EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-09-14
ALL ú ú 02 Page 217 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(6) S 822-012Do this task to adjust the horizontal stabilizer cable system: "Horizontal Stabilizer Trim Control System Adjustment" (AMM 27-41-00/501).
(7) S 822-013Do this task to adjust the trailing edge flap cable system: "Trailing Edge Flap System Adjustment" (AMM 27-51-00/501).
(8) S 822-014Do this task to adjust the spoiler cable system: System Adjustemnt" (AMM 27-61-00/501). "Spoiler Control
(9) S 822-015Do this task to adjust the speed brake cable system: Control System Adjustment" (AMM 27-62-00/501). "Speed Brake
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-09-14
ALL ú ú 02 Page 218 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
FLIGHT CONTROL CABLES AIR PRESSURE SEALS -
__________________________________________ MAINTENANCE PRACTICES
_____________________
TASK 27-09-17-902-001
1. General_______
A. General
(1) This procedure gives the locations of the air pressure seals for the control cables of the flight control systems. Refer to AMM 20-10-04/401 for instructions on removal and installation of these air pressure seals.
NO. OF ACCESS
CABLE SYSTEM SEALS LOCATION PANEL
NO.
LEFT ELEVATOR 2 AFT PRESSURE 3701
CABLES BULKHEAD
RIGHT ELEVATOR 2 AFT PRESSURE 3701
CABLES BULKHEAD
RUDDER 2 AFT PRESSURE 3701
CABLES BULKHEAD
STABILIZER 2 AFT PRESSURE 3701
TRIM CABLES BULKHEAD
SPEED BRAKE 2 LEFT WHEEL WHEEL
CABLES WELL CEILING WELL
Description and Location of Flight Control
Cable Air Pressure Seals
Figure 201
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-09-17
ALL ú
ú 01 Page 201
ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
FLIGHT CONTROL CABLE GUARD - REMOVAL/INSTALLATION
_________________________________________________
1. General_______
A. This procedure has two tasks, one for the removal and one for the installation of a flight control cable guard (which is referred to as the cable guard). The procedure has these parts:
(1)
The removal of a cable guard
(2)
The installation of a replacement cable guard.
TASK 27-09-18-004-025
2. Control Cable Guard Removal (Fig. 401)___________________________
A. References
(1)
AMM 25-22-00/201, Passenger Seats
(2)
AMM 25-27-15/401, Carpets
(3)
AMM 25-52-65/401, Cargo Compartment Ceiling Lining
(4)
AMM 29-15-00/201, Hydraulic Systems A, B, And Standby
(5)
AMM 38-41-00/201, Water Tank Pressurization System
B.
Access
(1)
Location Zone
218 Aft Cargo Compartment
(2)
Access Panels
4504 Aft Cargo Door
4505 Aft Cargo Door Access Panel
4506 Aft Cargo Door Access Panel
C.
Procedure
S 864-027
(1)
Remove power from the hydraulic systems A and B (AMM 29-15-00/201).
(2)
Remove pressure from the water tank (AMM 38-41-00/201).
(3)
Attach DO-NOT-OPERATE tags to the control columns.
S 014-030 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(21)
