S 714-022

 (4)  
Operate the rudder trim switch in each direction until the rudder trim indicator shows 9.5 units of rudder trim.

 (a)  
Make sure the two rudders move in the correct direction.

 (b)  
Make sure the two rudders move to 23.7 degrees in each direction.

 NOTE: Use the flight controls maintenance page of EICAS to
____ find the angle of the rudders.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-10
 ALL  ú ú 02 Page 406 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (c)  
Operate the rudder trim switch until the rudder trim indicator shows zero units of trim.

 (d)  
Make sure the rudders are in their neutral positions.

 I.
Put the Airplane Back to Its Usual Condition

 S 434-023
 (1)  
Connect the steering rod for the nose gear to the rudder forward quadrant.

 S 864-024

 (2)  
Remove the power from all the hydraulic systems (AMM 29-11-00/201).

 S 864-025

 (3)  
Remove electrical power if it is not necessary (AMM 24-22-00/201).

 S 414-026

 (4)  
Close access panels 324FR and 324FL (AMM 06-09-07/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-10
 ALL  ú ú 02 Page 407 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 RUDDER FEEL, CENTERING AND TRIM MECHANISM - REMOVAL/INSTALLATION
________________________________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is a task for the removal and a task for the installation of the rudder feel, centering and trim mechanism.
 B.  The removal procedure has these parts:
 (1)  
The removal of the access panels

 (2)  
The installation of the rig pins

 (3)  
The removal of the feel, centering and trim mechanism

 C.  
The installation procedure has these parts:

 (1)  
A check of the parts for worn areas

 (2)  
An adjustment of the spring tension for the feel, centering and trim mechanism

 (3)  
The installation of the feel, centering and trim mechanism

 (4)  
The lubrication of the feel, centering and trim mechanism

 (5)  
An operational test of the feel, centering and trim mechanism.

 TASK 27-21-11-004-001
 2.  Rudder Feel, Centering and Trim Mechanism Removal (Fig. 401)_________________________________________________
 A.  Special Tools and Equipment
 (1)  
G12001-50, Rig Pin Kit

 B.  
References

 (1)  
AMM 24-22-00/201, Manual Control

 (2)  
PASSENGER AIRPLANES; AMM 25-22-01/401, Main Passenger Cabin Ceiling Panel

 (3)  
FREIGHTER AIRPLANES; AMM 25-59-01/401, Main Deck Compartment Cargo Lining Panel

 C.  
Access

 (1)  
Location Zone
 211 Passenger Cabin-Nose to First Door, LH
 324 Vertical Fin, Rear Spar to Trailing Edge

 (2)  
Access Panel
 324FL Inspection Access Panel
 324FR Centering Mechanism Access Panel

 D.  
Procedure

 (1)  
Supply the electrical power (AMM 24-22-00/201).

 S 864-003

 (2)  
Put the FLT CONTROL HYD POWER - TAIL switches No. 1, 2, 3, and 4 on the overhead panel to the SHUTOFF position.

 S 864-005

 (3)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P6, Main Power Distribution Panel
 1) 6J24, RUD/ELEV SENSOR
 2) 6J25, RUD/ELEV IND

 S 864-002
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 2(107)