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MIL-DTL-28840-14 Revision G:2013
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CONNECTORS, ELECTRICAL, CIRCULAR, THREADED, HIGH SHOCK, HIGH DENSITY, SHIPBOARD, CRIMP CONTACTS, RECEPTACLE, JAM NUT MOUNTING, CLASSES D, DS, P, T, TS, Z, AND ZS |
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SAE ARP 6001 : 2012
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AEROSPACE - PASSIVE SIDE STICK UNIT, GENERAL REQUIREMENTS FOR FLY BY WIRE TRANSPORT AND BUSINESS |
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SAE ARP 4493 : 2013
|
AEROSPACE - DIRECT DRIVE SERVOVALVES |
|
SAE AS 19692 : 2016
|
Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
|
MIL-DTL-12109-21 Revision B:2011
|
SOLENOID, ELECTRICAL; CLASS 2 (MACHINE GUN) 7.62 MM, 24 VOLT DC, 8 AMP MAX |
|
MS3186 Revision G:2011
|
CONNECTOR, MOUNTING TO CONNECTORS, MOUNTING NUTS, PLAIN HEXAGON |
|
MIL-DTL-25531 Revision F:2013
|
Coupling Half, Quick Disconnect, Pneumatic Starter, External, Low Pressure |
|
MIL-DTL-5523 Revision E:2011
|
VALVE; RELIEF, HYDRAULIC PRESSURE |
|
MIL-DTL-917 Revision F:2014
|
ELECTRIC POWER EQUIPMENT, BASIC REQUIREMENTS FOR |
|
MIL-DTL-24694 Revision A:2011
|
VALVE, HYDRAULIC RELIEF, 1.5 - 35 BARS (22 - 500 POUNDS PER SQUARE INCH) CARTRIDGE TYPE, GENERAL SPECIFICATION FOR (METRIC) |
|
MS28882 Revision G:2009
|
VALVE, FUEL CHECK, LOW PRESSURE, GASKET SEAL STRAIGHT THREAD CONNECTION |
|
MIL-DTL-22263 Revision C:2009
|
Coupling Fuel Line, Flexible, 125 PSI General Specification for |
|
MS28884 Revision F:2009
|
VALVE, FUEL CHECK, LOW PRESSURE, FLARED TUBE CONNECTION |
|
MS21430 Revision B:2009
|
VALVE, CHECK, FUEL AND AIR, POPPET TYPE, ZERO, LEAK |
|
MIL STD 11991 : A
|
GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
|
MIL-DTL-6162 Revision C:2000
|
GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
|
SAE ARP 1281 : 2002
|
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
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SAE ARP 5305 : 2017
|
STRUCTURAL DESIGN AND CONSTRUCTION CONSIDERATIONS FOR ENCLOSED TURBOFAN/TURBOJET ENGINE TEST CELLS |
|
SAE ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
|
MIL-DTL-85061 Revision C:2009
|
COUPLING, FUEL LINE, FLEXIBLE, 125 PSI |
|
MIL-PRF-81975 Revision C:2008
|
COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
|
NASA STD 5020 : 2012
|
REQUIREMENTS FOR THREADED FASTENING SYSTEMS IN SPACEFLIGHT HARDWARE |
|
SAE AS 4073 : 2013(R2018)
|
AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
|
SAE ARP 5812 : 2017
|
ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE |
|
SAE ARP 1350 : 2012
|
PROCEDURE FOR INSTALLATION AND MOUNTING OF SINGLE HOLE MOUNT, CYLINDRICAL, ELECTRICAL CONNECTORS (FOR PRESSURE DIFFERENTIAL APPLICATIONS) |
|
NASA KSC E 165 : 2009
|
ELECTRICAL GROUND SUPPORT EQUIPMENT FABRICATION, SPECIFICATION FOR |
|
NASA PRC 9005 : 2007
|
PROCESS SPECIFICATION FOR LOCKWIRING |
|
NASA MSFC STD 561 : 2004
|
THREADED FASTENERS, REQUIREMENTS FOR SECURING OF FLIGHT HARDWARE USED ON SHUTTLE PAYLOADS AND EXPERIMENTS |
|
MIL-HDBK-454 Revision B:2007
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
|
MIL-PRF-57267 Base Document:2017
|
COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
|
MIL-DTL-9490 Revision E:2008
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
|
SAE ARP 4058 : 2017
|
GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS |
|
SAE AS 50881 : 2015
|
WIRING AEROSPACE VEHICLE |
|
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL-DTL-9398 Revision D:2007
|
GENERATOR, TACHOMETER, TWO-POLE, HIGH TEMPERATURE, AIRCRAFT |
|
MIL-STD-2193 Revision C:2012
|
Ship Hydraulic System Components |
|
SAE ARP 988 : 2016
|
ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |