Subject |
Spec # |
Spec Title |
Power |
MIL-STD-1275 |
CHARACTERISTICS OF 28 VOLT DC INPUT POWER TO UTILIZATION EQUIPMENT IN MILITARY VEHICLES |
MIL-STD-1399 -300B |
INTERFACE STANDARD SECTION 300B ELECTRIC POWER, ALTERNATING CURRENT |
|
MIL-STD-704 |
AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
|
Grounding |
MIL-STD-1310H |
SHIPBOARD BONDING, GROUNDING, AND OTHER TECHNIQUES FOR ELECTROMAGNETIC COMPATIBILITY, ELECTROMAGNETIC PULSE (EMP) MITIGATION, AND SAFETY |
APR1870 |
Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety |
|
PD-ED-1214 |
Electrical Grounding Practices for Aerospace Hardware, NASA |
|
MIL-HDBK-1857 |
HANDBOOK FOR GROUNDING, BONDING AND SHIELDING DESIGN PRACTICES |
|
EMI |
MIL-STD-461 |
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
MIL-STD-464C |
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
|
Harnessing |
NEMA WC 2700-2005 |
Standard For Aerospace And Industrial Electrical Cable |
AS50881 |
Wiring Aerospace Vehicle |
|
IPC/WHMA-A-620B |
Requirements and Acceptance for Cable and Wire Harness Assemblies (the bible for cable assy) |
|
Aircraft
|
MIL-STD-1760 |
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
MIL-STD-1553 |
DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
|
Safe
& |
MIL-STD-1901 |
MUNITION ROCKET AND MISSILE MOTOR IGNITION SYSTEM DESIGN, SAFETY CRITERIA FOR |
MIL-STD-331 |
FUZE AND FUZE COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR |
|
MIL-STD-1316 |
FUZE DESIGN, SAFETY CRITERIA FOR |
|
A&P |
AC 43.13-1B |
ACCEPTABLE METHODS, TECHNIQUES, AND PRATICES - AIRCRAFT INSPECTION AND REPAIR |
AC 43.13-2B |
ACCEPTABLE METHODS, TECHNIQUES, AND PRATICES - AIRCRAFT ALTERATIONS |
|
MIL-R-47196A |
RIVETS, BUCK TYPE, PREPARATION FOR AND INSTALLATION OF |
|
NASM47196 |
PREPARATION FOR AND INSTALLATION OF BUCK-TYPE RIVETS |
|
end