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时间:2011-04-13 07:45来源:蓝天飞行翻译 作者:航空
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 S 022-225
 (1) Remove the clamp and disconnect the wire bundle from the connector
 on the applicable antiskid valve torque motor:
 CONNECTORS

__________ ~............................................................. | Left Wing Gear Antiskid Module | ............................................................... | Valve No. 1 | Valve No. 2 | Valve No. 3 | Valve No. 4 | ............................................................... | DV25 | DV24 | DV26 | DV65 | 2...............…..............…...............…..............1 ~............................................................. | Left Body Gear Antiskid Module | ............................................................... | Valve No. 5 | Valve No. 6 | Valve No. 7 | Valve No. 8 | ............................................................... | DV41 | DV40 | DV42 | DV69 | 2...............…..............…...............…..............1 ~............................................................. | Right Body Gear Antiskid Module | ............................................................... | Valve No. 9 | Valve No. 10| Valve No. 11| Valve No. 12| ............................................................... | DV44 | DV43 | DV51 | DV73 | 2...............…..............…...............…..............1 ~............................................................. | Right Wing Gear Antiskid Module | ............................................................... | Valve No. 13 | Valve No. 14| Valve No. 15| Valve No. 16| ............................................................... | DV127 | DV126 | DV128 | DV77 | 2...............…..............…...............…..............1
 S 492-009
 (2) Put a cap on the open connector.
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 32-42-02
 ALL  ú ú 03 Page 203 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL

WING GEAR ANTISKID VALVE 
ASEE MODULE ANTISKID NORMAL  WING GEAR ANTISKID VALVE 
6.  (4 LOCATIONS) SCREW VALVE ANTISKID ASSEMBLY 1.  2.  RETAINER (2 LOCATIONS) O-RING (2 LOCATIONS) RETAINER (2 LOCATIONS) RETAINER (2 LOCATIONS) 0-RING (2 LOCATIONS) (2 LOCATIONS) RETAINER4. 5. 4. 2. 3.  ANTISKID MODULE 
SCREW 
CLAMP 
CONNECTOR  SUPPORT BRACKET 

NORMAL ANTISKID MODULE
NOTE:BODY GEAR SHOWN, WING GEAR EQUIVALENT.
A
Normal Antiskid Module - Antiskid Valve Figure 201
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-42-02
 ALL  ú ú 01 Page 204 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 032-010
 CAUTION: BE CAREFUL TO KEEP CONTAMINATION OUT OF THE PORTS OF THE
_______ ANTISKID MODULE AND THE ANTISKID VALVE. CONTAMINATION CAN CAUSE A MALFUNCTION OF THE ANTISKID VALVE.
 (3)  
Remove the four screws (6), and pull the antiskid valve (1) from the antiskid module assembly.

 S 492-011

 (4)
Install a plug on the open port in the antiskid module assembly.

 S 032-012

 (5)  
Remove the retainers (2 and 4) and the O-rings (3 and 5) from the valve, and discard the O-rings.


 TASK 32-42-02-412-013
 3. Antiskid Valve Assembly (Normal Antiskid Module) - Installation
_______________________________________________________________
 A. Special Tools and Equipment
 (1)  
T63619 - Packing Installation Tool
 Hydro-Aire Division, Crane Co.
 Burbank, CA 91510 USA


 B.
Consumable Material

 (1)  
C00272 Hydraulic Fluid - BMS 3-11

 C.
Parts


 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 201  |  1 | Antiskid Valve | 32-42-02 | 11 | 5 | | | 2 | Retainer | | | 40 | | | 3 | O-ring | | | 30 | | | 4 | Retainer | | | 35 | | | 5 | O-ring | | | 25 | | | 6 | Screw | | | 10 | 2......…........…...................................…..........…......…........1
 
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