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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本文链接地址：757 AMM 飞机维护手册 仪表 CHAPTER 31 - INSTRUMENTS 2(39)
