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MRC | Criteria | Characteristic |
---|---|---|
SR-5 | DESIGN CONTROL REFERENCE | ED741900-16 |
RTSE | III RELATIONSHIP TO SIMILAR EQUIPMENT | SIMILAR TO 6610-01-342-9774, 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 |
FAAZ | PHASE | SINGLE |
RDAL | III REFERENCE DATA AND LITERATURE | T.O. 5F28-2-4 |
SR-5 | MANUFACTURERS CODE | 73030 |
FTLD | III 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 |
AFXE | MAXIMUM VOLTAGE RATING IN VOLTS | 115.0 AC |
SR-5 | THE MANUFACTURERS DATA | |
FREQ | FREQUENCY IN HERTZ | 400.0 |
ATJK | POWER SOURCE | EXTERNAL |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | CONTROLLER,ELECTRONIC AIR INLET |
FEAT | SPECIAL FEATURES | ONE USED PER ENGINE-2 TOTAL FOR F-15 ACFT |
TMDN | III TYPE/MODEL DESIGNATION | DCU-181/A |
APXH | TERMINAL LOCATION | BACK |
CCFF | TERMINAL TYPE AND QUANTITY | 2 CONNECTOR, RECEPTACLE |
DCU-100 | DCU-272 A | DCU-272 A | DCU-272 A |
DCU-100 | DCU-263 A | DCU-263 A | DCU-267 A |
DCU-270 A | DCU-150 | DCU-267 A | DCU-177 E |
DCU-270 A | DCU-150 | DCU-251 A | DCU-251 A |
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