(10)
Align the elevator trailing edge with the index mark on the tail cone (Fig 402):
(a)
Install the rig pin E-5.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-71
ALL ú ú 04 Page 408 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(b) Adjust the elevator control pushrods in this task: "Adjustment
-Elevator and Tab Control System" (Ref 27-31-00/501).
S 714-013
(11)
Do a check for the output rod of the feel and centering unit (1):
(a)
Make sure the lower bolt hole of the output rod aligns with the bolt hole in the aft quadrant crank. 1) If it is necessary, adjust the output rod (1)
(Ref 27-31-00/501).
S 024-032
(12)
Remove the rig pin E-5.
S 714-014
(13)
Make sure that rig pin E-4 is free to move through the rig pin holes.
S 714-016
(14)
Do this task: "System Test - Power Mode Operation" (Ref 27-31-00/501).
S 714-017
(15)
Do this task: "System Test - Feel Force System and Autopilot Authority" (Ref 27-31-00/501).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-71
ALL ú ú 04 Page 409 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
ELEVATOR OUTPUT TORQUE TUBE - REMOVAL/INSTALLATION
__________________________________________________
1. General_______
A. This procedure has two tasks, one for the removal and one for the installation of the elevator output torque tube (which is referred to as the "torque tube"). The procedure has these parts:
(1)
The removal of the torque tube
(2)
The installation of the replacement torque tube
(3)
An adjustment of the elevator control pushrods.
TASK 27-31-74-004-001
2. Elevator Output Torque Tube Removal (Fig. 401)___________________________________
A. Special Tools and Equipment
(1)
F70207-93 Rigging Pin Kit
B.
References
(1)
12-31-41/201, Body Section 48 Access Doors and Panels
(2)
22-11-26/401, Autopilot Elevator Actuator
(3)
27-31-00/201, Elevator and Tab Control System
(4)
53-53-00/401, Tail Cone
C.
Access
(1)
Location Zone
701 Area 1 Tail Compartment
(2)
Access Panels
3802 Tail Cone Access Door
D.
Prepare for Removal
S 864-003
(1)
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 3(7)