| FREQUENCY IN HERTZ | 400.0 |
| FUNCTIONAL DESCRIPTION | ACCEPTS INPUTS FROM THE AIRCRAFT PITOT STATIC SYSTEM, ANGLE OF ATTACK, SENSOR, TEMPERATURE SENSOR & DUCT PITOT STATIC SENSOR;IT UTILIZES THESE INPUTS TO GENERATE THE COMMANDS NECESSARY TO CONTROL THE VARIABLE ENGINE INLET GEOMETRY DURING ALL FLIGHT CONDITIONS |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CONTROLLER,ELECTRONIC AIR INLET |
| MAXIMUM VOLTAGE RATING IN VOLTS | 115.0 AC |
| PHASE | SINGLE |
| POWER SOURCE | EXTERNAL |
| REFERENCE DATA AND LITERATURE | T.O. 5F28-2-4 |
| RELATIONSHIP TO SIMILAR EQUIPMENT | SIMILAR TO 6610-01-247-1798, EACHARE USED ON F-15E ONLY & MUST NOT BE USED TOGETHER ON THE SAME ACFT,USE 2 -1798 OR 2 -9774S NOT ONE OF EACH;ALSO SIMILAR TO 6610-00-122-6625 & 6610-01-223-8179 EXCEPT THEY ARE F-15A/B/C/D ONLY |
| SPECIAL FEATURES | ONE USED PER ENGINE-2 TOTAL FOR F-15 ACFT |
| TYPE/MODEL DESIGNATION | DCU-181/A |
| TERMINAL LOCATION | BACK |
| TERMINAL TYPE AND QUANTITY | 2 CONNECTOR, RECEPTACLE |