Part Details | ELECTRONIC AIR INLET CONTROLLER
6610-00-122-6625 A device which accepts inputs from various sensors and regulates air flow to the engine intakes by opening and closing the inlet ramps in order to let more or less air in to ensure efficient operation.
Alternate Parts: ED74190014, ED741900-14, DCU181A, DCU-181/A, 6610-00-122-6625, 00-122-6625, 6610001226625, 001226625
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | JAN 30, 1975 | 00-122-6625 | 53017 ( CONTROLLER, AIR INLET, ELECTRONIC ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6610-00-122-6625
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| ED741900-14 | 73030 | HAMILTON SUNDSTRAND CORPORATION |
| DCU-181/A | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
Technical Data | NSN 6610-00-122-6625
| Characteristic | Specifications |
|---|---|
| POWER SOURCE | EXTERNAL |
| MAXIMUM VOLTAGE RATING IN VOLTS | 115.0 AC |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | SINGLE |
| TERMINAL TYPE AND QUANTITY | 2 CONNECTOR, RECEPTACLE |
| TERMINAL LOCATION | BACK |
| SPECIAL FEATURES | ONE USED PER ENGINE-2 TOTAL FOR F-15 ACFT |
| END ITEM IDENTIFICATION | PW200 ENGINE,F15A/B/C/D |
| 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 |
| TYPE/MODEL DESIGNATION | DCU-181/A |
| RELATIONSHIP TO SIMILAR EQUIPMENT | SIMILAR TO 6610-01-223-8179, EACHARE USED ON F-15A/B/C/D, BUT -8179 IS USED W/PW220 ENGINE AND -6625 IS USED WITH PW200 ENGINE;ALSO SIMILAR TO 6610-01-247-1798 & 6610-01-342-9774 EXCEPTTHE -1798 & -9774 ARE F-15E ONLY |
| REFERENCE DATA AND LITERATURE | T.O. 5F28-2-4 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CONTROLLER,ELECTRONIC AIR INLET |