Mfg Part Number: CPU-194-A | Alternate P/N: CPU194A | Manufacturer: The Boeing Company |
NSN : 6610-01-432-8459 | Item Name : processor flight in | CAGE Code : 76301 |
FSC : 6610 Flight Instruments |
Thank you for your interest in the Processor Flight In parts we have in stock on Integrated Electronics Parts. This particular The Boeing Company item is listed alongside the NSN 6610-01-432-8459 and part number CPU-194-A, allowing you to locate it quickly and easily. This item is currently in stock, so we encourage you to take advantage of our Instant RFQ service to acquire a competitive quote for NSN 6610-01-432-8459 and part number CPU-194-A. With team members on standby to answer any one of your questions, responses to quote requests or inquiries are completed in as little as 15 minutes.
Take your time to explore our ever-expanding catalogs and you will find that the NSN 6610-01-432-8459 can be found listed under CAGE Code 76301. However, we carry an array of other NSN all of which have been sourced from trusted distributors like The Boeing Company. Get started with the procurement process by requesting a quote on part number CPU-194-A. Please include all of your part requirements and see how Integrated Electronics Parts can serve as your go-to sourcing solution. For additional questions, call or email us directly; we are ready to help you meet your operational deadlines however necessary.
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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