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 S 865-043
 (1)  Supply electrical power (Ref 24-22-00/201).
 E. Do the Test
 S 735-044
 (1)  Put the static pressure probe into the test port on the E1 shelf and the E2 shelf and measure the static pressure. The minimum acceptable pressure at both locations is 1.7 inches (43 mm) of water.
 NOTE: The above acceptance value is for standard pressure and
____ temperature. Acceptable conditions for measurement are an ambient temperature of 40°F (4°C) to 90°F (32°C) and -1000 to 2000 feet altitude. If the ambient temperature and altitude are outside of this range then the measured pressure value must be corrected to standard conditions.
 (a)  If the pressure in the E1 or the E2 racks is less than 1.7 inches (43 mm) of water, do these checks: 1) Make sure there are no leaks at the pressure gauge and the
 static probe connections. 2) Make sure all the rack mounted equipment is installed. 3) Make sure there are no leaks in and around the equipment
 shelf. 4) Make sure there are no leaks in the air supply ducts. 5) Make sure the air cleaner is clean (Ref 21-58-10/201). 6) Make sure the inlet screens for the supply system and the
 supply fan are not blocked. 7) Make sure the fan check valve is installed correctly. (AMM 21-58-03/401). 8) Make sure the supply fan check valve operates correctly (AMM 21-58-03/601).
 F. Put the Airplane to its Usual Condition
 S 865-089
 (1)  Remove the electrical power, if it is not necessary
 (Ref 24-22-00/201).

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MAINTENANCE MANUAL

 TASK 21-58-00-705-065
 10. System Test - CARGO FIRE Switch Test
____________________________________
 A. General
 (1)  The use of the CMC input monitoring is an alternate test to do the cargo fire switch test.
 B. References
 (1)  
24-22-00/201, Manual Control

 (2)  
25-52-01/401, Containerized Cargo Compartment Ceiling and Sidewall Linings

 (3)  
32-09-02/201, Air/Ground Relay System

 (4)  
AMM 45-10-00/201, Central Maintenance Computer System - Maintenance Practices

 C. Prepare for the Test
 S 865-066
 (1)  Supply electrical power (Ref 24-22-00/201).
 NOTE: When the APU is used for electrical power, make sure that
____ all busses are powered (green) on the EICAS "ELEC" synoptic page.
 S 015-067
 (2)  Remove the sidewall lining from the left side of the forward cargo compartment between Stations 500 and 600 to get access to the supply system (AMM 25-52-01/401).
 S 865-068
 WARNING: YOU MUST CAREFULLY FOLLOW THE STEPS IN THE SPECIFIED TASK TO
_______ PUT THE AIR/GROUND RELAY SYSTEM IN THE AIR MODE. FAILURE TO FOLLOW THE STEPS CORRECTLY CAN CAUSE THE AUTOMATIC OPERATION OF THE AIRPLANE SYSTEMS. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (3)  Do the "Put the Air/Ground Relay System in the Air Mode" task (Ref 32-09-02/201).
 D. Do the Test
 S 735-030
 (1)  Do a test with the cargo fire protection system armed and the airplane in the air mode.
 (a)  Make sure the EQUIP COOLING switch on the P5 overhead panel is set to NORM.
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 CAUTION:_______ DO NOT KEEP THE CARGO FIRE SWITCH IN THE ARMED POSITION
 FOR MORE THAN FIVE MINUTES.  BOTH EQUIPMENT COOLING FANS
 WILL STOP.  EXTENDED OPERATION OF AIRPLANE SYSTEMS WITHOUT

 COOLING AIRFLOW CAN CAUSE DAMAGE TO EQUIPMENT.
 (b)  
Set the CARGO FIRE FWD switch on the P5 overhead panel to ARMED.

 (c)  
Make sure that after 40 seconds these messages are not shown: ~.................................................. | EICAS caution | EQUIP COOLING | .................................................... | EICAS status | EE CLNG OVRD | .................................................... | EICAS status | FLT DK LOW FLOW | .................................................... | EICAS status | EQUIPMENT TEMP | .................................................... | EICAS status | EQUIP LOW FLOW | 2.....................…............................1
　
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