Part Details | THERMOSTATIC SWITCH
5930-00-200-9326 A switch that is actuated by changes in ambient temperature. Excludes CIRCUIT BREAKER; CONTROL, TEMPERATURE (as modified); FUSE (as modified); PROTECTOR, THERMAL-OVERLOAD, ELECTRICAL MOTOR; RELAY, THERMAL; and THERMOSTAT, FLOW CONTROL. See also CONTROL, TEMPERATURE (as modified) and REGULATOR, TEMPERATURE (as modified).
Alternate Parts: 17343104300, 17343-104-300, M2423615300, M24236/15-300, MILS2423615, MIL-S-24236/15, MILPRF2423615, MIL-PRF-24236/15, 5930-00-200-9326, 00-200-9326, 5930002009326, 002009326
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | MAR 31, 1973 | 00-200-9326 | 00451 ( SWITCH, THERMOSTATIC ) |
REFERENCE DRAWINGS & PICTURES
CYLINDRICAL W/FLANGE
Cross Reference | NSN 5930-00-200-9326
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 17343-104-300 | 73168 | KIDDE TECHNOLOGIES INC.DBA FENWAL SAFETY SYSTEMS |
| M24236/15-300 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-24236/15 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-PRF-24236/15 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5930-00-200-9326
| Characteristic | Specifications |
|---|---|
| STYLE DESIGNATOR | 4 CYLINDRICAL W/FLANGE |
| OVERALL LENGTH | 1.578 INCHES NOMINAL |
| OVERALL HEIGHT | 5.125 INCHES MAXIMUM |
| BODY DIAMETER | 0.625 INCHES NOMINAL |
| BODY HEIGHT | 3.500 INCHES NOMINAL |
| NONPILE-UP CONTACT ARRANGEMENT | 1 POLE, SINGLE THROW, NORMALLY OPEN, MOMENTARY ACTION |
| CONTACT ACTION STIMULUS | INCREASE |
| CONTACT ADJUSTABILITY | DEACTUATION POINT ADJUSTABLE, PRESET AND ACTUATION POINT ADJUSTABLE, PRESET |
| CONTACT ADJUSTMENT RANGE | +135.00 TO +1000.00 ACTUATION POINT DEGREES FAHRENHEIT AND +135.00 TO +1000.00 DEACTUATION POINT DEGREES FAHRENHEIT |
| CONTACT ADJUSTMENT TYPE | INTERNAL DEACTUATION POINT SCREW AND INTERNAL ACTUATION POINT SCREW |
| CONTACT STIMULUS RATING | AF300.00 ACTUATION POINT NOMINAL AND AF280.00 DEACTUATION POINT NOMINAL |
| OPERATING TEMP RATING | -65.0 DEG FAHRENHEIT MINIMUM AND 1000.0 DEG FAHRENHEIT MAXIMUM |
| MEDIA FOR WHICH DESIGNED | Q$DADF |
| TEMP SENSING ELEMENT TYPE | EXPANDING SHELL |
| TERMINAL TYPE | THREADED STUD |
| MOUNTING METHOD | FLANGE AND UNTHREADED HOLE |
| UNTHREADED MOUNTING HOLE DIAMETER | 0.221 INCHES NOMINAL |
| MOUNTING FACILITY PATTERN | THREE POSITION CIRCULAR |
| MOUNTING FACILITY CIRCLE RADIUS | 0.625 INCHES NOMINAL |
| FEATURES PROVIDED | HERMETICALLY SEALED CASE AND INTERNALLY GROUNDED |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| TEST DATA DOCUMENT | 81349-MIL-S-24236 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.). |
| SPECIFICATION/STANDARD DATA | 81349-MIL--24236 TO 15 GOVERNMENT SPECIFICATION |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | WEAPON SYSTEMS-AIRCRAFT, HERCULES C-130; ENGINE, AIRCRAFT, T56-A-7/15 (C-130B/E/H/N/P); AIRCRAFT, SOF (AC-130H, MC-130H, EC-130E, HC-130); AIRCRAFT, AWACS, E-3A; AIRCRAFT, STATOLIFTER C-135; U-2 AIRFRAME |