| AFGA |
OPERATING TEMP RANGE |
-55.0/+125.0 DEG CELSIUS |
| FEAT |
SPECIAL FEATURES |
WEAPON SYSTEM ESSENTIAL AUTOPILOT FLIGHT CONTROL COMPUTER FOR F-15 AND ASSOCIATED TEST EQUIPMENT |
| AGAV |
END ITEM IDENTIFICATION |
F-15 EAGLE, C-141 STARLIFTER AIRCRAFT. |
| CZEN |
VOLTAGE RATING AND TYPE PER CHARACTERISTIC |
-1.5 VOLTS MINIMUM POWER SOURCE AND 5.5 VOLTS MAXIMUM POWER SOURCE |
| CQSZ |
INCLOSURE CONFIGURATION |
FLAT PACK |
| ADAQ |
BODY LENGTH |
0.350 INCHES MINIMUM AND 0.400 INCHES MAXIMUM |
| AFJQ |
STORAGE TEMP RANGE |
-65.0/+150.0 DEG CELSIUS |
| CZEQ |
TIME RATING PER CHACTERISTIC |
45.00 NANOSECONDS MAXIMUM PROPAGATION DELAY TIME, LOW TO HIGH LEVEL OUTPUT AND 52.00 NANOSECONDS MAXIMUM PROPAGATION DELAY TIME, HIGH TO LOW LEVEL OUTPUT |
| ADAT |
BODY WIDTH |
0.200 INCHES MINIMUM AND 0.300 INCHES MAXIMUM |
| CSSL |
DESIGN FUNCTION AND QUANTITY |
1 COUNTER, BINARY |
| CBBL |
FEATURES PROVIDED |
MEDIUM SPEED AND RESETTABLE AND MEDIUM POWER AND POSITIVE OUTPUTS AND MONOLITHIC AND HERMETICALLY SEALED AND W/ENABLE |
| ADAU |
BODY HEIGHT |
0.008 INCHES MINIMUM AND 0.100 INCHES MAXIMUM |
| TEST |
TEST DATA DOCUMENT |
89954-144A5558 DRAWING (THIS IS THE BASIC GOVERNING DRAWING, SUCH AS A CONTRACTOR DRAWING, ORIGINAL EQUIPMENT MANUFACTURER DRAWING, ETC.; EXCLUDES ANY SPECIFICATION, STANDARD OR OTHER DOCUMENT THAT MAY BE REFERENCED IN A BASIC GOVERNING DRAWING) |
| CQSJ |
INCLOSURE MATERIAL |
CERAMIC AND GLASS |
| CQWX |
OUTPUT LOGIC FORM |
TRANSISTOR-TRANSISTOR LOGIC |
| TTQY |
TERMINAL TYPE AND QUANTITY |
16 FLAT LEADS |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| CQZP |
INPUT CIRCUIT PATTERN |
10 INPUT |
| CTFT |
CASE OUTLINE SOURCE AND DESIGNATOR |
-0-004-AG JOINT ELECTRON DEVICE ENGINEERING COUNCIL |
| CWSG |
TERMINAL SURFACE TREATMENT |
SOLDER |
| AEHX |
MAXIMUM POWER DISSIPATION RATING |
320.0 MILLIWATTS |