22-11-36
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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737-300/400/500MAINTENANCE MANUAL
6) AUTO FLT CONT SYS B ENGAGE INTLK B
7) AUTO FLT CONT SYS B WARN LIGHT BAT
(b) P18 Circuit Breaker panel
1) AUTO FLT CONT SYS A MACH TRIM AC
2) AUTO FLT CONT SYS A MACH TRIM DC
3) AFDS MCP DC
4) Airplanes with mechanical aileron force limiter:
AFDS AIL FORCE LIM
5) AUTO FLT CONT SYS A SNSR EXC AC
6) AUTO FLT CONT SYS A FCC DC
7) AUTO FLT CONT SYS A ENGAGE INTLK A
8) AUTO FLT CONT SYS A WARN LIGHT BAT
9) YAW DAMPER AC
10) YAW DAMPER DC
S 864-008
(2)
Supply electrical power (Ref 24-22-00/201).
S 864-013
(3)
Align the IRS (Ref 34-28-00/501 or 34-28-01/501).
S 864-018
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.
(4)
Supply hydraulic power (Ref 29-15-00/201).
S 714-010
(5)
Do these steps:
(a)
Set the autopilot A engage switch to the CWS position.
(b)
Make sure the autopilot A engage switch stays in the CWS position.
(c)
Disengage the autopilot A.
(d)
Set the autopilot B engage switch to the CWS position.
(e)
Make sure the autopilot B engage switch stays in the CWS position.
(f)
Disengage the autopilot B.
S 414-012
(6)
Install the 1201L electronic equipment access door (Ref 12-31-11/201).
(7)
Remove electrical power if it is not necessary (Ref 24-22-00/201).
S 864-011
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH AFC ACCESSORY UNIT ú
22-11-36
ú ú 06 Page 403 ú Jul 12/00
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737-300/400/500MAINTENANCE MANUAL
S 864-017
(8) Remove hydraulic power if it is not necessary (Ref 29-15-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH AFC ACCESSORY UNIT ú
22-11-36
ú ú 02 Page 404 ú Jul 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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737-300/400/500MAINTENANCE MANUAL
INTEGRATED FLIGHT SYSTEM ACCESSORY UNIT - REMOVAL/INSTALLATION
______________________________________________________________
1. General_______
A. This procedure contains two tasks. The first task is the removal of the Integrated Flight System Accessory Unit (IFSAU) from the equipment shelf in the electronic compartment. The second task is the installation of the IFSAU to the equipment shelf in the electronic compartment.
B. You can find the IFSAU on the E1-3 shelf in the electronic compartment. The cam-lock handle, which attaches to the fork on the shelf, keeps the IFSAU in the shelf.
TASK 22-11-37-004-001
2. Integrated Flight System Accessory Unit Removal_______________________________________________
A. Reference
(1)
AMM 12-31-11/201, Body Section 41 Access Door
(2)
AMM 20-10-07/201, Electrical/Electronic Black Box
B. Access
(1)
Location Zone
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 2(46)
