|
MIL-PRF-5503 Revision G:2013
|
ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
|
MIL-DTL-9395-50 Base Document:2014
|
SWITCH, PRESSURE, ABSOLUTE TYPE 1, 5 AMPERES, 28.5 +/- .5 INCHES HG |
|
MS21959 Revision D:2011
|
Body,Cluster Fitting, Two-Way, 90 Degrees, Internal Boss |
|
SAE AS 4073 : 2013(R2018)
|
AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
|
MS21958 Revision D:2011
|
Body, Cluster Fitting, Two-Way, 180 Degrees, Internal Boss |
|
MIL-PRF-83419 Revision F:2016
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
|
MIL-DTL-9395-6 Revision C:2006
|
SWITCHES, PRESSURE (ABSOLUTE), TYPE 1, SPDT, 3 AMPERES |
|
SAE ARP 5543 : 2015
|
AIRCRAFT WHEEL INFLATION VALVES INCORPORATING AN INFLATION PRESSURE GAUGE |
|
MIL-DTL-32106 Base Document:2003
|
INITIATORS, ELECTRICAL, FOR ROCKET MOTOR IGNITERS |
|
MIL-DTL-5523 Revision E:2011
|
VALVE; RELIEF, HYDRAULIC PRESSURE |
|
MIL-DTL-5099 Revision C:2011
|
INDICATOR, CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1 |
|
MS28882 Revision G:2009
|
VALVE, FUEL CHECK, LOW PRESSURE, GASKET SEAL STRAIGHT THREAD CONNECTION |
|
NASA SSTD 8070 0044 : 2012
|
STANDARD FOR CARBON STEEL PIPING SYSTEMS |
|
MIL-PRF-27197 Revision F:2017
|
INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
|
SAE AS 4875 : 2016
|
FITTINGS, STRAIGHT THREADED BOSS OR FLANGED, FLUID CONNECTION |
|
MIL-DTL-81716 Revision A:2009
|
PACKING, PREFORMED, STRAIGHT THREADED TUBE FITTING BOSS, TYPE 2 HYDRAULIC (-65 DEGREES F TO +275 DEGREES F) |
|
MIL-PRF-38135 Revision D:2014
|
INDICATOR, INDICATED AIRSPEED AVU-19A, STANDBY |
|
SAE ARP 4925 : 2014
|
AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS |
|
SAE AS 4841 : 2017
|
FITTINGS, 37 DEGREES INTERNAL FLARE, FLUID CONNECTION, PROCUREMENT SPECIFICATION |
|
MIL-PRF-81975 Revision C:2008
|
COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
|
SAE AMS P 5510 : 2013
|
O-RING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS, TYPE 1 HYDRAULIC (-65 TO 160 DEGREES F) |
|
MIL-DTL-9395-49 Base Document:2014
|
SWITCH, PRESSURE, ABSOLUTE TYPE 1, 5 AMPERES, 24.5 +/- .5 INCHES HG |
|
MIL-DTL-9395-1 Revision D:2006
|
SWITCHES, PRESSURE (GAGE), TYPE 2, SPDT, 3 AMPERES |
|
MIL-DTL-7891 Revision G:2008
|
FILLER VALVE, AIRCRAFT OXYGEN |
|
MS21345 Revision B:2016
|
FITTINGS - INSTALLATION OF UNIVERSAL ELBOW |
|
MIL-DTL-25308 Revision C:2010
|
GAGE, PRESSURE, DIAL INDICATING, HYDRAULIC, TYPE ME-1 |
|
SAE AS 4875/1 : 2016
|
FITTINGS, STRAIGHT THREAD BOSS OR FLANGED 37 DEGREES FLARED, FLUID CONNECTION |
|
MS21946 Revision F:2012
|
Body, Cluster Fitting, One-Way, Internal Boss |
|
MIL-PRF-6164 Revision G:2012
|
VALVE; AIRCRAFT, PNEUMATIC, HIGH-PRESSURE CHARGING |
|
NASA SSTD 8070 0126 : 2014
|
TUBING SYSTEMS FOR FACILITY SYSTEMS, SPECIAL TEST EQUIPMENT, AND AEROSPACE HARDWARE |
|
NASA SSTD 8070 0069 : 2008
|
LOW PRESSURE VACUUM JACKETED PIPE |
|
NASA SSTD 8070 0047 : 2016
|
STANDARD FOR STAINLESS STEEL PIPING SYSTEMS AA, ACK1, ACK4, ACK6, B, BCK1, BCK3, BCK4, BCK6, BCK10, C, EE, G, H, JJ, K3, L1, L2, NCK1, NCK2, NCK3, NCK10, NCK11, P, R, T, AND Z |
|
MIL-DTL-38394 Revision E:2009
|
Transmitter, Pressure TRU-81/A, Oil, 0-500 PSI |
|
MIL-DTL-5498 Revision G:2013
|
ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
|
SAE AS 4941 : 2015
|
AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
|
JSSG-2009 Revision A:2013
|
Air Vehicle Subsystems |
|
MIL-PRF-25435 Revision D:2008
|
TRANSMITTERS, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL-DTL-9395-48 Revision C:2006
|
SWITCH, PRESSURE, ABSOLUTE TYPE 1, 5 AMPERES |
|
SAE AS 683 : 2012
|
INSTALLATION PROCEDURES AND TORQUES FOR FLUID CONNECTIONS |
|
SAE ARP 4752 : 2013
|
AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS |
|
SAE ARP 4763 : 2017
|
AEROSPACE - GENERAL REQUIREMENTS FOR HYDRAULIC RELIEF VALVES |
|
MIL-DTL-5508 Revision C:2007
|
FUSES, AIRCRAFT AUTOMATIC QUANTITY-MEASURING, HYDRAULIC |
|
AN6248 Revision 3:2011
|
PUMP - HYDRAULIC HAND, TYPE 3000 |
|
SAE ARP 5555 : 2016
|
RECOMMENDATIONS FOR INSTALLATION OF SEALS IN STANDARD GLANDS |
|
SAE AS 5586 : 2005
|
GENERAL REQUIREMENTS FOR HYDRAULIC SYSTEM RESERVOIRS |
|
MIL-DTL-9395-32 Revision D:2006
|
SWITCHES, PRESSURE, DIFFERENTIAL (TYPE 3), 4 AMPERES |
|
MS21960 Revision D:2011
|
Body, Cluster Fitting, Three-Way, Internal Boss |
|
MIL-DTL-9395-30 Revision H:2012
|
Switches, Pressure, (Gage), Type II 5 Amperes |
|
SAE AS 4875/3 : 2016
|
FITTINGS, STRAIGHT THREAD PORT OR FLANGED TO 24 DEGREES CONE FLARELESS, FLUID CONNECTION |
|
11/30250206 DC : 0
|
BS EN 6140 - AEROSPACE SERIES - PLUG, PROTECTIVE, NON METALLIC FOR FITTING ENDS <= 3000 PSI HYDRAULIC SYSTEMS |