2..................…....................…......................................1
Wire Labels and Color Codes for Switch P/N 721101A1 Table 401
~....................................... | TERMINAL T309/ | SWITCH SW43896 | | T310 PIN NO. | WIRE COLOR | ......................................... | 10 | Brown | | 8 | Yellow | | 6 | Green | | 5 | Black | | 7 | White | | 9 | Blue | | 11 | Orange | | 12 | Grey | 2..................…....................1
Terminal No. and Color Code For Switch SW43896 Table 402
(h)
Set the wire bundle on top of the terminal block insulator.
(i)
Install the approach plate assembly and the medallion cover. 1) Install three screws behind the control wheel.
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(3) S 864-045Supply the electrical power (Ref 24-22-00/201).
(4) S 864-047Remove the DO-NOT-CLOSE tags and close these circuit breakers: (a) P7 Overhead Circuit Breaker Panel 1) 7D7, FLT CONT CMPTR SERVO L 2) 7D8, FLT CONT COMPTR PWR L 3) 7D12, FLT CONT CMPTR SERVO C 4) 7D13, FLT CONT CMPTR PWR C 5) 7D14, FLT CONT CMPTR SERVO R 6) 7D15, FLT CONT CMPTR PWR R 7) 7E9, MCP L 8) 7E18, MCP R 9) 7E24, AUTO FLT WARN
(5) S 744-049Do this task: Ground Test - Autopilot Disconnect Switch (Ref 22-10-00/501).
(6) S 864-052Remove the electrical power if it is not necessary (Ref 24-22-00/201).
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747-400 MAINTENANCE MANUAL
AFCS GO-AROUND SWITCH - REMOVAL/INSTALLATION
____________________________________________
TASK 22-11-04-004-017
1. AFCS Go-Around Switch Removal/Installation__________________________________________
A. General
(1) For the removal/installation of the AFCS Go-Around Switches, refer to AMM 76-12-02/401.
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747-400 MAINTENANCE MANUAL
AUTOPILOT/FLIGHT DIRECTOR PITCH AXIS CONTROL - DESCRIPTION AND OPERATION
________________________________________________________________________
1. General_______
A. The following section describes the details of the pitch axis control autopilot (A/P) and flight director (F/D) operation in all modes of flight. Additional information on autopilot/flight director (AP/FD) mode desciption and flight profile is discussed in 22-10-00/001.
B. The major components providing pitch axis control of the airplane are (Fig. 1 and 2):
(1)
Elevator Autopilot Servos (3)
(2)
Flight Control Computers (3) (Ref 22-10-00/001)
(3)
AFCS Mode Control Panel (1) (Ref 22-10-00/001)
C. The above components rely on inputs from the following systems or components to provide pitch axis AP/FD commands (Fig. 3):
(1)
Air Data Systems
(2)
Autopilot Disengage Switches
(3)
Flap Control Units
(4)
Flight Management Computer System
(5)
Go-Around Switches
(6)
Inertial Reference System
(7)
ILS Navigation System
(8)
Radio Altimeter System
(9)
Speed Brake Position Transducer
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