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National Stock Number:
6610-01-308-1859
Federal Supply Class:
6610
National Item Identification Number:
013081859
Description:
COMPUTER,AIR DATA
Detail:
A COMPUTER SPECIFICALLY DESIGNED TO CONVERT BASIC AIR DATA INPUT SIGNALS INTO ELECTRICAL OUTPUT SIGNALS REPRESENTING THE NECESSARY FLIGHT PARAMETERS SUCH AS PRESSURE ALTITUDE, MACH NUMBER, AIRSPEED, AND IMPACT PRESSURE. SEE ALSO COMPUTER, AIR SPEED; COMPUTER, ALTIMETER-PRESSURE; COMPUTER, ALTITUDE; COMPUTER, MACH NUMBER; COMPUTER, PRESSURE-ALTITUDE; COMPUTER, TRUE WIND DIRECTION AND INTENSITY; AND COMPUTER, ZONE WIND.
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Manufacturer Information:
| 16VC004-4 | 81755 | LOCKHEED MARTIN CORPORATION | | 4025116-907 | 07187 | HONEYWELL INTERNATIONAL INC. |
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Techincal Specification:
| INPUT INTELLIGENCE TYPE | AIR PRESSURE AND | | AIR TEMPERATURE AND | | ANGLE OF ATTACK AND | | ALTITUDE, GENERAL DATA | | INTELLIGENCE INPUT METHOD | AIR OR | | ELECTRICAL | | OUTPUT INTELLIGENCE TYPE | ALTITUDE AND | | ASTRO TRACKER AND | | TRUE AIR SPEED AND | | ANGLE OF ATTACK AND | | MACH NUMBER AND | | TEMPERATURE AND | | AIR DENSITY AND | | MAPS COORDINATES VOLTAGE | | POWER SOURCE | EXTERNAL | | ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115.0 | | FREQUENCY IN HERTZ | 400.0 | | PHASE | SINGLE | | TERMINAL TYPE | CONNECTOR, PLUG | | TERMINAL QUANTITY | 5 | | CONNECTOR MANUFACTURER PART NUMBER | MS27497E20B35SD AND | | MS27497E20B35SC AND | | MS27497E20B35SB AND | | MS27847E20B35S AND | | MS27497E14B35PA | | CONNECTOR MANUFACTURER CODE | 81349 | | TERMINAL LOCATION | FRONT | | MOUNTING TYPE | RACK | | CRITICALITY CODE JUSTIFICATION | AGAV | | UNPACKAGED UNIT LENGTH | 14.910 INCHES NOMINAL | | UNPACKAGED UNIT WIDTH | 6.200 INCHES NOMINAL | | FUNCTIONAL DESCRIPTION | THIS IS A DEVICE CONTAING PRESSURE TRANSDUCERS, INTERFACE ELECTRONICS CIRCUITRY, AND A DIGITAL COMPUTER. IT RECIEVES INPUTS OF PITOT STATIC PRESSURE, ANGLE OF ATTACK, TOTAL TEMPERATURE, AND BAROMETRIC SETTING. THE DEVICE CONVERTS THESE INPUTS INTO DIGITAL DATA FOR PROCESSING. THE DIGITAL COMPUTER IN THE DEVICE CORRECTS FOR ERRORS CAUSED BY LOCAL FLOW AND CONVERTS THE DATA INTO DESIRED PARAMETERS. THIS PROCESSED AIR DATA OF ALTITUDE, AIR SPEED, ANGLE OF ATTACK, MACH, TEMPERATURE, PRESSURE PARAMETER RATES AND VALIDITY AND SWITCH DISCRETES ARE PROVIDED TO OTHER AIRCRAFT SUBSYSTEMS VIA DIGITAL AND ANALOG OUTPUTS. | | REFERENCE DATA AND LITERATURE | 5F5-4-28-4 | | THE MANUFACTURERS DATA | | | MANUFACTURERS CODE | 07187 | | DESIGN CONTROL REFERENCE | 4025116-907 |
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