22-11-41
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
~............................................................ | AIRPLANE WIRES | SWITCH WIRES | .............................................................. | OPTION 1 | OPTION 2 | P/N 721101A1 | P/N 43896 | .............................................................. | Green | Green | GRN | Green | .............................................................. | Blk/Grn | Blk/Blu | BKB | Black | .............................................................. | Brown | Brown | BRN | Brown | .............................................................. | Yellow | Yellow | YEL | Yellow | .............................................................. | Spare | Spare | BKY | Orange | .............................................................. | Blue | Blue | BLU | Blue | .............................................................. | Black/Yellow | Blk/Gra | BKA | White | .............................................................. | Spare | Spare | BKG | Grey | 2..............…..............…..............…...............1
(h)
Set the wire bundle on top of the terminal block insulator.
(i)
Put the sponge rubber pad (8) on top of the wire bundle.
(j)
Install the approach plate assembly and the medallion cover.
S 864-014
(3)
Supply the electrical power (Ref 24-22-00/201).
S 864-015
(4)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a) P6-2 Circuit Breaker Panel
1) AFCS B SNSR EXC AC
2) AFCS B FCC DC
3) AFCS ENGAGE INTLK B
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22-11-41
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737-300/400/500MAINTENANCE MANUAL
4) AFCS B WARN LIGHT BAT
5) AFCS B MACH TRIM AC
6) AFCS B MACH TRIM DC
(b) P18-1 Circuit Breaker Panel
1) AFDS MCP DC
2) AFCS A SNSR EXC AC
3) AFCS A FCC DC
4) AFCS ENGAGE INTLK A
5) AFCS A WARN LIGHT BAT
6) AFCS A MACH TRIM AC
7) AFCS A MACH TRIM DC
S 714-016
(5)
Do this task: "Autopilot Disengage Switch Test" (AMM 22-11-41/501).
S 864-017
(6)
Remove the electrical power if it is not necessary (Ref 24-22-00/201).
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22-11-41
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737-300/400/500MAINTENANCE MANUAL
AUTOPILOT DISENGAGE SWITCH - ADJUSTMENT/TEST
____________________________________________
1. General_______
A. This procedure contains the installation test of the autopilot disengage switch.
B. This test makes sure that the autopilot disengage switch operates correctly after the replacement.
C. You can find the autopilot disengage switch on each outboard horn of the pilot's control wheel.
TASK 22-11-41-715-003
2. Autopilot Disengage Switch Test_______________________________
A. References
(1)
24-22-00/201, Manual Control
(2)
29-15-00/201, Hydraulic A, B, and Standby System
B. Access
(1) Location Zones
101 Control Cabin, Left
102 Control Cabin, Right
C. Autopilot Disengage Switch Test
S 865-002
(1) Supply electrical power (Ref 24-22-00/201).
S 865-001
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDER, ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(2)
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本文链接地址：737-300 400 500 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 2(56)
