(g)  
Remove the roller (4) from the lever (7).

 TASK 32-32-04-404-022
 5.  Wing Landing Gear Downlock-Operated Sequence Valve Mechanism Installation_________________________________________________________________________
 A. Special Tools and Equipment
 (1)  
G12001 Kit (Rigging Pins) ~............................................................. | Rigging Pin No. | Length (inch) | Diameter (inch)| ............................................................... | WD-5 | 3.25 | 0.185 to 0.188| ............................................................... | WD-6 | 3.25 | 0.185 to 0.188| 2....................…....................…...................1

 B.
References

 (1)  
29-11-00/201, Main Hydraulic Supply System

 (2)  
32-00-30/201, Landing Gear Door Locks

 (3)  
IPC 32-32-04 Fig. 2

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-32-04
 ALL  ú ú 03 Page 409 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 C.  Access
 (1)  
Location Zone
 735 Wing Landing Gear, LH
 745 Wing Landing Gear, RH

 D.  
Procedure

 S 424-023
 (1)  
Install the sequence valve mechanism (Fig. 401):

 (a)  
Install the roller (4) on the lever (7).

 (b)  
Connect the lever assembly (7) to the clevis with the bolt (8).

 (c)  
Connect the link (11) to the valve with the bolt (12).

 (d)  
Connect the clevis assembly (10) to the valve with the four bolts (3).

 (e)  
If the bolt heads have holes, install a lockwire.

 (f)  
Connect the link (11) to the lever assembly (7) with the bolt (9).

 (g)  
Use the four screws to install the top cover (5).

 (h)  
Connect the outer cover (6) to the valve attach bracket.

 (i)  
Install the striker arm (1) with the striker plates (16) attached, to the upper side strut.

 S 824-024
 (2)  
Adjust the sequence valve mechanism:

 (a)  
Install the rigging pin in the rigging pin hole.

 1)  Install or remove striker arm plates (16) to permit the easy installation of the rigging pin.
 CAUTION:_______MAKE SURE YOU REMOVE THE RIGGING PIN. FAILURE TO REMOVE THE RIGGING PIN WILL CAUSE DAMAGE TO THE MECHANISM IF THE DOOR OPERATES.
 (b)  Remove the rigging pin.
 1)  Install or remove striker arm plates (16) to permit the easy removal of the rigging pin.
 E.  Put the Airplane to Its Usual Condition.
 S 094-025
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASKS BELOW TO REMOVE
_______ THE DOOR LOCKS FROM THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT REMOVE THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (1)  Do this task: "Wing Landing Gear Door Lock Removal"
 (Ref 32-00-30/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-32-04
 ALL  ú ú 01 Page 410 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
 (2)  S 094-037Do this task: "Body Landing Gear Door Lock Removal" (Ref 32-00-30/201).
 (3)  S 864-026Remove the pressure from hydraulic system No. 4 (Ref 29-11-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-32-04
 ALL  ú ú 01 Page 411 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 WING LANDING GEAR UPLOCK-OPERATED SEQUENCE VALVE AND MECHANISM -
________________________________________________________________ REMOVAL/INSTALLATION
　
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 起落架 LANDING GEAR 4(76)