MIL-T-5522 Revision D:1975
|
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS |
MIL V 81940 : B
|
VALVE, SAMPLING AND BLEED, HYDRAULIC, TYPE LI SYSTEMS |
MIL-F-8785 Revision C:1980
|
FLYING QUALITIES OF PILOTED AIRPLANES |
MIL-H-8890 Base Document:1961
|
HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
MIL-T-6845 Revision D:1985
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TUBING, STEEL, CORROSION-RESISTANT (304) AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION |
MIL-M-7997 Revision C:1981
|
MOTOR, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT GENERAL SPECIFICATION FOR |
SAE ARP 243 : 1993
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NOMENCLATURE, AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS |
MIL-B-8584 Revision C:1970
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BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF |
AN929 Revision 14:2017
|
CAP INSERT, ASSEMBLY, PRESSURE SEAL, FLARED TUBE FITTING |
SAE AIR 1362 : 2016
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AEROSPACE HYDRAULIC FLUIDS PHYSICAL PROPERTIES |
MS33656 Revision J:1987
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FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL |
MIL-P-5994 Revision D:1972
|
PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR |
MIL F 9490 : D
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
SAE ARP 994 : 2016
|
DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS |
MIL V 25675 : B
|
VALVE, CHECK, MINIATURE, HYDRAULIC, AIRCRAFT AND MISSILE |
MS33583 Revision C:1993
|
TUBING END, DOUBLE FLARE, STANDARD DIMENSIONS FOR |
MS33584 Revision C:1990
|
TUBING END, STANDARD DIMENSIONS FOR FLARED |
MIL F 8815 : D
|
FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
SAE AS 1290 : 2011
|
GRAPHIC SYMBOLS FOR AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS |
SAE ARP 584D : 2012
|
COILED TUBING - CORROSION RESISTANT STEEL, HYDRAULIC APPLICATIONS, AEROSPACE |
MIL-P-19692 Revision E:1994
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PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR |
MS33611 Revision A:1983
|
TUBE BEND RADII |
MIL G 8348 : H
|
GAGE, ASSEMBLIES, AIR PRESSURE, DIAL INDICATING CHUCK TYPE SELF CONTAINED |
MIL-H-5440 Revision H:1993
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
MIL-R-8931 Revision A:1994
|
RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE |
MIL C 85052 : A
|
CLAMP LOOP, CUSHION, GENERAL SPECIFICATION FOR |
FED-STD-791 Revision D:2007
|
TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
MIL F 18372 : 0
|
FLIGHT CONTROL SYSTEMS, DESIGN, INSTALLATION AND TEST OF, AIRCRAFT (GENERAL SPECIFICATION FOR) |
MIL-STD-1247 Revision D:2009
|
MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS |
MIL-B-5087 Revision B:1964
|
BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
MIL-W-5088 Revision L:1991
|
Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
AN6240 Revision 2:2008
|
Filter - Hydraulic Replaceable Element Vent Type |
MS21344 Revision A:2016
|
FITTING INSTALLATION OF FLARED TUBE STRAIGHT THREADED CONNECTORS DESIGN STANDARD FOR |
MIL-F-7179 Revision G:1993
|
FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |