|
MIL DTL 28840/14 : G
|
CONNECTORS, ELECTRICAL, CIRCULAR, THREADED, HIGH SHOCK, HIGH DENSITY, SHIPBOARD, CRIMP CONTACTS, RECEPTACLE, JAM NUT MOUNTING, CLASSES D, DS, P, T, TS, Z, AND ZS |
|
SAE ARP 6001 : 2012
|
AEROSPACE - PASSIVE SIDE STICK UNIT, GENERAL REQUIREMENTS FOR FLY BY WIRE TRANSPORT AND BUSINESS |
|
SAE ARP 4493 : 2013
|
AEROSPACE - DIRECT DRIVE SERVOVALVES |
|
SAE AS 19692 : 2016
|
AEROSPACE - MILITARY TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED HYDRAULIC PUMP |
|
MIL DTL 6162 : C
|
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 |
|
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 85061C : 2009
|
COUPLING, FUEL LINE, FLEXIBLE, 125 PSI |
|
MIL PRF 81975 : C
|
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 : B
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
|
MIL PRF 57267 : 0
|
COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
|
MIL DTL 9490 : E
|
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 : D
|
GENERATOR, TACHOMETER, TWO-POLE, HIGH TEMPERATURE, AIRCRAFT |
|
MIL STD 2193 : C
|
SHIP HYDRAULIC SYSTEM COMPONENTS |
|
SAE ARP 988 : 2016
|
ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |