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HomeNSNInstruments and Laboratory EquipmentFlight Instruments2118952-1 NSN 6610-01-432-8458 - 7d8a4e66

2118952-1 NSN 6610-01-432-8458 - 7d8a4e66

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NSN 6610-01-432-8458 - (6610014328458) 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
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"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."
SUPPSUPPLEMENTARY FEATURES"TECH 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."
TMDNTYPE/MODEL DESIGNATIONCPU194/A

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