TM 1-1520-238-T-10 12–10 Change 10 12–1. DASE – WIRING DIAGRAM (BUCS DEACTIVATED) 12–1 (SERIAL NO. 82-23355 THRU 88-0199) (cont) A2 1 7 A16 10 7 A17 10 A18 A20 J447 P447 8 J459 A16 P459 A15 W211 B19 B18 J912 W119 W211 P912 W118 + RATE OF TURN C D 19 HI 39 LO 20 RTN 38 B16 J407 2 J118 P118 A400 P407 W211 1 - RATE OF TURN A1 SHEET 9 OF 11 M50-236-9C (SEE NOTE 13) 1 11 J456 P456 A12 P (SEE NOTE 13) P P P A320 P L P750 P/O VIDEO DISPLAY UNIT (VDU) GS604 P A636 P/O AIR DATA PROCESSOR (ADP) J1 GS290 ASE RELEASE SW S1 P P113 J113 P/O PILOT CYCLIC STICK A401 W255 W118 W119 W118 W117 J908 P908 M P944 1J3 M(2) B(10) A(10) N(2) X(8) SIDE SLIP P/O CPG CYCLIC STICK D(10) E(10) C(10) W211 PILOT CROSSOVER DISCONNECT G(10) F(10) AFT CROSSOVER DISCONNECT ASE RELEASE SW S1 CPG CROSSOVER DISCONNECT PILOT CROSSOVER DISCONNECT V_ut