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MIL-PRF-5503 Revision G:2013
|
ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
|
MIL-DTL-5515 Revision F:2013
|
PUMP, HYDRAULIC, RAM, HAND DRIVEN |
|
SAE AS 19692 : 2016
|
Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
|
DEFSTAN 00-970(PT0)/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/17(2016) : 2016
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/7(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/14(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
|
DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
|
DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
|
DEFSTAN 00-970(PT0)/11(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/13(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
MIL-DTL-5523 Revision E:2011
|
VALVE; RELIEF, HYDRAULIC PRESSURE |
|
DEFSTAN 00-970(PT0)/15(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/12(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
|
DEFSTAN 00-970(PT0)/16(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
SAE ARP 5796 : 2013
|
FLIGHT CRITICAL CONTROL VALVES, MILITARY AIRCRAFT |
|
SAE ARP 1281 : 2002
|
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
|
MIL-DTL-25427 Revision B:2009
|
COUPLING ASSEMBLY, HYDRAULIC, SELF SEALING, QUICK DISCONNECT, GENERAL SPECIFICATION FOR |
|
MIL-DTL-5513 Revision D:2012
|
SWIVEL JOINT, HYDRAULIC |
|
SAE AS 85720 : 2018
|
FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE BEAM SEAL, 5000/8000 PSI, GENERAL SPECIFICATION FOR |
|
SAE AS 5466 : 2012
|
AEROSPACE - GENERAL REQUIREMENTS FOR HYDRAULIC FUSE - QUANTITY MEASURING |
|
SAE AS 4157 : 2017
|
COUPLING ASSEMBLIES, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT, 8000 POUNDS PER SQUARE INCH, GAGE |
|
MIL-DTL-19068 Revision B:2006
|
VALVES, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 2 SYSTEMS |
|
SAE ARP 4378 : 2017
|
ACCUMULATOR, HYDRAULIC, WELDED BELLOWS, FACTORY PRE-CHARGED |
|
SAE ARP 5812 : 2017
|
ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE |
|
SAE ARP 1070E : 2019
|
DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
|
SAE AS 4941 : 2015
|
AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
|
SAE AS 85421 : 2015
|
FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, BEAM SEAL, 3000/4000 PSI, GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
|
MIL-HDBK-516 Revision C:2014
|
AIRWORTHINESS CERTIFICATION CRITERIA |
|
MIL-DTL-9490 Revision E:2008
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, 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 ARP 1070 : 2014
|
DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
|
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
|
SAE ARP 4763 : 2017
|
AEROSPACE - GENERAL REQUIREMENTS FOR HYDRAULIC RELIEF VALVES |
|
MIL-DTL-5508 Revision C:2007
|
FUSES, AIRCRAFT AUTOMATIC QUANTITY-MEASURING, HYDRAULIC |
|
SAE AS 5072 : 2013
|
COUPLING ASSEMBLIES, NON-LOCKING PROBE STYLE, MINIATURE SELF-ALIGNING, SELF-SEALING DISCONNECTS |
|
JSSG-2009 Revision A:2013
|
Air Vehicle Subsystems |
|
SAE AS 5586 : 2005
|
GENERAL REQUIREMENTS FOR HYDRAULIC SYSTEM RESERVOIRS |
|
SAE AS 5467 : 2016
|
GENERAL REQUIREMENTS FOR HYDRAULIC FUSE - FLOW RATE |
|
SAE ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
|
SAE ARP 4945 : 2013
|
AEROSPACE-SOLENOID VALVE, HYDRAULIC, THREE WAY, TWO POSITION, DIRECT ACTING |
|
SAE ARP 1595 : 2013(R2019)
|
DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS |
|
SAE AIR 4543 : 2017
|
AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED |
|
SAE AS 1709 : 2014
|
COUPLING ASSEMBLY, HYDRAULIC SELF SEALING, QUICK DISCONNECT |
|
SAE ARP 4379 : 2016
|
AEROSPACE - ACCUMULATOR, HYDRAULIC, CYLINDRICAL, PISTON SEPARATED |
|
SAE ARP 988 : 2016
|
ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |