TM 1-1520-238-T-7 11–115 11–13. FLIGHT CONTROL SYSTEM – WIRING INTERCONNECT DIAGRAM (cont) 11–13 W211 A14 X1 X2 C2 C1 A13 H C3 W118 A16 A15 A14 A15 W119 B10 TB3-9 TB2-28 G B J G W117 P488 J18 J24 P441 J11 P423 J27 P431 1 G H J K M L A1 GS7 B1 B2 A2 A3 B3 TRIM BRAKE RELAY C A B TB3-7/8 GS7 H F A K1-9/10 (NOTE 2) 28 VDC RELEASE G F E TRIM B7 B6 TB2-29 B14 B16 (NOTE 7) P/O ELECTRICAL POWER DISTRIBUTION BOX A402 A7 M70-001-2A SHEET 2 OF 3 B15 H YAW TRIM 28 VDC PITCH TRIM 28 VDC ROLL TRIM 28 VDC XK1-9/10 W668 A(1) B(1) E(1) C(1) D(1) F(1) G(1) H(1) J(1) K(1) N(1) L(1) M(1) (NOTE 3)