AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
For competitive procurement options on part number CPU-194 A from Joint Electronics Type Designation System (CAGE Code 80058), look no further than Just Parts Unlimited. With the form presented on this page, you can submit information on your needs to receive tailored procurement solutions from our staff.
Part Number CPU-194 A Details:
Part number CPU-194 A is manufactured by Joint Electronics Type Designation System and listed with the item name Processor Flight Information. Classified under NSN 6610-01-432-8459, the NIIN of this item is 014328459, its INC is 53049, and its NCB code is 01 (USA).
For organization and identification purposes, this item is listed within the Federal Supply Group (FSG) 66 Instruments and Laboratory Equipment and Class (FSC) 6610 Flight Instruments. These details are important for confirming parts before making a purchase.
Disclaimer: This is a quotation for the goods listed above. This quotation is meant as an estimate and does not reflect a final bill or invoice. All quotations are subject to change until acceptance by ASAP Semiconductor of a binding Purchase Order, and quotations may be withdrawn or revised at the sole discretion of ASAP Semiconductor. This quotation is subject to the ASAP Semiconductor Terms & Conditions available at https://www.asapsemi.com/terms-conditions.aspx . All United States Government and Department of Defense bids are quoted as CAGE code 6RE77 from ASAP Semiconductor’s Anaheim, California facility. Any quotation from ASAP Semiconductor without 6RE77 is void.
How to Get Started on Procurement
| 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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