HARDWARE

EICAS Display Formats Schematic (Typical)

Figure 13

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EICAS Self Test Page Format
Figure 14 (Sheet 1)

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LEFT EICAS COMPUTER
PRESENT STATUS
1 PRESENT LEG INTERFACE FAULT REPORTS
1  ARINC 429 RECEIVER FAULT  <SELECTED 
NO  ARINC 429 TRANSMITTER FAULT 
NO  ANALOG DISCRETE OUTPUT FAULT 
NO  FREQUENCY INPUT FAULT 
NO  ANALOG INPUT FAULT 
NO  ANALOG PARAMETER DISAGREE 

NO PRESENT LEG INTERNAL FAULTS
TO ACCESS BITE FUNCTIONS PRESS KEYS: MAN VIEW SELECTED FAULT REPORTS REC RETURN TO SELF TEST PAGE
PRESENT STATUS
(SUMMARY PAGE)

LEFT EICAS COMPUTER
ARINC 429 RECEIVER FAULT RPT 1 OF 1 LEG NUMBER: 0
DETECTED INTERFACE FAULT
ARINC 429 INPUT AVM-L CROSS VALIDITY FAIL
RECORD DATE: 12-22-2003 RECORD TIME: 20:36 AIR/GND: GND THRUST MODE: -
DETAILS:REFERENCE DATA:_______________
EVENT TYPE: HARD FAIL CODE: ---LEFT VALUE: INACTIVE RIGHT VALUE: ACTIVE
TO ACCESS BITE FUNCTIONS PRESS KEYS:
AUTO  VIEW PREVIOUS FAULT REPORT 
MAN  VIEW NEXT FAULT REPORT 
REC  RETURN TO  PRESENT STATUS  PAGE 

PRESENT STATUS (FAULT REPORT PAGE)
EICAS Self Test Page Format
Figure 14 (Sheet 2)

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FAULT HISTORY (FAULT REPORT PAGE)
EICAS Self Test Page Format
Figure 14 (Sheet 3)

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CU TEST/CU MONITOR CODE  BINARY TO HEXADECIMAL CONVERSION  BIT  FAILURE 
( ) 000 0000  0 1 2 3 4 5 6 7 8 9 A B C HEXADECIMAL CODE D E F 2 1 
0  0  0  0  0  0  0  0  1  1  1  1  1  1  1  1  1  CROSS VALIDITY 
0  0  0  0  1 1 1 1  0  0  0  0  1  1 1 1  2  WRAPAROUND 
0  0  1  1  0  0  1  1  0  0  1  1  0  0  1 1  3  NO HANDSHAKE 
0  1  0  1  0  1  0  1  0  1  0  1  0  1  0  1  4  IOC RAM TEST 
　
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本文鏈接地址：757 AMM 飛機維護手冊 儀表 CHAPTER 31 - INSTRUMENTS 2(39)