757 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 3(120)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 (a) Move the captain's control column full forward.
 (b) Move the captain's control column full aft.
 (c) Move the captain's control column back to the neutral position.
 (d) Verify that the control columns move smoothly and without
 binding through the entire travel range.
 S 732-070
 (9)  Do the Autopilot Hardover Test in the Elevator Control System -
System Test (AMM 27-31-00/501).
 NOTE: When accomplishing the Autopilot Hardover Test for the____
 purpose of post-installation checking of the feel unit roller
 bearing, it is only necessary to perform that portion of the
 hardover test with pitot systems number 1 and 2 not
 pressurized.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-17
 ALL  ú ú 02 Page 218 ú May 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 S 732-063
 (10)
 Do the MCDP Ground Test 68 - Elevator Servo Limit (FIM 22-00-04/101, Fig. 111).

 S 412-064

 (11)
 Close the access door for the forward stabilizer compartment, 311AL (AMM 06-42-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-17
 ALL  ú ú 02 Page 219 ú May 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 ELEVATOR FEEL ACTUATOR - REMOVAL/INSTALLATION
_____________________________________________
 1.  General_______
 A.  This procedure contains steps to remove and install the elevator feel actuator.
 TASK 27-31-18-024-001
 2.  Remove the Feel Actuator________________________
 A.  Equipment
 (1)  
Gage Assembly - B27039-3, Part of the Elevator
 and Stabilizer Rigging Equipment, B27039-1

 B.  
References

 (1)  
06-42-00/201, Empennage Access Doors and Panels

 (2)  
24-22-00/201, Electrical Power - Control

 C.  
Access

 (1)  
Location Zones 211/212 Control Cabin 313/314 Stabilizer Center Section Compartment

 (2)  
Access Panels
 313AL Elevator Feel Actuator

 D.  
Prepare for the Removal

 S 864-002
 (1)  
Supply electrical power (Ref 24-22-00).

 S 864-003

 (2)  
Put the L, R, and C FLT CONTROL SHUTOFF switches on the right side panel, P61, to the OFF position.

 S 864-004

 (3)  
Put the RIGHT and CENTER STAB TRIM SHUTOFF valve switches on the control stand panel, P10, to the CUTOUT position.

 S 864-005

 (4)  
Open these circuit breakers on the overhead panel, P11, and attach DO-NOT-CLOSE tags:

 (a)  
11B19, STAB TRIM ALT (IF INSTALLED)

 (b)  
11C12, STAB TRIM SHUTOFF LEFT

 (c)  
11C13, STAB TRIM SHUTOFF RIGHT

 (d)  
11C05 or 11H11, STAB TRIM CONT L

 (e)  
11H17, FLT CONT SHUTOFF TAIL LEFT

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-18
 ALL  ú ú 02 Page 401 ú Jan 20/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

ELEVATOR FEEL ACTUATOR SEE A
1. FEEL UNIT 
BSEE HYDRAULIC LINES  A  A 
3. FEEL ACTUATOR  B  B  2. TORQUE BOX FOR THE AFT MECHANISM 
FWD 
A ELEVATOR FEEL ACTUATOR  INBD 
Figure 401 (Sheet 1) Elevator Feel Actuator Installation 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：757 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 3(120)