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MRC | Criteria | Characteristic |
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FTLD | Functional Description | ACCEPTS INPUTS FROM THE AIRCRAFT PITOT STATIC SYSTEM, ANGLE OF ATTACK, SENSOR, TEMPERATURE SENSOR AND DUCT PITOT STATIC SENSOR;IT UTILIZES THESE INPUTS TO GENERATE THE COMMANDS NECESSARY TO CONTROL THE VARIABLE ENGINE INLET GEOMETRY DURING ALL FLIGHT CONDITIONS |
FAAZ | Phase | SINGLE |
ATJK | Power Source | EXTERNAL |
CXCY | Part Name Assigned By Controlling Agency | CONTROLLER,ELECTRONIC AIR INLET |
FREQ | Frequency In Hertz | 400 |
CCFF | Terminal Type And Quantity | 2 CONNECTOR, RECEPTACLE |
APXH | Terminal Location | BACK |
RDAL | Reference Data And Literature | T.O. 5F28-2-4 |
FEAT | Special Features | ONE USED PER ENGINE-2 TOTAL FOR F-15 ACFT |
TMDN | Type/Model Designation | DCU-181/A |
MRC | Decoded Requirement | Clear Text Reply |
AGAV | End Item Identification | PW200 ENGINE,F15A/B/C/D |
AFXE | Maximum Voltage Rating In Volts | 115.0 AC |
RTSE | Relationship To Similar Equipment | RSIMILAR 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 AND 6610-01-342-9774 EXCEPTTHE -1798 AND -9774 ARE F-15E ONLY |
Guaranteed on-time |
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Customized and |
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Over 5100 |
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Complete Purchasing |