NSN 6610-01-308-1859
Part Details | AIR DATA COMPUTER
6610-01-308-1859 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.
Alternate Parts: 4025116907, 4025116-907, 16VC0044, 16VC004-4, 6610-01-308-1859, 01-308-1859, 6610013081859, 013081859
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | SEP 23, 1989 | 01-308-1859 | 30742 ( COMPUTER, AIR DATA ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6610-01-308-1859
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4025116-907 | 07187 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 16VC004-4 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 6610-01-308-1859
| Characteristic | Specifications |
|---|---|
| INPUT INTELLIGENCE TYPE | AIR PRESSURE AND AIR TEMPERATURE AND ANGLE OF ATTACK AND ALTITUDE, GENERAL DATA |
| INTELLIGENCE INPUT METHOD | E$DAAAE |
| 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 | AMS27497E20B35SD$$AMS27497E20B35SC$$AMS27497E20B35SB$$AMS27847E20B35S$$AMS27497E14B35PA |
| CONNECTOR MANUFACTURER CODE | 81349 |
| TERMINAL LOCATION | FRONT |
| MOUNTING TYPE | RACK |
| UNPACKAGED UNIT LENGTH | 14.910 INCHES NOMINAL |
| UNPACKAGED UNIT WIDTH | 6.200 INCHES NOMINAL |
| END ITEM IDENTIFICATION | F-16A/B/C/D |
| 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 |
