NSN 6610-01-303-4272
Part Details | AIR DATA COMPUTER
6610-01-303-4272 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: CPU163A, CPU-163/A, 8508700925, 8508700-925, 8508700924, 8508700-924, 8508700923, 8508700-923, 8508700921, 8508700-921, 6610-01-303-4272, 01-303-4272, 6610013034272, 013034272
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | JUN 30, 1989 | 01-303-4272 | 30742 ( COMPUTER, AIR DATA ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6610-01-303-4272
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CPU-163/A | 07878 | AERONAUTICAL AND SUPPORT EQUIPMENTTYPE/ASETDS/AFLCMC/EZSC |
| 8508700-925 | 07187 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 8508700-924 | 07187 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 8508700-923 | 07187 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 8508700-921 | 07187 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 6610-01-303-4272
| Characteristic | Specifications |
|---|---|
| INPUT INTELLIGENCE TYPE | AIR PRESSURE AND AIR TEMPERATURE AND ALTITUDE AND AIRSPEED |
| INTELLIGENCE INPUT METHOD | E$DAAAE |
| OUTPUT INTELLIGENCE TYPE | TRUE AIR SPEED AND MACH NUMBER AND PRESSURE ALTITUDE AND TEMPERATURE |
| POWER SOURCE | EXTERNAL |
| ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115.0 |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | SINGLE |
| TERMINAL TYPE | CONNECTOR, RECEPTACLE |
| TERMINAL QUANTITY | 2 |
| CONNECTOR MANUFACTURER PART NUMBER | DPX2NA-67318-0156 |
| CONNECTOR MANUFACTURER CODE | 71468 |
| TERMINAL LOCATION | BACK |
| MOUNTING TYPE | RACK |
| UNPACKAGED UNIT LENGTH | 12.620 INCHES NOMINAL |
| UNPACKAGED UNIT WIDTH | 4.880 INCHES NOMINAL |
| UNPACKAGED UNIT HEIGHT | 7.620 INCHES NOMINAL |
| END ITEM IDENTIFICATION | C-17A AIRFRAME |
| FUNCTIONAL DESCRIPTION | RECIEVES INPUTS FROM THE PITOT STATIC SUB-SYSTEM, TOTAL AIR TEMPERATURE PROBES, BAROMETER SETTING, AND FROM THE AIRCRAFT PROPULSION DATA MANAGEMENT COMPUTER. THIS DATA IS USED BY THE AIR DATA COMPUTER TO COMPUTE PARAMETERS SUCH AS TRUE AIRSPEED, MACH NUMBER, PRESSURE ALTITUDE, AND STATIC AIR TEMPERATURE WHICH ARE OUTPUT ON 1553 BUSES. |
| TYPE/MODEL DESIGNATION | CPU-163/A |
| REFERENCE DATA AND LITERATURE | 5N5-13-24-4 |
