| AFGA |
OPERATING TEMP RANGE |
-55.0/+125.0 DEG CELSIUS |
| CZEN |
VOLTAGE RATING AND TYPE PER CHARACTERISTIC |
15.5 VOLTS MAXIMUM POWER SOURCE |
| AGAV |
END ITEM IDENTIFICATION |
AIRCRAFT, HORNET F/A-18; AIRCRAFT, F-16; AIRCRAFT, AIRLIFTER C-17A; WASP CLASS LHD; AIRCRAFT, GALAXY C-5; F414 ENGINE (F/A-18 F & G AIRCRAFT); AIRCRAFT, STARLIFTER C-141 |
| TEST |
TEST DATA DOCUMENT |
81349-MIL-M-38510 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL |
| CBBL |
FEATURES PROVIDED |
POSITIVE OUTPUTS AND MONOLITHIC AND HERMETICALLY SEALED AND TRUE/COMPLEMENTARY |
| ADAT |
BODY WIDTH |
0.245 INCHES MINIMUM AND 0.285 INCHES MAXIMUM |
| CQZP |
INPUT CIRCUIT PATTERN |
HEX 1 INPUT |
| ZZZK |
SPECIFICATION/STANDARD DATA |
81349-MIL-M-38510/55 GOVERNMENT SPECIFICATION |
| CQSZ |
INCLOSURE CONFIGURATION |
FLAT PACK |
| CTFT |
CASE OUTLINE SOURCE AND DESIGNATOR |
F-5 MIL-M-38510 |
| AEHX |
MAXIMUM POWER DISSIPATION RATING |
200.0 MILLIWATTS |
| ADAU |
BODY HEIGHT |
0.045 INCHES MINIMUM AND 0.085 INCHES MAXIMUM |
| CSSL |
DESIGN FUNCTION AND QUANTITY |
6 BUFFER, INVERTING |
| CQSJ |
INCLOSURE MATERIAL |
CERAMIC AND GLASS |
| CQWX |
OUTPUT LOGIC FORM |
COMPLEMENTARY-METAL OXIDE-SEMICONDUCTOR LOGIC |
| FEAT |
SPECIAL FEATURES |
WEAPON SYSTEM ESSENTIAL |
| CZEQ |
TIME RATING PER CHACTERISTIC |
345.00 NANOSECONDS MAXIMUM PROPAGATION DELAY TIME, LOW TO HIGH LEVEL OUTPUT AND 225.00 NANOSECONDS MAXIMUM PROPAGATION DELAY TIME, HIGH TO LOW LEVEL OUTPUT |
| ADAQ |
BODY LENGTH |
0.440 INCHES MAXIMUM |
| TTQY |
TERMINAL TYPE AND QUANTITY |
16 FLAT LEADS |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| AFJQ |
STORAGE TEMP RANGE |
-65.0/+175.0 DEG CELSIUS |
| CWSG |
TERMINAL SURFACE TREATMENT |
SOLDER |