Part Details | COMPUTER CONTROL
5826-01-248-1752 A control which is an essential part of the central processing unit of a computer. It controls the other basic hardware units in such a manner that all operations are conducted in the correct time and logic sequence. It also prevents the introduction of a new task prior to completion of the task in process. The control comprises an instruction counter, an instruction and index register and comparator.
Alternate Parts: SLZ94391, SLZ9439-1, 5826-01-248-1752, 01-248-1752, 5826012481752, 012481752
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 58 | JAN 18, 1987 | 01-248-1752 | 19592 ( CONTROL, COMPUTER ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5826-01-248-1752
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| SLZ9439-1 | 10639 | AVIONICS SPECIALTIES INC. |
Technical Data | NSN 5826-01-248-1752
| Characteristic | Specifications |
|---|---|
| POWER SOURCE | EXTERNAL |
| TERMINAL TYPE AND QUANTITY | 1 COAXIAL RECEPTACLE |
| TERMINAL LOCATION | BACK |
| CASE MATERIAL | ALUMINUM ALLOY |
| CASE SURFACE TREATMENT | ZINC CHROMATE |
| INCLOSURE TYPE | ENCASED |
| MAXIMUM OVERALL LENGTH | 5.740 INCHES |
| MAXIMUM OVERALL WIDTH | 5.772 INCHES |
| MAXIMUM OVERALL HEIGHT | 2.240 INCHES |
| MOUNTING METHOD | RACK |
| END ITEM IDENTIFICATION | AN/ASQ-141(V) INTEGRATED DUAL FLIGHT DIRECTOR SYSTEM |