(d)  
L EICAS TEST shows at the top of the right side of the two display units.

 (e)  
TEST IN PROGRESS message shows in the message list at the top of the left side of the two display units for approximately 5 seconds.

 (f)  
SELF TEST COMPLETE replaces the TEST IN PROGRESS message.

 (g)  
Make sure NO INTERFACE FAULTS shows and NO INTERNAL FAULTS shows.

 (h)  
All aural indications stop.

 (i)  
CMPTR FAIL and DU FAIL messages do not show.

 (j)  
Red, green, and blue color blocks show on the two displays.

 S 715-018
 (10)
 Push the left master CAUTION switch/light after the TEST OK message (or the SELF TEST COMPLETE message) shows.

 S 715-019

 (11)
 Make sure that both master CAUTION switch/lights go off.

 S 715-066

 (12)
 Make sure that the EICAS program pin codes that follow show for the left (right) computer as applicable:

 (a)  AD05 (A504)
 S 715-003
 (13) Set the COMPUTER switch on the DISPLAY select panel to the R position and do the step before to test the program pin codes for the right EICAS computer.
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 S 715-004
 (14) Make sure that the correct program pin codes show for the right EICAS computer:
 (a)  
AIRPLANES WITH PRE -1000 SERIES EICAS COMPUTERS; All the ENGINE, SUB-SYS, and DISCRETE DISAGREE codes are zero.

 (b)  
Make sure NO INTERFACE FAULTS shows and NO INTERNAL FAULTS shows.

 (c)  
CMPTR FAIL and DU FAIL messages do not show.

 (d)  
Red, green, and blue color blocks show on the two displays.

 S 715-005
 (15)
 Push and release the test switch on the EICAS MAINT panel two times to stop the test mode and start it again.

 S 715-059

 (16)
 Make sure that after 10 seconds, the message TEST OK or SELF TEST COMPLETE shows.

 S 715-006

 (17)
 Push the right master CAUTION switch/lights and make sure that both master CAUTION lights go off.

 (18)
 Set the COMPUTER switch to L.

 (19)
 Make sure that the message TEST OK or SELF TEST COMPLETE shows.

 S 715-021
 S 715-007
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 S 715-008
 (20)
 Push and release each of the switches listed in the table that follows.

 S 715-009

 (21)
　
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本文鏈接地址：757 AMM 飛機維護手冊 儀表 CHAPTER 31 - INSTRUMENTS 2(60)