TM 1-1520-238-T-7 11–209 11–27. DASE– WIRING INTERCONNECT DIAGRAM (COLLECTIVE) (BUCS DEACTIVATED) (cont) 11–27 P/O AFT AVIONICS MATRIX MODULE J447 2 P447 A2 J4 P683 OUT P688 P459 J459 J1 BUCS 1 65 66 BUCS TRACER 62 J215 SP1(HS) J402 P402 B17 J408 SP1 (M) J756 P756 59 J5 P499 N P A4 2 B18 A6 122 (NOTE 7) 28 VDC^ATTD/HOVER HOLD P686 MAGNETIC SWITCH P447 J447 J2 IN 28 VDC HOLD ATTD/HOVER 28 VDC IN SELF TEST ROTOR BRAKE P682 SP4(HS) GND BUCS 2 28 VDC IN 68 G 28 VDC IN (NOTE 10) GS601 J3 P682 61 YAW BUCS TRACER 28 VDC=NORMAL GND=BUCS FAIL 28 VDC=NORMAL GND=BUCS ON 28 VDC IN 28 VDC IN PITCH BUCS TRACER IN 28 VDC IN 28 VDC ROLL BUCS TRACER J4 P683 114 115 P/O DASEC (NOTE 10) 22 P756 J756 24 B19 J417 SP1 (M) J402 (NOTE 10) P402 J2 P686 60 A69 (NOTE 10) J415 SP1 (M) A7 A10 B12 J4 P493 P499 J5 K R TB3-4 TB3-3 A323 M70-220-8A SHEET 8 OF 14 W119 W119 W119 W211 W211 W211 W170 W115 46 45 HI LO PRIMARY MUX BUS (NOTE 17) W211 W211 W170 W211 G(6) J(6) L(9) B(5) A(4) W642 (NOTE 10) 114 119 M(9) W211 124 125 HI LO SECONDARY MUX BUS W211 K(6)