Mfg Part Number: CPU-194 A | Alternate P/N: CPU194A | Manufacturer: Joint Electronics Type Designation |
NSN : 6610-01-432-8459 | NIIN : 014328459 | Item Name : processor flight information |
CAGE Code : 80058 | FSC : 6610 Flight Instruments |
Thank you for choosing NSN Part CPU-194 A of Hardware and Fasteners for all your operational needs. You have reached our NSN RFQ page which features all of our highly sought-after NSN 6610-01-432-8459 parts and components with Processor Flight Information, manufactured by MFG Joint Electronics Type Designation. Some of these items include part CPU-194 A, and various others, all of which have been vetted for quality assurance and authenticity. At Hardware and Fasteners, we are committed to providing customers quality items that have been sourced from leading manufacturers across the globe. If you find yourself in need of quality parts and components, you have come to the right place.
CPU-194 A part of NSN 6610-01-432-8459 products that we feature by MFG Joint Electronics Type Designation are paired alongside CAGE Code 80058. Hardware and Fasteners uses CAGE Codes, allowing our customers to narrow down our vast catalogs with ease. When you find an item that works for your operations, fill out and submit an RFQ form for your comparisons. As you complete the form, please include target prices, desired quantities, and expected shipping time frames. Within 15 minutes of completion, an account manager will draft a sourcing solution that keeps your unique requirements in mind. Alternatively, you can call or email us directly; we are available 24/7x365!
MRC | Criteria | Characteristic |
---|---|---|
AJAF | Unpackaged Unit Length | 9.50 INCHES NOMINAL |
ACUQ | Alternating Current Voltage Rating In Volts | 115 |
FAAZ | Phase | SINGLE |
TMDN | Type/Model Designation | CPU-194/A |
FTLD | 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. |
AJAG | Unpackaged Unit Width | 6.20 INCHES NOMINAL |
FREQ | Frequency In Hertz | 400 |
AJAH | Unpackaged Unit Height | 6.50 INCHES NOMINAL |
ACUR | Direct Current Voltage Rating In Volts | 26 |
AXQJ | Intelligence Input Method | AIR OR ELECTRICAL |
CXCY | Part Name Assigned By Controlling Agency | AIR DATA PROCESSOR |
AXQH | Input Intelligence Type | AIR PRESSURE AND ANGLE OF ATTACK AND AIR TEMPERATURE AND ALTITUDE, GENERAL DATA |
AXQK | Output Intelligence Type | AIR DATA |
AGAV | End Item Identification | F-15S |
FEAT | Special Features | THERE ARE 2 DIFFERENT MECHANICAL MOUNTS, 1 USED IN THE EAIC LOCATION AND 1 USED IN THE ADC LOCATION |
AWZJ | Power Source | EXTERNAL |
MRC | Decoded Requirement | Clear Text Reply |
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