Part Details | THERMOSTATIC SWITCH
5930-00-134-0404 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: 123SCEC407601, 123SCEC407-601, FYLD91382, FYLD9138-2, FYLD9138, FYLD50799, FYLD-50799, 123SCEC407601, 123SCEC407-601, 123SCEC4071, 123SCEC407-1, 123SCEC407, 123SB104201, 123SB10420-1, 5930-00-134-0404, 00-134-0404, 5930001340404, 001340404
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | SEP 20, 1968 | 00-134-0404 | 00451 ( SWITCH, THERMOSTATIC ) |
REFERENCE DRAWINGS & PICTURES
CYLINDRICAL
Cross Reference | NSN 5930-00-134-0404
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 123SCEC407-601 | 21856 | CENTROID, INC. |
| FYLD9138-2 | 05624 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
| FYLD9138 | 05624 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
| FYLD-50799 | 05624 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
| 123SCEC407-601 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
| 123SCEC407-1 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
| 123SCEC407 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
| 123SB10420-1 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
Technical Data | NSN 5930-00-134-0404
| Characteristic | Specifications |
|---|---|
| STYLE DESIGNATOR | 6 CYLINDRICAL |
| OVERALL LENGTH | 2.562 INCHES MAXIMUM |
| OVERALL WIDTH | 1.687 INCHES MAXIMUM |
| BODY DIAMETER | 1.125 INCHES MAXIMUM |
| BODY LENGTH | 1.937 INCHES MAXIMUM |
| CONTACT ADJUSTABILITY | DEACTUATION POINT NOT ADJUSTABLE AND ACTUATION POINT NOT ADJUSTABLE |
| OPERATING TEMP RATING | 400.0 DEG FAHRENHEIT MAXIMUM |
| MEDIA FOR WHICH DESIGNED | GAS |
| TERMINAL TYPE | CONNECTOR, RECEPTACLE |
| MOUNTING METHOD | FLANGE AND UNTHREADED HOLE |
| UNTHREADED MOUNTING HOLE DIAMETER | 0.165 INCHES MINIMUM AND 0.175 INCHES MAXIMUM |
| MOUNTING FACILITY PATTERN | FOUR POSITION RECTANGULAR |
| LONGEST HORIZONTAL DISTANCE BETWEEN MOUNTING CENTERS | 1.052 INCHES MINIMUM AND 1.072 INCHES MAXIMUM |
| LONGEST VERTICAL DISTANCE BETWEEN MOUNTING CENTERS | 1.052 INCHES MINIMUM AND 1.072 INCHES MAXIMUM |
| END ITEM IDENTIFICATION | AIRCRAFT MODEL C-2A |