TM 1-1520-238-T-7 Change 7 11–185 11–24. DASE – WIRING INTERCONNECT DIAGRAM (PITCH) (BUCS DEACTIVATED) (cont) 11–24 J912 P912 P459 B10 B9 B15 J459 B14 B8 B9 J2 P686 121 114 116 119 109 P688 J1 COMMAND IN P682 ROLL ENGAGE J3 1 S350 SQUAT SWITCH S350 SP2(M) 1 P P T3 T3 J447 P P B9 P688 J1 (NOTE 1) 0-10 VAC (NOTE 1) 0-10 VAC 8 15 26 27 POSITION (PITCH) IN PILOT STICK POSITION (PITCH) IN CPG STICK B8 P STATUS HARS BIT IN 5 VDC 0-5 VAC (NOTE 4) 30 31 LVDT 2 IN POSITION SERVOCYLINDER PITCH 43 T3 42 VALVE IN PITCH SCAS SOLENOID (PITCH) OUT (NOTE 8) MAGNETIC SWITCH 28 VDC 28 VDC P447 P683 GND=ASE FAIL J4 28 VDC=NORMAL P459 28 VDC P371-39 P371-38 J459 B17 PITCH SCAS RTN GND POWER IN COMPUTER POWER IN PITCH SAS GND 28 VDC 28 VDC 75 74 (HS) GS601 P682 SP5 H (NOTE 6) 5 VDC IN VALID IN HARS RATE 27 D GS601 116 28 P683 J4 P/O DASEC A69 M70-219-6B J447 W211 W119 W211 W211 W119 A5 W211 W118 W119 P371 - 46 P371 - 47 B16 125 124 HI LO SECONDARY MUX BUS 46 45 HI LO HI LO B10 52 28 VDC IN PITCH BUCS TRACER T3 T3 T3 A CONTROL CIRCUITS GS850 W119 W211 S350 SP1(M) P447 W119 SHEET 6 OF 8 (NOTE 18) (NOTE 19) (NOTE 13) (NOTE 19) PRIMARY MUX BUS HI LO HI LO HI LO HI LO (NOTE 18) (NOTE 13) 59 TRACER (NOTE 16) J408 SP1 W211 AT(7) AD(3) AS(5) AP(5) AM(4) AK(4) AL(4) AG(3) AH(3) AJ(3) AE(3) AF(3) AB(3) AA(3) PILOT CROSSOVER DISCONNECT (NOTE 13)