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SAE ARP 4493 : 2013
|
AEROSPACE - DIRECT DRIVE SERVOVALVES |
|
SAE AIR 5699 : 2013
|
A GUIDE FOR THE DAMAGING EFFECTS OF TIRE AND WHEEL FAILURES |
|
SAE ARP 994 : 2016
|
DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS |
|
SAE ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
|
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)/12(2014) : 2014
|
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)/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)/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/16(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
SAE ARP 4378 : 2017
|
ACCUMULATOR, HYDRAULIC, WELDED BELLOWS, FACTORY PRE-CHARGED |
|
SAE ARP 1281 : 2002
|
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
|
MIL-PRF-5503 Revision G:2013
|
ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
|
SAE ARP 5796 : 2013
|
FLIGHT CRITICAL CONTROL VALVES, MILITARY AIRCRAFT |
|
SAE AS 85720 : 2018
|
FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE BEAM SEAL, 5000/8000 PSI, GENERAL SPECIFICATION FOR |
|
SAE ARP 1802 : 2014
|
SELECTION AND APPLICATION OF POLYTETRAFLUOROETHYLENE (PTFE AND TFE) BACKUP RINGS FOR HYDRAULIC AND PNEUMATIC FLUID POWER APPLICATIONS |
|
SAE ARP 4945 : 2013
|
AEROSPACE-SOLENOID VALVE, HYDRAULIC, THREE WAY, TWO POSITION, DIRECT ACTING |
|
SAE AIR 5992 : 2015
|
DESCRIPTIONS OF SYSTEMS INTEGRATION TEST RIGS (IRON BIRDS) FOR AEROSPACE APPLICATIONS |
|
MIL-HDBK-516 Revision C:2014
|
AIRWORTHINESS CERTIFICATION CRITERIA |
|
SAE AIR 560 : 2007
|
MISSILE HYDRAULIC PUMPS |
|
MIL-DTL-19068 Revision B:2006
|
VALVES, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 2 SYSTEMS |
|
SAE AS 5586 : 2005
|
GENERAL REQUIREMENTS FOR HYDRAULIC SYSTEM RESERVOIRS |
|
SAE AS 19692 : 2016
|
Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
|
SAE AS 85421 : 2015
|
FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, BEAM SEAL, 3000/4000 PSI, GENERAL SPECIFICATION FOR |
|
SAE AIR 1922 : 2017
|
AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
|
SAE ARP 5891 : 2014
|
ACHIEVING CLEANLINESS STANDARDS FOR AIRCRAFT HYDRAULIC SYSTEMS DURING MANUFACTURE |
|
SAE AS 1709 : 2014
|
COUPLING ASSEMBLY, HYDRAULIC SELF SEALING, QUICK DISCONNECT |
|
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
|
SAE ARP 584 :2012(S2017)
|
COILED TUBING - CORROSION RESISTANT STEEL, HYDRAULIC APPLICATIONS, AEROSPACE |
|
MIL-DTL-9490 Revision E:2008
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
|
SAE ARP 4386 : 2017
|
TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES |
|
SAE AIR 5829 : 2008
|
AIR IN AIRCRAFT HYDRAULIC SYSTEMS |
|
JSSG-2009 Revision A:2013
|
Air Vehicle Subsystems |
|
MIL-PRF-32287 Revision A:2011
|
PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT |
|
MIL PRF 0032287 : 0
|
PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT |
|
SAE ARP 6200 : 2014
|
TEST REQUIREMENTS AND MEANS FOR COMMERCIAL AIRCRAFT HYDRAULIC SYSTEMS |
|
SAE ARP 4146D : 2012
|
COILED TUBING - TITANIUM ALLOY, HYDRAULIC APPLICATIONS, AEROSPACE |
|
SAE ARP 4752 : 2013
|
AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS |
|
SAE J 1782 : 2013
|
SHIP SYSTEMS AND EQUIPMENT - HYDRAULIC SYSTEMS - NOISE CONTROL |
|
MIL-DTL-5508 Revision C:2007
|
FUSES, AIRCRAFT AUTOMATIC QUANTITY-MEASURING, HYDRAULIC |
|
SAE AIR 737 : 2012
|
AEROSPACE HYDRAULIC AND PNEUMATIC SPECIFICATIONS, STANDARDS, RECOMMENDED PRACTICES, AND INFORMATION REPORTS |
|
SAE AIR 4094 : 2016
|
AIRCRAFT FLIGHT CONTROL SYSTEMS DESCRIPTIONS |
|
SAE AIR 5451 : 2017
|
A GUIDE TO LANDING GEAR SYSTEM INTEGRATION |
|
SAE ARP 5555 : 2016
|
RECOMMENDATIONS FOR INSTALLATION OF SEALS IN STANDARD GLANDS |
|
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
|
SAE ARP 5794 : 2014
|
CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
|
SAE ARP 4925 : 2014
|
AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS |
|
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 ARP 4379 : 2016
|
AEROSPACE - ACCUMULATOR, HYDRAULIC, CYLINDRICAL, PISTON SEPARATED |
|
SAE ARP 988 : 2016
|
ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |
|
SAE ARP994C:2023
|
Design of Tubing Installations for Aerospace Hydraulic Systems |
|
SAE AIR5992:2009(R2023)
|
Descriptions of Systems Integration Test Rigs (Iron Birds) for Aerospace Applications |