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AN 6270 : 0010
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HOSE ASSEMBLY - DETACHABLE SWIVEL FITTING, LOW PRESSURE |
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MIL-DTL-83797 Revision C:2008
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HOSE, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
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DEFSTAN 00-970(PT0)/9(2012) : 2012
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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MIL-DTL-8790 Revision F:2007
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Hose Assemblies, Rubber, Hydraulic, High Pressure 3,000 PSI, Operating Temperature Range -65 Degrees F to +275 Degrees F, Field Attachable |
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DEFSTAN 00-970(PT0)/17(2016) : 2016
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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DEFSTAN 00-970(PT0)/14(2014) : 2014
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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DEFSTAN 00-970(PT0)/7(2011) : 2011
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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MIL-DTL-6000 Revision D:2007
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HOSE, RUBBER, AIRCRAFT, FUEL, OIL, COOLANT, WATER, AND ALCOHOL |
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MIL-PRF-7061 Revision E:2014
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HOSE, ELASTOMERIC, AIRCRAFT, SELF-SEALING, AROMATIC FUEL |
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MIL-PRF-26385 Revision G:2013
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HOSE, OXYGEN AND PRESSURIZATION, OZONE RESISTANT |
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MIL-DTL-83796 Revision B:2008
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HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
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DEFSTAN 00-970(PT0)/11(2013) : 2013
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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DEFSTAN 00-970(PT0)/13(2014) : 2014
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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DEFSTAN 00-970(PT0)/12(2014) : 2014
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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DEFSTAN 00-970(PT0)/15(2015) : 2015
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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MIL-PRF-87961 Revision B:2013
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HOSE AND HOSE ASSEMBLIES, AIR DUCT, AIR BREATHING, OXYGEN SYSTEM |
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DEFSTAN 00-970(PT0)/8(2011) : 2011
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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DEFSTAN 00-970(PT0)/16(2015) : 2015
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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MIL-DTL-8788 Revision G:2015
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Hose, Rubber, Hydraulic, High Pressure 3,000 PSI, Operating Temperature Range -65 Degrees F to +160 Degrees F |
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DEFSTAN 00-970(PT0)/10(2013) : 2013
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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MIL STD 11991 : A
|
GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
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MIL-DTL-6162 Revision C:2000
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GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
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MIL-DTL-62478 Revision C:2010
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COUPLER, OPTICAL |
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MIL-STD-1587 Revision D:2017
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MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
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MIL-DTL-8795 Revision G:2014
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Hose Assemblies, Elastomeric, Hydraulic, Fuel, Coolant, and Oil Resistant, General Specification for |
|
MIL-R-8931 Revision A:1994
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RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE |
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ZZ-H-617 Revision C:2002
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Hose, Rubber, Windshield Wiper |
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SAE ARP 5316 : 2014
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STORAGE OF ELASTOMER SEALS AND SEAL ASSEMBLIES WHICH INCLUDE AN ELASTOMER ELEMENT PRIOR TO HARDWARE ASSEMBLY |
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MIL-DTL-13444 Revision H:2006
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Hose and Hose Assemblies, Rubber: Fuel and Oil |
|
MIL-PRF-62368 Revision C:2009
|
Motor, Gearhead, 18-30 Volts, Direct Current |
|
SAE AS 6399 : 1999
|
HOSE, RUBBER, WIRE-WOUND, SYNTHETIC, ICE ELIMINATING SYSTEM |
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MIL-DTL-8794 Revision F:2007
|
HOSE, SYNTHETIC RUBBER - HYDRAULIC FLUID, FUEL, AND OIL RESISTANT |
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MIL-DTL-5593 Revision E:2006
|
HOSE, AIRCRAFT, LOW PRESSURE AIR AND VACUUM, FLEXIBLE |
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SAE AS 5316 : 2017
|
STORAGE OF ELASTOMER SEALS AND SEAL ASSEMBLIES WHICH INCLUDE AN ELASTOMER ELEMENT PRIOR TO HARDWARE ASSEMBLY |
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SAE AIR 5386 : 2013
|
HOSE AND HOSE ASSEMBLY SELECTION, INSTALLATION, INSPECTION AND MAINTENANCE GUIDELINES, LISTING OF |
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MIL-HDBK-695 Revision F:2017
|
RUBBER PRODUCTS: RECOMMENDED SHELF LIFE |
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MIL-DTL-27516 Revision G:2011
|
Hose and Hose Assembly, Nonmetallic, Suction and Discharge |
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N285.0-17/N285.6 SERIES-17
|
General requirements for pressure-retaining systems and components in CANDU nuclear power plants / Material Standards for reactor components for CANDU nuclear power plants |
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MIL-DTL-26894 Revision D:1998
|
Hose and Hose Assembly, Rubber, Gasoline, Refueling, Low Temperature |
|
MIL-DTL-5498 Revision G:2013
|
ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
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MIL-PRF-62365 Revision C:1997
|
MOTOR, HYDRAULIC, CONSTANT DISPLACEMENT |
|
MIL-DTL-6615 Revision G:2008
|
Hose Assemblies, Rubber, Fuel and Nonpotable Water, with Reattachable Couplings, Low Temperature, General Specification for |
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MIL-DTL-28693 Revision B:2016
|
Hose, Rubber, Oil and Gasoline Discharge, Smooth Bore, Lightweight Buoyant Type, Longitudinally Reinforced, 6 Inch |
|
MIL-DTL-29210 Revision E:2009
|
HOSE ASSEMBLY, RUBBER, METAL LINED, WIRE REINFORCED, 250 PSIG, SATURATED STEAM SERVICE |
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SAE AIR 797 : 2013
|
HOSE CHARACTERISTICS AND SELECTION CHART |
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MIL-DTL-5508 Revision C:2007
|
FUSES, AIRCRAFT AUTOMATIC QUANTITY-MEASURING, HYDRAULIC |
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MIL PRF 62478 : A
|
COUPLER, OPTICAL |
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SAE AIR 1364 : 1995
|
AGE CONTROL OF AGE SENSITIVE ELASTOMERIC MATERIALS |
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MIL-DTL-13719 Revision G:2012
|
HOSE AND HOSE ASSEMBLY, RUBBER, HYDRAULIC BRAKE, TYPE 1 AND TYPE 2 |
|
MIL-DTL-26521 Revision L:2014
|
Hose Assembly, Nonmetallic, Fuel, Collapsible, Low Temperature with Non-Reusable Couplings |
|
CSA N285.2 : 0
|
REQUIREMENTS FOR CLASS 1C, 2C AND 3C PRESSURE-RETAINING COMPONENTS AND SUPPORTS IN CANDU NUCLEAR POWER PLANTS |