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时间:2011-04-06 23:15来源:蓝天飞行翻译 作者:航空
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

 NOTE: The MAN L and MAN R switches are on the P5 overhead
____
 panel.

 (c)  
Select <GROUND TEST on the CMC main menu.

 (d)  
Select <21 CABIN PRESSURE from the ground tests menu.

 (e)  
Select <CPCS-A or <CPCS-B from the cabin pressure menu.

 (f)  
Make sure that IN PROGRESS is shown on the CMC CDU.

 (g)  
Make sure PASS is shown on the CMC CDU.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 714-029
 (18) Do a manual operation test (AMM 21-31-01/401)
 (a)  Push the applicable (MAN L or MAN R) switch-light, on the P5
 panel, to the ON position.
 (b)  Move the OPEN/CLOSE switch, on the P5 panel, to the CLOSE
 position.
 (c)  Make sure the outflow valve position indicator moves to the
 closed position.
 (d)  Move the OPEN/CLOSE switch, on the P5 panel, to the OPEN
 position.
 (e)  Make sure the outflow valve position indicator moves to the
 fully open position.
 (f)  Move the OPEN/CLOSE switch, on the P5 panel, to the CLOSED
 position until the outflow valve position, on the EICAS ECS
 maintenance page, is between 0.90 and 0.95.
 NOTE:____ ON AIRPLANES WITH -23 OR -33 PRESSURE CONTROLLERS,
 a valve failure message will show if the outflow valve
 is not 90% to 95% fully open when the manual control is
 turned off.  The controller will not move the outflow
 valve to the correct position.
 (g)  Push the applicable (MAN L or MAN R) switch-light, on the P5

 panel, to the off position. S 864-032
 (19) Remove electrical power if it is not necessary (AMM 24-22-00/201).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 INTERFACE CONTROL UNIT (ICU) - REMOVAL/INSTALLATION
___________________________________________________
 1.  General_______
 A.  There is a right and a left interface control unit (ICU).
 B.  The left and the right ICU's are the same and are immediately outboard of each outflow valve.
 C.  The removal and the installation steps are the same for the left and the right ICU.
 D.  You must do a test of the ICU after you install it.
 E.  You can get access to the ICU through a panel in the bulk cargo
 compartment aft bulkhead.

 TASK 21-31-10-004-001
 2.  Interface Control Unit (ICU) Removal (Fig. 401)____________________________________
 A.  References
 (1)  
IPC 21-31-10 Fig. 1

 (2)  
WDM 21-31-12

 (3)  
SSM 21-31-02


 B.  Access
 (1)  Location Zone
 151 Area Aft of Bulk Cargo Compartment, LH
 152 Area Aft of Bulk Cargo Compartment, RH

 C.  Procedure
 S 864-027
 (1)  
Remove Electrical Power (AMM 24-22-00/201)

 S 014-004

 (2)  
Open the access panel on the aft bulkhead in the bulk cargo compartment.

 (3)  
Remove the bonding jumper from the ICU.

 S 034-007

 (4)  
Remove the electrical connectors from the ICU.


 S 034-006
 (a)  Left ICU - DM7950A, DM7950B and DM7950C
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 ALL  ú ú 03 Page 401 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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