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| MRC | Criteria | Characteristic |
|---|---|---|
| TMDN | III TYPE/MODEL DESIGNATION | CPU194/A |
| AJAF | III UNPACKAGED UNIT LENGTH | 9.50 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | F-15S |
| AJAH | III UNPACKAGED UNIT HEIGHT | 6.50 INCHES NOMINAL |
| ACUQ | ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115.0 |
| FAAZ | PHASE | SINGLE |
| AWZJ | POWER SOURCE | EXTERNAL |
| SUPP | III SUPPLEMENTARY FEATURES | TECH CHARACTERISTICS: MIL-STD-1750A PROCESSOR, CONTAINS 1553 BUS, BUILT-IN-TEST/3 EXTERNAL FAIL INDICATORS, REQUIRES NO COOLING AIR, PROVIDES PRESSURE SIGNAL OUTPUTS, PROVIDES AIR DATA TO OTHER AIRCRAFT SYSTEMS. |
| FREQ | FREQUENCY IN HERTZ | 400.0 |
| AXQK | OUTPUT INTELLIGENCE TYPE | AIR DATA |
| AXQJ | INTELLIGENCE INPUT METHOD | AIR OR ELECTRICAL |
| AXQH | INPUT INTELLIGENCE TYPE | AIR PRESSURE AND ANGLE OF ATTACK AND AIR TEMPERATURE AND ALTITUDE, GENERAL DATA |
| FTLD | III FUNCTIONAL DESCRIPTION | PROCESSOR ACCEPTS INPUTS FROM AIRCRAFT FREESTREAM PITOT-STATIC PRESSURE SYSTEM, ANGLE OF ATTACK SENSORS, AIRCRAFT TOTAL TEMPERATURE SENSORS, ENGINE AIR INLET DUCT PITOT-STATIC PRESSURE SYSTEM AND THE ALTIMETER BAROMETRIC SETTING. CORRECTED INPUTS ARE USED TO 1) COMPUTE ACCURATE AIR DATA FOR PRIMARY FLIGHT INSTRUMENTS 2) GENERATE COMMANDS NECESSARY TO CONTROL THE VARIABLE ENGINE INLET GEOMETRY, 3) PROVIDE THE AFCS WITH PITOT PRESSURE, STATIC PRESSURE, AND IMPACT PRESSURE. |
| ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 26.0 |
| FEAT | SPECIAL FEATURES | THERE ARE 2 DIFFERENT MECHANICAL MOUNTS, 1 USED IN THE EAIC LOCATION AND 1 USED IN THE ADC LOCATION. |
| AJAG | III UNPACKAGED UNIT WIDTH | 6.20 INCHES NOMINAL |
| CPU-1506-1 | CPU-133 A | CPU-133 A | CPU 1017 |
| CPU-136 A | CPU-133 A | CPU 1017 | CPU-123G B |
| CPU-1504-1 | CPU-123E B | CPU-123E B | CPU-1.4-EB |
| CPU-133 A | CPU-1505-1 | CPU-133 A | CPU-136 A |
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