Request a Quote for NSN 6610-01-432-8458 with Part Number CPU-194-A by Joint Electronics Type Designation

Mfg Part Number: CPU-194-A	Alternate P/N: CPU194A	Manufacturer: Joint Electronics Type Designation
NSN : 6610-01-432-8458	Item Name : computer air data	CAGE Code : 80058
FSC : 6610 Flight Instruments

Thank you for your interest in the Computer Air Data parts we have in stock on Integrated Electronics Parts. This particular Joint Electronics Type Designation item is listed alongside the NSN 6610-01-432-8458 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 6610-01-432-8458 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.

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Take your time to explore our ever-expanding catalogs and you will find that the NSN 6610-01-432-8458 can be found listed under CAGE Code 80058. However, we carry an array of other NSN all of which have been sourced from trusted distributors like Joint Electronics Type Designation. 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.

Characteristics Data of NSN 6610-01-432-8458, 6610014328458

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