MIL A 85670 : 0
|
ANTENNA, BROADBAND AS-3191/A, AS-3792/A, AND AS -3793/A |
MIL-I-83294 Base Document:1971
|
INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
MIL-A-23121 Revision C:1970
|
AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
MIL-HDBK-1587 Base Document:1996
|
MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
MIL-A-81973 Base Document:1974
|
AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
MIL S 8805 : D
|
SWITCHES, AND SWITCH ASSEMBLIES, SENSITIVE AND PUSH, SNAP ACTION, GENERAL SPECIFICATION FOR |
MIL S 22885 : E
|
SWITCH, PUSH BUTTON, ILLUMINATED, GENERAL SPECIFICATION FOR |
MIL-W-5088 Revision L:1991
|
Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
MIL-HDBK-508 Base Document:1998
|
WIRING AND WIRING DEVICES FOR COMBAT AND TACTICAL VEHICLES, SELECTION AND INSTALLATION OF |
MIL-STD-339 Base Document:1987
|
WIRING AND WIRING DEVICES FOR COMBAT AND TACTICAL VEHICLES, SELECTION AND INSTALLATION OF |
MIL-W-8160 Revision D:1961
|
WIRING, GUIDED MISSILE, INSTALLATION OF, GENERAL SPECIFICATION FOR |
MIL-STD-1250 Revision A:1992
|
CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
MIL-E-47231 Base Document:1974
|
ELECTRICAL COMPONENTS, POTTING OF |
MIL S 25057 : B
|
SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
MIL-HDBK-1250 Revision A:1995
|
CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
MIL-C-24360 Revision A:1969
|
CABLE ASSEMBLY, AIRCRAFT AUTONAVIGATOR ALIGNMENT, UMBILICAL |
MIL-S-83129 Revision A:1972
|
SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
MIL-DTL-85110 Revision B:1997
|
BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
MIL-A-28865 Revision A:1987
|
ANTENNA GROUP, OE-82()/WSC-1(V) |
MIL-C-81582 Revision B:1975
|
CONNECTOR, ELECTRICAL, BAYONET COUPLING, ENVIRONMENTAL RESISTING, UMBILICAL, GENERAL SPECIFICATION FOR |
MIL-A-46864 Revision B:1991
|
ADHESIVE, EPOXY, MODIFIED, FLEXIBLE, TWO COMPONENT |
IPC HDBK 630 : 0
|
GUIDELINES FOR DESIGN, MANUFACTURE, INSPECTION AND TESTING OF ELECTRONIC ENCLOSURES ASSEMBLY |
JSSG-2006 Base Document:1998
|
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
MIL-A-23622 Base Document:1963
|
ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT |
MIL C 5015 : G
|
CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR |
ADS-13F-HDBK : 1997
|
AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
MIL-D-81227 Revision B:1976
|
DETECTOR KIT, WATER, AUTOMOTIVE, AVIATION FUEL |
MIL-S-38399 Revision A:1975
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
MIL S 28788 : A
|
SWITCH, AIR AND LIQUID FLOW, SENSING GENERAL SPECIFICATION FOR |
MIL-I-83456 Base Document:1974
|
INSTALLATION OF SEGMENTED LIGHTNING DIVERTER STRIPS ON AIRCRAFT RADOMES, GENERAL SPECIFICATION FOR |
MIL-A-47089 Base Document:1974
|
ADHESIVE, METAL FILLED, CONDUCTIVE, ELECTRICAL AND THERMAL |