(5)
<TROUBLE SHOOT DATA (Ref. Fig. 080) If you push the '<TROUBLE SHOOT DATA' LSK, the screen shows:
-
The date when the failure occurred
-
The time when the failure occurred
-
The failure type
-
The failure class
-
The count of failure occurrence
-
The failure message
-
The port number
-
The bus name
-
The equipment code
-
The system number.
If there are no trouble shooting data, the display shows 'NO
TROUBLESHOOTING DATA AVAILABLE'
(6)
<CLASS 3 FAULTS (Ref. Fig. 081) If you push the '<CLASS 3 FAULTS' LSK, the display shows each class 3 failure detected during the last flight leg with:
-The time when the failure occurred
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page B53 1 1 Config-2 Aug 01/05 1 1 1CES 1
R Previous Leg Report Figure 077A
R 1EFF : 1 1 1CES 151-199, 201-210, 1 111 Page B5431-36-00 Config-2 May 01/05
CFDS - LRU Identification
Figure 078
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page B55 1 1 Config-2 Aug 01/05 1 1 1CES 1
R LRU Identification Figure 078A
R 1EFF : 1 1 1CES 151-199, 201-210, 1 111 Page B5631-36-00 Config-2 May 01/05
CFDS - Ground Scanning Report
Figure 079
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page B57 1 1 Config-2 Aug 01/05 1 1 1CES 1
R Class III Faults Figure 079A
1EFF : 1 1 1CES 151-199, 201-210, 1 111 Page B5831-36-00 Config-2 May 01/05
CFDS - Trouble Shooting Data Menu
Figure 080
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page B59 1 1 Config-2 Aug 01/05 1 1 1CES 1
R Result Power Up Test Figure 080A
R 1EFF : 1 1 1CES 151-199, 201-210, 1 111 Page B6031-36-00 Config-2 May 01/05
CFDS - Last Leg Class 3 Faults
Figure 081
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page B61 1 1 Config-2 Aug 01/05 1 1 1CES 1
-
The ATA reference of the failure
-
The FIN of the component
-
The failure message.
If you push the LSK adjacent to the failure the display shows the
trouble shooting data for the failure.
The display shows a maximum of two failures at a time. If there more
failures, push the next page key on the MCDU keyboard. If there are
no failures, the display shows the message NO FAULT DETECTED.
(7) <TEST (Ref. Fig. 082) If you push the '<TEST' LSK the display shows:
-<AIDS TEST
-<FDIMU BATTERY TEST.
(a) <AIDS TEST If you push the '<AIDS TEST' LSK the FDIMU initiates a complete BITE procedure. If the test is longer than 1 second, the display shows TEST IN PROGRSS xxS (x= approximate maximum waiting time in seconds). If the system has no failures the display shows TEST OK. If faults are detected, the test result menu shows the faulty LRU with:
-
The ATA reference of the failure
-
The FIN of the component
-
The class of the failure
-
The failure message.
If you push the LSK adjacent to the failure class the display
shows the trouble shooting data for the failure.
(b) <FDIMU BATTERY TEST If you push the '<FDIMU DMU BATTERY TEST' LSK the FDIMU initiate a battery test which does not interfere with the normal FDIMU operation. If the test is longer than 1 second, the screen shows the TEST IN PROGRSS xS (x= approximate maximum waiting time in seconds). If the system has no failures the display shows BATTERIES OK. If faults are detected, the test result menu shows the faulty LRU with:
-
The ATA reference of the failure
-
The FIN of the component
-
The class of the failure
-
The failure message.
If you push the LSK adjacent to the failure class the display
shows the trouble shooting data for the failure.
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page B62 1 1 Config-2 Aug 01/05 1 1 1CES 1
R Create Test Figure 081A
R 1EFF : 1 1 1CES 151-199, 201-210, 1 111 Page B6331-36-00 Config-2 May 01/05
CFDS - Test Menus
Figure 082
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page B64 1 1 Config-2 Aug 01/05 1 1 1CES 1 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM 指示/记录系统 3(117)
