(17)
 Remove the DO-NOT-CLOSE tags and close these circuit breakers on the overhead panel, P11:

 (a)  
11H17, FLT CONT SHUTOFF TAIL LEFT

 (b)  
11H18, FLT CONT SHUTOFF TAIL CTR

 (c)  
11H28, FLT CONT SHUTOFF TAIL RIGHT

 S 864-030
 (18)
 Remove the DO-NOT-OPERATE tags and move the FLT CONTROL SHUTOFF switches L, C, and R on the right side panel, P6l, to ON.

 S 864-031

 (19)
 Make sure that these circuit breakers on the P11 panel are closed:

 (a)  
EICAS (6 locations)

 S 824-032
 (20)
 Push the STATUS switch on the display select panel, P9, to show the control surface position indicator on the bottom EICAS display.

 S 214-033

 (21)
 Operate the rudder pedals through their full travel range and do the checks that follow:

 (a)  
Make sure that the rudder operates smoothly and correctly when the pedals are moved.

 (b)  
Make sure the rudder position indicator operates correctly and shows full rudder travel in each direction.

 (c)  
Release the rudder pedals. Make sure the rudder goes back to its neutral position.

 F.
Put the Airplane Back to its Usual Condition

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-02
 ALL  ú ú 01 Page 407 ú Jan 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 S 094-002
 WARNING: STAY AWAY FROM THE NOSE WHEELS WHEN THE LOCKPIN IS REMOVED.
_______ THE WHEELS CAN TURN TO THE CENTER POSITION QUICKLY, AND CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (1)  
Make sure that the nose wheels are in their center position and remove the towing lever lockpin from the nose gear (Fig. 402).

 S 414-034

 (2)  
Close access panel 113AL (Ref 06-41-00).

 S 864-035

 (3)  
Remove the power from the left, right, and center hydraulic systems (Ref 29-11-00).

 S 864-036

 (4)  
Remove electrical power if it is not necessary (Ref 24-22-00).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-02
 ALL  ú ú 01 Page 408 ú Mar 20/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
 RUDDER PEDAL ADJUSTMENT CRANK - REMOVAL/INSTALLATION
____________________________________________________
 1.  General_______
 A.  This procedure contains 2 tasks. The first task contains the data that is necessary to remove the captain's (or the first officer's) rudder pedal adjustment crank. The second task contains the data that is necessary to install it.
 TASK 27-21-03-024-006
 2.  Remove Rudder Pedal Adjustment Crank____________________________________
 A.  Equipment
 (1)  
Rig Pins from Set B20003-XX (Ref 20-10-24):

 (a)  
R1A - P/N B20003-26

 (b)  
R1B - P/N B20003-26

 (c)  
R2 - P/N B20003-22

 B.  
References

 (1)  
06-41-00/201, Fuselage Access Doors and Panels

 (2)  
20-10-24/201, Rig Pins

 (3)  
24-22-00/201, Electrical Power - Control

 C.  
Access

 (1)  
Location Zones
 211 Control Cabin (Left)
 212 Control Cabin (Right)
 113 Area Forward of NLG Wheel Well (Left)

 (2)  
Access Panel 113AL Flight/Landing Gear/Engine Control Components

 D.  
Prepare for Removal

 S 864-007
 (1)  
Supply electrical power (Ref 24-22-00).

 S 864-027

 (2)  
Remove the power from the left, right, and center hydraulic systems (Ref 29-11-00).

 S 864-008

 (3)  
Move the FLT CONTROL SHUTOFF switches L, C, and R on the right side panel, P61, to OFF. Attach DO-NOT-OPERATE tags and make sure that the amber switch-position legend lights come ON.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機(jī)維護(hù)手冊 飛行操縱 FLIGHT CONTROLS 2(38)