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MRC | Criteria | Characteristic |
---|---|---|
AJAG | III UNPACKAGED UNIT WIDTH | 6.20 INCHES NOMINAL |
AXQH | INPUT INTELLIGENCE TYPE | AIR PRESSURE AND ANGLE OF ATTACK AND AIR TEMPERATURE AND ALTITUDE, GENERAL DATA |
SR-5 | DESIGN CONTROL REFERENCE | 2118952-5 |
FREQ | FREQUENCY IN HERTZ | 400.0 |
FAAZ | PHASE | SINGLE |
SR-5 | THE MANUFACTURERS DATA | |
AJAF | III UNPACKAGED UNIT LENGTH | 9.50 INCHES NOMINAL |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | AIR DATA PROCESSOR |
AGAV | III END ITEM IDENTIFICATION | F-15S |
SR-5 | MANUFACTURERS CODE | 64547 |
AXQK | OUTPUT INTELLIGENCE TYPE | AIR DATA |
AXQJ | INTELLIGENCE INPUT METHOD | AIR OR ELECTRICAL |
TMDN | III TYPE/MODEL DESIGNATION | CPU-194/A |
ACUQ | ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115.0 |
ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 26.0 |
FTLD | III FUNCTIONAL DESCRIPTION | THE PROCESSOR ACCEPTSINPUTS FROM THE AIRCRAFT FREE STREAM PITOT-STATIC PRESSURE SYSTEM, ANGLE OF ATTACK SENSORS, AIRCRAFT TOTAL TEMPERATURE SENSORS, NGINE AIR INLET DUCT PITOT-STATIC PRESSURE SYSTEM, AND ALTIMETER BAROMETRIC SETTING. DS NECESSARY TO CONTROL THE VARIABLE ENGINGE INLET GEOMETRY 3) PROVIDE THE AFCS WITH PITOT PRESSURE, STATIC PRESSURE AND IMPACT PRESSURE.SUPPGTECH CHARACTERISTICS: MILSTD-1750A PROCESSOR, CONTAINS 1553 BUS, BUILT-IN-TEST/3 EXTERNAL FAIL INDICATORS, REQUIRES NO COOLING AIR, PROVIDES PRESSURE SIGNAL OUTPUTS, CONTROLS ENGINE INTAKE AIR FLOW, PROVIDES AIR DATA TO OTHER AIRCRAFT SYSTEMS. |
AWZJ | POWER SOURCE | EXTERNAL |
FEAT | SPECIAL FEATURES | THERE ARE 2 DIFFERENT MECHANICAL MOUNTS, 1 USED IN THE EAIC LOCATION AND 1 USED IN THE ADC LOCATION |
AJAH | III UNPACKAGED UNIT HEIGHT | 6.50 INCHES NOMINAL |
68 00 4225 | 68 00 8475 | 68-000123-001 | 68-0.25 |
68-000123-001 | 68-00-3075 | 68-00-3275 | 68-000568-010 |
68-00009-1 | 68-000568-010 | 68-00-C650W | 68-000123-002 |
68-00009-1 | 68-000123-001 | 68 00027 024 | 68-000583-001 |
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