TM 1-1520-238-T-7 11–203 11–27. DASE– WIRING INTERCONNECT DIAGRAM (COLLECTIVE) (BUCS DEACTIVATED) (cont) 11–27 E A F N B F C D A B E G F A14 B10 TB3 - 6 W211 (NOTE 9) CB18 P/O PILOT CIRCUIT ASE AC T1 A D W119 W211 M H P431 J27 P441 J24 1 1 A11 GS2 A E J GS1 A323 A16 A18 A17 A15 A13 B7 A6 P P499 J5 P493 J4 P A5 B17 B16 GS3 TB3 - 7 C J L K J K F TB2-1 A13 J5 P499 5A CB28 ASE DC A76 BUS 1 115 VAC ESS BUS 3 28 VDC BREAKER PANEL TRANSFORMER DASE EXCITATION TRANSFORMER DASE EXCITATION T2 26 VAC OUT 115 VAC IN 115 VAC IN 26 VAC OUT GND GND A11 B1 B1 A402 P/O ELECTRICAL POWER DISTRIBUTION BOX (NOTE 9) G K B E TB2 - 7 F GS6 TB2 - 15 VDC IN 28 B14 B13 A11 J20 P433 J1 P1 54 34 D P431 J27 B4 B2 (NOTE 5) SQUAT RELAY X2 X1 B1 B3 XK4-1/2 K4-1/2 P/O AFT AVIONICS MATRIX MODULE 1A W605 P(4) N(6) L(4) K(4) M(4) P P P P P B P M70-220-2A SHEET 2 OF 14 P P W211 W211 W211 AB(3) AA(3) Z(3) Y(3) X(3) W(3) V(3) U(3) T(3) S(3) R(3) C(1) A(1) B(1) W605 W668 W119 W642 (NOTE 9) (CENTER) P 1 1 2 2