| CQSZ |
INCLOSURE CONFIGURATION |
DUAL-IN-LINE |
| ADAQ |
BODY LENGTH |
2.096 INCHES MAXIMUM |
| AFGA |
OPERATING TEMP RANGE |
-55.0/+125.0 DEG CELSIUS |
| CQZP |
INPUT CIRCUIT PATTERN |
12 INPUT |
| AFJQ |
STORAGE TEMP RANGE |
-65.0/+150.0 DEG CELSIUS |
| CQSJ |
INCLOSURE MATERIAL |
CERAMIC |
| CZEN |
VOLTAGE RATING AND TYPE PER CHARACTERISTIC |
7.0 VOLTS MAXIMUM POWER SOURCE |
| CSSL |
DESIGN FUNCTION AND QUANTITY |
1 INTEGRATOR |
| ADAU |
BODY HEIGHT |
0.165 INCHES MINIMUM AND 0.210 INCHES MAXIMUM |
| CBBL |
FEATURES PROVIDED |
HERMETICALLY SEALED AND W/CLOCK AND BURN IN AND POSITIVE OUTPUTS |
| CTFT |
CASE OUTLINE SOURCE AND DESIGNATOR |
D-5 MIL-M-38510 |
| FEAT |
SPECIAL FEATURES |
WEAPON SYSTEM ESSENTIAL |
| TEST |
TEST DATA DOCUMENT |
96906-MIL-STD-883 STANDARD (INCLUDES INDUSTRY OR ASSOCIATION STANDARDS, INDIVIDUAL MANUFACTUREER STANDARDS, ETC.). |
| ADAT |
BODY WIDTH |
0.510 INCHES MINIMUM AND 0.620 INCHES MAXIMUM |
| CQWX |
OUTPUT LOGIC FORM |
EMITTER-COUPLED LOGIC AND TRANSISTOR-TRANSISTOR LOGIC |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| TTQY |
TERMINAL TYPE AND QUANTITY |
40 PRINTED CIRCUIT |
| AGAV |
END ITEM IDENTIFICATION |
F-16 AIRCRAFT. F100-PW-200 (F-16 A/B/C/D) AIRCRAFT ENGINE. |
| CWSG |
TERMINAL SURFACE TREATMENT |
SOLDER |