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 Computer Air Data. Classified under NSN 6610-01-432-8458, the NIIN of this item is 014328458, its INC is , 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are subject to change until acceptance by ASAP Semiconductor of a binding Purchase Order, and quotations may be withdrawn or revised at the sole discretion of ASAP Semiconductor.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.
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MRC | Criteria | Characteristic |
---|---|---|
AJAF | Unpackaged Unit Length | 9.50 INCHES NOMINAL |
ACUQ | Alternating Current Voltage Rating In Volts | 115 |
FAAZ | Phase | SINGLE |
FREQ | Frequency In Hertz | 400 |
TMDN | Type/Model Designation | CPU194/A |
AJAG | Unpackaged Unit Width | 6.20 INCHES NOMINAL |
AJAH | Unpackaged Unit Height | 6.50 INCHES NOMINAL |
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. |
ACUR | Direct Current Voltage Rating In Volts | 26 |
AXQJ | Intelligence Input Method | AIR OR ELECTRICAL |
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 |
SUPP | Supplementary Features | LTECH 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. |
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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