S 864-019
 (1)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P180 DC Power Distribution Panel
 1) 180E22 LATERAL CONT VLV SYS 4

HYDRAULIC LINES

Inboard Flight Spoiler Ratio Changer Actuator Installation
Figure 401 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-61-13
 ALL  ú ú 01 Page 404 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 864-020
 (2)  
Put the FLT CONTROL HYD POWER - WING system 4 switch on the P5 panel to the NORM position.

 S 864-021

 (3)  
Do this task to pressurize hydraulic systems No. 1 and 4:
 "Hydraulic System Pressurization" (Ref 29-11-00/201).

 S 714-022

 (4)  
Do a check of the operation of the actuator:

 (a)  
Put the speed brake control lever in the UP position to lift the spoilers No. 5 and 8.

 (b)  
Make sure that the ratio changer actuator extends.

 (c)  
Make sure there are no hydraulic leaks.

 (d)  
Put the speed brake control lever in the DOWN position.

 (e)  
Make sure that the ratio changer actuator retracts.

 E.
Put the Airplane Back to Its Usual Condition

 S 864-023
 (1)  
Do this task to depressurize hydraulic systems No. 1 and 4:
 "Hydraulic System Depressurization" (Ref 29-11-00/201).

 S 414-024

 (2)  
Close the access panel 572FB on the left wing or 672FB on the right wing below the inboard spoiler actuator.

 (3)
Do this task: "Hydraulic Reservoir Servicing" (Ref 12-12-01/301).

 (4)  
Do this task: "Remove Electrical Power" (Ref 24-22-00/201).

 S 614-025
 S 864-026
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-61-13
 ALL  ú ú 01 Page 405 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 INBOARD FLIGHT SPOILERS RATIO CHANGER ACTUATOR - INSPECTION/CHECK
_________________________________________________________________
 1.  General_______
 A.  There is one task in this procedure; an inspection of the inboard flight spoiler ratio changer actuator. To do the inspection, you measure the inner and the outer diameters of the parts that connect the ratio changer actuator.
 B.  You usually do this procedure before you install a ratio changer
 actuator.

 TASK 27-61-13-206-001
 2.  Ratio Changer Actuator Inspection (Fig. 601)_________________________________
 A.  Standard Tools and Equipment
 (1)  
Micrometer - 0 to 1 inch(0-25mm)

 (2)  
Vernier caliper

 B.  
References

 (1)
AMM 27-61-13/401, Inboard Flight Spoiler Ratio Changer Actuator

 C.  
Access

 (1)  
Location Zone
 575 Spoiler No. 5
 675 Spoiler No. 8

 (2)  
Access Panel
 572FB Access Panel
 672FB Access Panel

 D.  
Procedure

 (1)  
Do this task: "Ratio Changer Actuator Removal" (AMM 27-61-13/401).

 S 226-003

 (2)  
Examine the bolts, bushings and other parts that connect the ratio changer actuator for worn areas (Fig. 601):

 (a)  
Remove the parts.

 (b)  
Use a micrometer or a vernier caliper to measure the parts.

 (c)  
Compare the dimensions you measured with the permitted dimensions shown on Fig. 601.

 (d)  
Repair or replace the parts that are not in the tolerance.

 (e)  
Install the parts.

 S 026-002
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
中國航空網 m.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 6(99)