MISSILE, MINUTEMAN III, LGM-30,HELICOPTER, CHINOOK, CH-47,AIRCRAFT, STRATOLIFTER C/KC-135,AIRCRAFT, HERCULES C-130,AIRCRAFT, TOMCAT F-14,AIRCRAFT, HAWKEYE E-2C,AIRCRAFT, FREEDOM FIGHTER F-5,AIRCRAFT, THUNDERBOLT II, A-10,AIRCRAFT, F-16,CARRIER, PERS M-113A1, M-113A2, M-113A3,BLADE, MINE CLEARING,,TANK, M-60 SERIES,HELICOPTER, KIOWA OH-58 A&C,TANK, ABRAMS M-1,MISSILE, AIR LAUNCH CRUISE (ALCM) AGM-86B,FIGHTING VEHICLE SYSTEMS, BRADLEY (BFVS),HELICOPTER, BLACK HAWK UH-60A, UH-60L, HH/UH-60M, UH-60V,HELICOPTER, SEA KNIGHT H-46,AIRCRAFT, T-38,HELICOPTER, RH-53,AIRCRAFT, HORNET F/A-18,HELICOPTER, LAMPS MARK III, SH-60B,AIRCRAFT, PROWLER EA-6B,HELICOPTER, COBRA/ATTACK, AH-1J,HELICOPTER, UTILITY/SEARCH AND RECOVERY UH-1N,TA-4J AIRCRAFT,AIRCRAFT, HARRIER AV-8B,AIRCRAFT, HERCULES C-130F,AIRCRAFT, HERCULES KC-130,AIRCRAFT, ORION P-3,ENGINE, AIRCRAFT T-400,COMMUNICATIONS PROGRAM, COMBAT THEATER (TRI-TAC) 478I,SUPPORT EQUIPMENT, F-16 AIRCRAFT,SUPPORT EQUIPMENT, B-52 AIRCRAFT,SUPPORT EQUIPMENT, B-1 AIRCRAFT,SPECIAL, COMMON GROUND EQUIPMENT, AGE,MIDS JTRS AN/USQ190,AIRCRAFT, SOF (AC-130H, AC-130J, AC-130U, EC-130E, EC-130H,,AIRCRAFT, C-2A (REPROCURED),LIGHT ARMORED VEHIC (TAMCN: E09467B),HELICOPTER, H1 ALL VERSIONS,AIRCRAFT, T-39,HELICOPTER, MH-53E,HELICOPTER, ADVANCE ATTACK, AH-1W,ROCKET SYSTEM LAUNCH PROGRAM (SUPPORT EQUIP, MX PEACEKEEPER),LANDING CRAFT AIR CUSHION (LCAC),E2/C2 ALL SERIES AIRCRAFT,HELICOPTER, CARRIER BASED ASW, SH-60F,HELICOPTER, SEARCH AND RESCUE, HH-60H,HELICOPTER, USCG SEARCH AND RESCUE, HH-60J,AIRCRAFT,B-2 BOMBER (ATB),ARLEIGH BURKE CLASS DDG,CONSOLIDATED GROUND SUPPORT EQUIPMENT,THIS WILL BE THE PARENT WSDC FOR ALL ARMY MRAP WSDCS,T1A AIRCRAFT,MRAP BAE RG33 SV (SOCOM),SPECIAL, MISC. GENERAL D035,U-2 AIRFRAME,U-2 SUPPORT EQUIPMENT,HELICOPTER, ELECTRONIC COUNTERMEASURES, EH-60A,TANK, COMBAT, FT, 120MM GUN (M1A1),HELICOPTER OBSERVATION (AHIP), OH-58D,ASSAULT AMPHIBIOUS VEHICLE, COMMAND (AAVC7A1),ASSAULT AMPHIBIOUS VEHICLE, PERSONNEL AAVP7A1,ASSAULT AMPHIBIOUS VEHICLE, RECOVERY AAVR7A1,F5,HELICOPTER, SEAHAWK, H-60,AVIATION ENGINE TEST SYSTEMS (AETS),AIRCRAFT, F/A-18, A - D, E/F, G (GROWLER)
5.500 INCHES MAXIMUM
3.000 INCHES NOMINAL SINGLE MOUNTING FACILITY
2.438 INCHES MAXIMUM
4.500 INCHES MAXIMUM
METAL
HERMETIC
0.266 INCHES NOMINAL SINGLE MOUNTING FACILITY
MODERATELY RUGGED
MRAP - RG-33
1
GENERAL
1
66.0 OHMS NOMINAL SINGLE WINDING
CONTINUOUS
AIR
2 UNTHREADED HOLE SINGLE MOUNTING FACILITY
GENERAL PURPOSE WAREHOUSE
60.340 CUBIC INCHES
IN-LINE SINGLE MOUNTING FACILITY
1 POLE, SINGLE THROW, NORMALLY OPEN, DOUBLE MAKE, MOMENTARY ACTION
600.0 MILLIAMPERES DC SINGLE WINDING
0.04 SECONDS MAXIMUM FIXED OPERATE TIME
0.01 SECONDS MAXIMUM FIXED RELEASE TIME
28.0 VOLTS DC 25 DEG CELSIUS SINGLE WINDING
400.0 AMPERES DC RESISTIVE LOAD
100.0 AMPERES DC INDUCTIVE LOAD
400.0 AMPERES DC MOTOR LOAD
115.0 AC AND 28.0 DC
81349-MIL-R-6106 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.).
