TM 1-1520-238-T-7 Change 3 11–181 11–24. DASE – WIRING INTERCONNECT DIAGRAM (PITCH) (BUCS DEACTIVATED) (cont) 11–24 J219 P219 P/O LONGITUDINAL (PITCH) SERVOCYLINDER B14 OUT (NOTE 3) L34 P493 J4 W Z B15 115 VAC IN A11 GS3 TB3-6 T2 26 VAC OUT HYDRAULIC VALVE IN 15 1 1 3 OUT (NOTE 4) LVDT 1 HI 4 LO 6 P P P SCAS LVDT 0±15VDC HI LO ELECTRO- P J220 P220 4 5 GS466 EXCITATION IN LVDT 1 CASE GND 26 VAC 5 1 2 J219 P219 P P A323 P P499 J5 B12 B13 A2 A4 A18 A17 A3 S P TB1-5 A13 J5 P499 P/O AFT AVIONICS MATRIX MODULE P499 J5 G A H J B GS1 N H G A TB3-7 A1 A19 A20 B7 B17 B16 G D K A F F G E B A C J L GND TB2-1 K TRANSFORMER DASE EXCITATION T1 GND 115 VAC IN 26 VAC OUT TRANSFORMER DASE EXCITATION M70-219-2A SHEET 2 OF 8 P P 14 P P P P P P P W211 W211 W211 W211 W211 W211 W211 HI LO P W642 B(1) C(1) D(1) E(1) F(1) G(1) H(1) J(1) L(1) K(1) M(3) N(3) P(3) R(4) S(4) T(4) U(3) V(3) W(4) X(3) Y(3)