(b)  
Push the NEXT PAGE key until you find all the GROUND TEST MSG pages.

 (c)  
Make a list of all the CMCS messages, CMCS message numbers, and ATA numbers that show on the GROUND TEST MSG pages.

 (d)  
Go to the CMCS Message Index of the Fault Isolation Manual (FIM) to find the corrective action for each CMCS message.

 F. Put the Airplane to its Usual Condition
 S 865-083
 (1)  
Remove the electrical power, if it is not necessary
 (Ref 24-22-00/201).

 S 865-110

 (2)  
Make sure the LOWER LOBE CARGO COND AIR FLOW RATE selector on the overhead P461 panel is in the OFF position.

 TASK 21-58-00-705-056
 3. Operational Test - Override Mode Test
_____________________________________
 A. References
 (1)  24-22-00/201, Manual Control
 B. Access
 (1)  Location Zone 121 Forward Cargo Compartment Forward Half, LH
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A
747-400 MAINTENANCE MANUAL
 C. Prepare for the Test
 S 865-057
 (1)  
Supply electrical power (Ref 24-22-00/201).

 S 865-058

 (2)  
Make sure the EQUIP COOLING selector, on the P5 panel, is in the NORM position.

 D. Do the Test
 S 715-005
 (1) Do a test of the equipment cooling system in the override mode.
 CAUTION: DO NOT KEEP THE EQUIP COOLING SWITCH IN THE OVRD POSITION
_______ FOR MORE THAN FIVE MINUTES. EXTENDED OPERATION OF AIRPLANE SYSTEMS WITHOUT COOLING AIRFLOW CAN RESULT IN DAMAGE TO EQUIPMENT.
 (a)  Set the EQUIP COOLING switch on the P5 overhead panel to OVRD.
 NOTE: The ground crew call horn will operate after
____ approximately 60 seconds, and the EICAS status message EE CLNG OVRD will appear.
 (b)  Make sure the caution message EQUIP COOLING is shown on EICAS.
 NOTE: The EICAS message EQUIP COOLING may not display
____ immediately. Permit at least 4 minutes for the message to display.
 (c)  
Set the EQUIP COOLING switch on the P5 overhead panel to NORM.

 (d)  
Make sure there are no equipment cooling messages shown on EICAS.

 E. Put the Airplane to its Usual Condition
 S 865-087
 (1)  Remove the electrical power, if it is not necessary (Ref 24-22-00/201).
 TASK 21-58-00-705-059
 4. Operational Test - Bypass Valve and Supply/Exhaust Fan Test
___________________________________________________________
 A. References
 (1)  
24-22-00/201, Manual Control

 (2)  
AMM 32-09-02/201, Air/Ground Relay System

 B. Access
 (1)  Location Zone 121 Forward Cargo Compartment Forward Half, LH
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 ALL  ú ú 08 Page 505 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 C.  Prepare for the Test
 S 865-060
 (1)  
Supply electrical power (Ref 24-22-00/201).

 S 865-061

 (2)  
Make sure the EQUIP COOLING selector, on the P5 panel, is in the NORM position.

 S 865-180

 (3)  
Make sure the Ground Test Enable switch on the P461 panel, is in the NORM position.

 D.  Do the Test
 S 715-039
 (1)  Do a test of the fans and the bypass valve.
 (a)  
Make sure that the exhaust fan and the supply fan are on (listen for the sound of each fan).

 (b)  
For an outside ambient temperature of less than approximately 45°F (7°C); make sure air flows from the heat ducts below the forward cargo floor.

 (c)  
For an outside ambient temperature of more than approximately 45°F (7°C); make sure air flows from the ground exhaust valve.

 NOTE: The temperature switch that controls the exhaust path
　
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