NSN 6625-01-482-7561
Part Details | FAULT LOCATING INDICATOR
6625-01-482-7561 An electrically activated item specifically designed to indicate the occurrence of a malfunction in a component of an electronic set, central or system. It may indicate the malfunction by a pop-out button (e.g. ground fault interrupt outlets) or color change by emitted light or displayed in a window. The indicator may utilize a "push to test" button. It does not make quantitative or qualitative tests such a provided by test sets.
Alternate Parts: 200027372, 17G5737741, 17G573774-1, 200027372, 6625-01-482-7561, 01-482-7561, 6625014827561, 014827561
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | MAR 01, 2001 | 01-482-7561 | 60639 ( INDICATOR, FAULT LOCATING ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6625-01-482-7561
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 200027372 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 17G573774-1 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 200027372 | 98747 | OGDEN AIR LOGISTICS CENTER |
Technical Data | NSN 6625-01-482-7561
| Characteristic | Specifications |
|---|---|
| CASE MATERIAL | PLASTIC |
| CURRENT TYPE | AC |
| AC VOLTAGE RATING | 90.0 VOLTS MINIMUM AND 260.0 VOLTS MAXIMUM |
| PHASE | A$C |
| FREQUENCY RATING | 50.0 HERTZ MINIMUM AND 400.0 HERTZ MAXIMUM |
| LENGTH | 7.750 INCHES NOMINAL |
| WIDTH | 7.500 INCHES NOMINAL |
| HEIGHT | 6.500 INCHES NOMINAL |
| SPECIAL FEATURES | ITENS SUPPLIED: INTERFACE BOX (SIB) 1; TEST CABLE (TC-1, 30FT) 1; CROSSWIRE TEST CABLE (TC-2, 8FT) 1; 9 TO 25 PIN ADAPTER 1; SELF-TEST ADAPTERS (ST1, ST2) 2; ADAPTER CABLES (1-25) 23; 9 PIN SERIAL PC INTERFACE CABLE 1; AC POWER CORD 1; CARRYING CASE 1; ADAPTER CASES 2; TOTAL WEIGHT 9 LBS; OTHER REQUIREMENTS 486 IBM PC COMPATIBLE (PENTIUM PREFERRED); 8 MB RAM; HARD DRIVE (W/ AT LEAST 40 MB FREE); WINDOWS COMPATIBLE; SERIAL PORT (RS-232C); PARALLEL PORT (OPT OF R PRINTING REPORTS); SCREEN RESOLUTION: 640X480/800X600 OR HIGHER PREFERRED; ITEM HAS SOFTWARE UPDATE FOR TESTING THE MULTIPLEX DATA BUS IN THE C-17 AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | MULTIPLEX BUS FAULT ISOLATOR |