Mfg Part Number: CPU-194 A
Alternate P/N: CPU194A
NSN : 6610-01-432-8458
NIIN : 014328458
CAGE Code : 64547
Manufacturer: Honeywell International Inc
Item Name : Computer Air Data
FSC : 6610 Flight Instruments
In our inventory, we have more than two billion new and obsolete NSN part like CPU-194 A. Aviation Sphere can offer an impressive selection of NSN parts. This includes parts like CPU-194 A Computer Air Data from manufacturer Honeywell International Inc and many more, all of which are available with short lead times and competitive prices. For parts not in our inventory, our dedicated account managers can help you track them down through our international supply chain network that extends across the United States, Canada, and the United Kingdom. Furthermore, Aviation Sphere is an AS9120B, ISO 9001:2015, and FAA AC 0056B accredited business, as well as the only independent distributor with a strict No China Sourcing Pledge, allowing us to ensure that each part part like CPU-194 A, you purchase from us is fully traceable or comes directly from its manufacturer.
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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 |
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