We’re pleased to announce that CPU-194 A (Computer Air Data, NSN: 6610-01-432-8458) is now in stock and ready for immediate quoting. This component, manufactured by Joint Electronics Type Designation System (CAGE Code: 80058), is classified under NIIN 01-432-8458 and NCB Code 01 (USA), with additional categorization under FSG 66 Instruments and Laboratory Equipment/FSC 6610 Flight Instruments and INC . Our team can provide same-day shipping for urgent requirements.
To receive your competitive quote within 15 minutes, simply complete our RFQ form part CPU-194 A, ensuring all required fields are filled. Our streamlined process guarantees fast, no-obligation pricing so you can secure your supply of CPU-194 A without delay. Contact us today to meet your procurement needs efficiently
ASAP Part Services, a trusted subsidiary of ASAP Semiconductor, is a premier distributor of Joint Electronics Type Designation System components—specializing in obsolete and hard-to-find parts. As an AS9120B, ISO 9001:2015, and FAA AC 0056B certified supplier, we adhere to the highest industry standards under the Aviation Suppliers Association (ASA). Our global network spans 5,000+ top manufacturers, ensuring access to over 2 billion unique parts for critical needs.
With strategically located shipping centers in California, we offer rapid same-day or next-day delivery on in-stock items like CPU-194 A. Whether you're sourcing rare components or need expedited logistics, we provide reliable solutions to keep your operations moving forward.
| 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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