"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"
RDAL
REFERENCE DATA AND LITERATURE
T.O. 5F28-2-4
RTSE
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"