7025015787945 | 5985014980332 |
5985013243461 | 1510000808414 |
7025015588807 | 7010015006979 |
5905000000136 | 6135014938794 |
7025014906701 | 6150012089751 |
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Our website offers parametric search capabilities allowing our customers to search for parts through a number of filters, one of which is by National Stock Number, or NSN. A National Stock Number is an identifier applied to any item of supply that is repeatedly procured, stocked, stored, issued, and used throughout the federal supply system. ASAP Inventory has a broad selection of NSN parts CPU-194 A such as 6610014328458 from manufacturers like Honeywell International Inc. To begin the purchasing process immediately, submit an RFQ today.
MRC | Criteria | Characteristic |
---|---|---|
AJAG | UNPACKAGED UNIT WIDTH | 6.20 INCHES NOMINAL |
ACUQ | ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115 |
FAAZ | PHASE | SINGLE |
ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 26 |
AXQH | INPUT INTELLIGENCE TYPE | AIR PRESSURE AND ANGLE OF ATTACK AND AIR TEMPERATURE AND ALTITUDE, GENERAL DATA |
AXQK | OUTPUT INTELLIGENCE TYPE | AIR DATA |
FEAT | SPECIAL FEATURES | THERE ARE 2 DIFFERENT MECHANICAL MOUNTS, 1 USED IN THE EAIC LOCATION AND 1 USED IN THE ADC LOCATION. |
TMDN | TYPE/MODEL DESIGNATION | CPU194/A |
AJAF | UNPACKAGED UNIT LENGTH | 9.50 INCHES NOMINAL |
AJAH | UNPACKAGED UNIT HEIGHT | 6.50 INCHES NOMINAL |
AWZJ | POWER SOURCE | EXTERNAL |
SUPP | 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 |
AXQJ | INTELLIGENCE INPUT METHOD | AIR OR ELECTRICAL |
FTLD | 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. |
AGAV | END ITEM IDENTIFICATION | F-15S |
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