TM 1-1520-238-T-7 11–196 11–26. DASE – WIRING INTERCONNECT DIAGRAM (YAW) (BUCS DEACTIVATED) (cont) 11–26 BREAKER PANEL (CENTER) L(4) A15 A18 B13 M L A B A18 A17 A L N A F P E B G C J L A20 B17 B16 26 VAC OUT 115 VAC IN T2 P1 J1 115 VAC BUS 1 ASE AC CB28 ASE DC A11 A D P441 F TB2-15 J24 B1 X1 M B3 (NOTE 12) 1 P/O PILOT CIRCUIT K(4) 1 A11 J5 ^P499P A323 J M GS2 J4 A19 P493 A17 K B F H D GS1 P499 J5 B7 A16 TB3-7 GS3 K TB3-6 TB2-1 GND T1 115 VAC IN 26 VAC OUT GND P/O AFT AVIONICS MATRIX MODULE A13 J5 P499 34 ESS. 28 VDC 5A A76 BUS 3 CB18 54 P431 J27 B14 GND DC 28 VDC IN B13 A11 B1 P431 J20 P433 J27 A402 B1 K H TB2-7 X2 K4-1/2 GS6 G E B4 XK4-1/2 B2 (NOTE 5) SQUAT RELAY P/O ELECTRICAL POWER DISTRIBUTION BOX (NOTE 12) M70-221-2A SHEET 2 OF 7 DASE EXCITATION TRANSFORMER DASE EXCITATION TRANSFORMER 1A W605 W211 W211 A(1) B(1) C(1) W211 W211 W211 P P P P P P X(3) Z(3) V(3) S(3) R(3) T(3) U(3) AB(3) W(3) P P M(4) N(4) P(6) P P P W668 W605 W119 W119 W211 W642 B D D Y(3) AA(3) (NOTE 12) 2 2 1 1