Receive a Quick Quote for Part CPU-194-A with NSN 6610-01-432-8458 by Pep West Inc

Mfg Part Number: CPU-194-A	Alternate P/N: CPU194A	Manufacturer: Pep West Inc
NSN : 6610-01-432-8458	NIIN : 014328458	Item Name : Computer Air Data
CAGE Code : 64547	FSC : 6610 Flight Instruments

Thank you for taking an interest in the various military NSN parts and aerospace parts we offer on our website. You have currently taken interest in part number CPU-194-A, a Pep West Inc item produced under CAGE Code 64547. For further identification purposes, part number CPU-194-A is also listed with the NSN 6610014328458, and it is organized under Federal Supply Class (FSC) 6610 Flight Instruments for ease of procural. By filling out and submitting the form provided below, you will be able to receive purchasing options on this item directly from our staff. For us to best tailor our presented solution to your unique needs and restrictions alike, we ask that you please offer our team details like your desired quantity, target pricing, and expected fulfillment timeframe. We can even accommodate many time constraints and limitations that customers may face, so be sure to let us know of any requests when you submit an RFQ form for part number CPU-194-A.

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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

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