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时间:2011-10-29 12:39来源:蓝天飞行翻译 作者:航空
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11J3, EICAS UPPER DSPL

 (c)  
11J29, EICAS CMPTR RIGHT

 (d)  
11J30, EICAS LOWER DSPL

 (e)  
11J31, EICAS DSPL SW

 (f)  
11J32, EICAS DSPL SELECT

 


 S 862-115
 (3)  AIRPLANES WITH PREDICTIVE WINDSHEAR; Open these circuit breakers on the overhead circuit breaker panel, P11, and attach DO-NOT-CLOSE tags:
 (a)  
11F2, WX RADAR L

 (b)  
AIRPLANES WITH DUAL WEATHER RADAR R/T'S;
 11F27, WX RADAR R

 

 S 752-100
 (4)  Do the steps that follow to show the fault reporting pages:
 (a)  
Push the TEST switch on the EICAS MAINT panel.

 (b)
Push the MAN switch twice to show PRESENT STATUS faults.


 NOTE:____Stop for 1 to 3 minutes. Some faults have time delays.
 NOTE: The PRESENT STATUS page will only show if there are
____ faults. The display will not change if there are no faults.
  ú

 31-41-00
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A

757 MAINTENANCE MANUAL
 1)  Follow the instruction on the screen to show the fault reporting page(s).
 (c)  Push the AUTO switch twice to show FAULT HISTORY faults.
 NOTE: The FAULT HISTORY page will only show if there are
____ faults. The display will not change if there are no faults.
 1)  Follow the instruction on the screen to show the fault reporting page(s).
 S 862-116
 (5)  AIRPLANES WITH PREDICTIVE WINDSHEAR; Close these circuit breakers on the overhead circuit breaker panel, P11, and remove the DO-NOT-CLOSE tags:
 (a)  
11F2, WX RADAR L

 (b)  
AIRPLANES WITH DUAL WEATHER RADAR R/T'S; 11F27, WX RADAR R


 S 862-101
 (6)  Remove electrical power if it is not necessary (AMM 24-22-00/201).
 TASK 31-41-00-752-107
 8.  How to Clear EICAS Faults from the Fault Reporting Pages________________________________________________________
 A.  General
 (1)  
After you repair an EICAS fault, you must remove it from the fault reporting pages.

 (2)  
This task shows how to remove EICAS faults from the fault reporting pages.

 (3)  
The fault reporting pages contain either PRESENT STATUS faults or FAULT HISTORY faults.

 (a)  
The PRESENT STATUS faults occurred during flight leg 0.

 (b)  
The FAULT HISTORY faults occurred during flight leg 1 through flight leg 9.

 


 B.  References
 (1)  24-22-00/201, Electrical Power Control
  ú

 31-41-00
 ALL  ú ú 10 Page 211 ú Sep 28/01
 
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