NSN 6610-01-432-8459
Part Details | FLIGHT INFORMATION PROCESSOR
6610-01-432-8459 A unit which accepts electrical/electronic data such as attitude, altitude, air speed, barometric pressure, and the like, which have been converted by the COMPUTER, AIR DATA from air/pressure signals to electrical/electronic data, as well as signals from a data bus. The data is processed by this unit to prepare for displaying the results on a cathode ray tube or liquid crystal display.
Alternate Parts: 68870241211, 68-870241-211, 21189525, 2118952-5, CPU194A, CPU-194/A, 6610-01-432-8459, 01-432-8459, 6610014328459, 014328459
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | JUN 17, 1996 | 01-432-8459 | 53049 ( PROCESSOR, FLIGHT INFORMATION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6610-01-432-8459
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 68-870241-211 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 2118952-5 | 64547 | HONEYWELL INTERNATIONAL INCDBA HONEYWELL |
| CPU-194/A | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
Technical Data | NSN 6610-01-432-8459
| Characteristic | Specifications |
|---|---|
| INPUT INTELLIGENCE TYPE | AIR PRESSURE AND ANGLE OF ATTACK AND AIR TEMPERATURE AND ALTITUDE, GENERAL DATA |
| INTELLIGENCE INPUT METHOD | E$DAAAE |
| OUTPUT INTELLIGENCE TYPE | AIR DATA |
| POWER SOURCE | EXTERNAL |
| DIRECT CURRENT VOLTAGE RATING IN VOLTS | 26.0 |
| ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115.0 |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | SINGLE |
| SPECIAL FEATURES | THERE ARE 2 DIFFERENT MECHANICAL MOUNTS, 1 USED IN THE EAIC LOCATION AND 1 USED IN THE ADC LOCATION |
| UNPACKAGED UNIT LENGTH | 9.50 INCHES NOMINAL |
| UNPACKAGED UNIT WIDTH | 6.20 INCHES NOMINAL |
| UNPACKAGED UNIT HEIGHT | 6.50 INCHES NOMINAL |
| END ITEM IDENTIFICATION | F-15S |
| FUNCTIONAL 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. |
| TYPE/MODEL DESIGNATION | CPU-194/A |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | AIR DATA PROCESSOR |