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HomeNSNInstruments and Laboratory EquipmentFlight Instruments2118952-5 NSN 6610-01-432-8459 - 822f3665

2118952-5 NSN 6610-01-432-8459 - 822f3665

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NSN 6610-01-432-8459 - (6610014328459) Technical Details :

MRCNameDetails
ACUQALTERNATING CURRENT VOLTAGE RATING IN VOLTS115.0
ACURDIRECT CURRENT VOLTAGE RATING IN VOLTS26.0
AGAVEND ITEM IDENTIFICATIONF-15S
AJAFUNPACKAGED UNIT LENGTH9.50 INCHES NOMINAL
AJAGUNPACKAGED UNIT WIDTH6.20 INCHES NOMINAL
AJAHUNPACKAGED UNIT HEIGHT6.50 INCHES NOMINAL
AWZJPOWER SOURCEEXTERNAL
AXQHINPUT INTELLIGENCE TYPE"AIR PRESSURE AND ANGLE OF ATTACK AND AIR TEMPERATURE AND ALTITUDE, GENERAL DATA"
AXQJINTELLIGENCE INPUT METHODAIR OR ELECTRICAL
AXQKOUTPUT INTELLIGENCE TYPEAIR DATA
CXCYPART NAME ASSIGNED BY CONTROLLING AGENCYAIR DATA PROCESSOR
FAAZPHASESINGLE
FEATSPECIAL FEATURES"THERE ARE 2 DIFFERENT MECHANICAL MOUNTS, 1 USED IN THE EAIC LOCATION AND 1 USED IN THE ADC LOCATION"
FREQFREQUENCY IN HERTZ400.0
FTLDFUNCTIONAL 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."
TMDNTYPE/MODEL DESIGNATIONCPU-194/A

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