M70-219-5A CR3 CR1 CR7 CR8 CR4 CR6 CR9 P1077 - P (NOTE 17) (NOTE 16) (NOTE 17) W611 W611 W119 W642 W605 W211 W119 SHEET 5 OF 8

M70-219-4A AAG (NOTE 15) (NOTE 14) (NOTE 16) W611 W211 W211 W211 ABM A W211 W211 ON OFF SHEET 4 OF 8

M70-219-6B J447 W211 W119 W211 W211 W119 A5 W211 W118 W119 P371 - 46 P371 - 47 B16 125 124 HI LO SECONDARY MUX BUS 46 45 HI LO HI LO B10 52 28 VDC IN PITCH BUCS TRACER T3 T3 T3 A CONTROL CIRCUITS GS850 W119 W211 S350 SP1(M) P447 W119 SHEET 6 OF 8 - TM-1-1520-238-T-7_519

TM-1-1520-238-T-7 Army Model AH-64 Helicopter (NSN
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TM 1-1520-238-T-7 11–184 11–24. DASE – WIRING INTERCONNECT DIAGRAM (PITCH) (BUCS DEACTIVATED) (cont) 11–24 J1 1 A76 P/O AFT AVIONICS MATRIX MODULE 1 P683-121 (NOTE 15) CR5 (NOTE 9) P463 J1 EMER BUS 28 VDC 5A CB29 COMM IFF S P/O PILOT CIRCUIT BREAKER PANEL (CENTER) A4 B3 P683-122 B9 P485 SPI A2 J447 P170 P447 P447 A3 A137 B4 A1 B8 A1 15 J4 A323 10 GS2 C 4.7K 1/4W 13 8 R1 B7 B1 B10 A9 P683-120 (NOTE 14) J447 9 11 4 6 DIODE BOARD A11 A14 P493 P/O PILOT ASE PANEL CR2 7 2 M70-219-5A CR3 CR1 CR7 CR8 CR4 CR6 CR9 P1077 - P (NOTE 17) (NOTE 16) (NOTE 17) W611 W611 W119 W642 W605 W211 W119 SHEET 5 OF 8 (NOTE 10) W211 W211 2 AP(6) AR(7) AS(6) A(4) B(4) C(4) D(4) E(4) F(4) G(4) H(4) J(4) K(4) L(4) M(4) N(4) AN(4) Z(3) 2 1

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