Part Details | FLOW SWITCH
5930-00-539-6600 A switch which is specifically designed to operate by the influence of a gaseous, liquid, or solid media velocity on its actuator.
Alternate Parts: G2057251, G-205725-1, 338018686, 33-801868-6, 338018686, 33-801868-6, G330050S1, 7408010P6, 340C100581, 340C10058-1, 2A2450, 2A2450, 24502A, 2450-2A, 2450, 2A2450PT1, 2A2450, 2ATYPE2450, 2AM0DELTYPE2450, 041106, 035656, 020035, 8176871, 5930-00-539-6600, 00-539-6600, 5930005396600, 005396600
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-539-6600 | 36841 ( SWITCH, FLOW ) |
REFERENCE DRAWINGS & PICTURES
RECTANGULAR
Cross Reference | NSN 5930-00-539-6600
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| G-205725-1 | 64959 | AMERICAN TELEPHONE AND TELEGRAPH CO |
| 33-801868-6 | 07397 | GENERAL DYNAMICS ADVANCEDINFORMATION SYSTEMS INC. |
| 33-801868-6 | 04655 | GENERAL DYNAMICS MISSION SYSTEMS,INC. |
| G330050S1 | 24930 | HARRIS CORPORATIONDBA ELECTRONIC SYSTEMS, RADAR |
| 7408010P6 | 03538 | LOCKHEED MARTIN CORPORATIONDIV RMS |
| 340C10058-1 | 94990 | MOTOROLA INC.DBA INTEGRATED INFORMATION SYSTEMS |
| 2A2450 | 49956 | RAYTHEON COMPANYDBA RAYTHEON |
| 2A2450 | 3B150 | RAYTHEON COMPANYDBA RAYTHEON |
| 2450-2A | 82877 | ROTRON INCORPORATEDDBA AMETEK ROTRON |
| 2450 | 82877 | ROTRON INCORPORATEDDBA AMETEK ROTRON |
| 2A2450PT1 | 82877 | ROTRON INCORPORATEDDBA AMETEK ROTRON |
| 2A2450 | 82877 | ROTRON INCORPORATEDDBA AMETEK ROTRON |
| 2ATYPE2450 | 82877 | ROTRON INCORPORATEDDBA AMETEK ROTRON |
| 2AM0DELTYPE2450 | 82877 | ROTRON INCORPORATEDDBA AMETEK ROTRON |
| 041106 | 82877 | ROTRON INCORPORATEDDBA AMETEK ROTRON |
| 035656 | 82877 | ROTRON INCORPORATEDDBA AMETEK ROTRON |
| 020035 | 82877 | ROTRON INCORPORATEDDBA AMETEK ROTRON |
| 8176871 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5930-00-539-6600
| Characteristic | Specifications |
|---|---|
| STYLE DESIGNATOR | RECTANGULAR |
| OVERALL LENGTH | 3.687 INCHES NOMINAL |
| OVERALL HEIGHT | 1.188 INCHES NOMINAL |
| OVERALL WIDTH | 1.531 INCHES NOMINAL |
| BODY LENGTH | 2.000 INCHES NOMINAL |
| NONPILE-UP CONTACT ARRANGEMENT | 1 POLE, DOUBLE THROW, ONE POSITION MOMENTARY |
| CONTACT ACTION STIMULUS | INCREASE |
| CONTACT ADJUSTABILITY | DEACTUATION POINT NOT ADJUSTABLE AND ACTUATION POINT NOT ADJUSTABLE |
| CONTACT STIMULUS RATING | AJ2450.00 ACTUATION POINT NOMINAL AND AJ2250.00 ACTUATION POINT NOMINAL AND AJ2250.00 ACTUATION POINT NOMINAL AND AJ2350.00 ACTUATION POINT NOMINAL AND AJ1600.00 DEACTUATION POINT NOMINAL AND AJ1250.00 DEACTUATION POINT NOMINAL AND AJ1500.00 DEACTUATION POINT NOMINAL AND AJ1550.00 DEACTUATION POINT NOMINAL AND AJ850.00 DIFFERENTIAL POINT NOMINAL |
| MEDIA FOR WHICH DESIGNED | Q$DADF |
| TERMINAL TYPE | TAB, SOLDER LUG |
| MOUNTING METHOD | CLAMP |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | COMMUNICATIONS TERMINAL, SATELLITE AN/GSC=39 9V)1, AIRCRAFT, SOF (AC-130H, MC-130H, EC-130E, HC-130), 485L TACS, TELETYPE, MODEL 28, AIRCRAFT, HERCULES C-130, AIRCRAFT, STRATOLIFTER C-135, AIRCRAFT, EAGLE F-15, SUPPORT EQUIPMENT, B-1 AIRCRAFT, SATELLITE COMMUNICATIONS TERMINAL, AN/GSC-52(V). |