D:1998
|
CONNECTORS, PLUG AND RECEPTACLE, ELECTRIC, RECTANGULAR, HIGH DENSITY, POLARIZATION CENTER JACKSCREW - GENERAL SPECIFICATION FOR |
|
MIL DTL 17 : J
|
CABLES, RADIO FREQUENCY, FLEXIBLE AND SEMIRIGID, GENERAL SPECIFICATION FOR |
|
MIL-DTL-8815-33 Base Document:2011
|
FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 3500 PSI, 5 MICRON ABSOLUTE, -65 DEGREES F TO 275 DEGREES F, AVIATION GROUND POWER UNIT (AGPU) |
|
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 4752 : 2013
|
AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS |
|
SAE AIR 5490 : 2016
|
CARBON BRAKE CONTAMINATION AND OXIDATION |
|
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 4941 : 2015
|
AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
|
SAE AS 4623 : 2016
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 3,000 PSI, 275 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS |
|
SAE AIR 4543 : 2017
|
AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED |
|
SAE AS 6116 : 2016
|
ALUMINUM FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPERABLE, FLUID SYSTEM, UP TO 1500 PSI (10340 KPA) MAXIMUM, SPECIFICATION FOR |
|
SAE ARP4912C:2017
|
DESIGN RECOMMENDATIONS FOR SPARE SEALS IN LANDING GEAR SHOCK STRUTS |
|
MIL-STD-1568 Revision D:2015
|
Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
|
SAE ARP 988 : 2016
|
ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |
|
SAE AS 1946 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, UP TO 1500 PSI AND 450 DEGREES F, HYDRAULIC AND PNEUMATIC |