MICROCIRCUIT,LINEAR
Microcircuits, Electronic
Application: ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); COUNTERMEASURE SET AN/SLQ-32; TRAINER, B-1B AIRCRAFT; TEST STATION, OQ-290(V)MSM; MISSILE, TOMAHAWK; SUPPORT EQUIPMENT, B-1 AIRCRAFT; SUPPORT EQUIPMENT, B-52 AIRCRAFT; MISSILE, AIR-TO-AIR, PHOENIX (AIM-54); AIRCRAFT, ( AC-130H, MC-130H, EC-130E, H
Technical characteristics
21 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| AFJQ | STORAGE TEMP RANGE | CELSIUS -65.0 TO 150.0 |
| CWSG | TERMINAL SURFACE TREATMENT | SOLDER |
| CZEN | VOLTAGE RATING AND TYPE PER CHARACTERISTIC | VOLTS MINIMUM POWER SOURCE -20.0 AND VOLTS MAXIMUM POWER SOURCE 20.0 |
| CSSL | DESIGN FUNCTION AND QUANTITY | RECEIVER, LINE DIFFERENTIAL 2 |
| ADAU | BODY HEIGHT | INCHES MINIMUM 0.140 AND INCHES MAXIMUM 0.185 |
| AEHX | MAXIMUM POWER DISSIPATION RATING | MILLIWATTS 400.0 |
| AFGA | OPERATING TEMP RANGE | CELSIUS -55.0 TO 125.0 |
| TEST | TEST DATA DOCUMENT | 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", "AVERAGE", "NOMINAL", ETC.). 81349--IL---38510 |
| TTQY | TERMINAL TYPE AND QUANTITY | PRINTED CIRCUIT 16 |
| AGAV | END ITEM IDENTIFICATION | ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); COUNTERMEASURE SET AN/SLQ-32; TRAINER, B-1B AIRCRAFT; TEST STATION, OQ-290(V)MSM; MISSILE, TOMAHAWK; SUPPORT EQUIPMENT, B-1 AIRCRAFT; SUPPORT EQUIPMENT, B-52 AIRCRAFT; MISSILE, AIR-TO-AIR, PHOENIX (AIM-54); AIRCRAFT, ( AC-130H, MC-130H, EC-130E, H |
| CQSJ | INCLOSURE MATERIAL | CERAMIC AND GLASS |
| CQSZ | INCLOSURE CONFIGURATION | DUAL-IN-LINE |
| CQZP | INPUT CIRCUIT PATTERN | DUAL 5 INPUT |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| CTFT | CASE OUTLINE SOURCE AND DESIGNATOR | MIL-M-38510 D-2 |
| ADAT | BODY WIDTH | INCHES MINIMUM 0.220 AND INCHES MAXIMUM 0.310 |
| ZZZK | SPECIFICATION/STANDARD DATA | GOVERNMENT SPECIFICATION 81349--IL---38510 TO 104 |
| CZEQ | TIME RATING PER CHACTERISTIC | NANOSECONDS MAXIMUM PROPAGATION DELAY TIME, LOW TO HIGH LEVEL OUTPUT 75.00 AND NANOSECONDS MAXIMUM PROPAGATION DELAY TIME, HIGH TO LOW LEVEL OUTPUT 75.00 |
| FEAT | SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL; DESIGN ANALYSIS |
| NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| ADAQ | BODY LENGTH | INCHES MAXIMUM 0.896 |
Supersedes
This item replaces cancelled NIINs 005347202 · 009852178 · 010383355 · 010426533 · 010467171 · 010418056 · 010383368 · 010451868 · 010341495 · 010850373 · 011025873 · 011526957 · 011227627 · 011664970 · 011813097 · 011928405. An older drawing citing one of those numbers resolves here.