R 1EFF : 062-099, 106-149, 151-199, 201-299, 1 46-21-00Page 83 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 ATIMS - PREVIOUS LEGS REPORT Page
 Figure 019

R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 46-21-00Page 84 1401-499, 1Aug 01/05 1 1 1CES 1

 ATIMS - LRU IDENTIFICATION Page
 Figure 020

R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 46-21-00Page 85 1401-499, 1Aug 01/05 1 1 1CES 1

 ATIMS - GROUND SCANNING Page
 Figure 021

R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 46-21-00Page 86 1401-499, 1Aug 01/05 1 1 1CES 1

R  **ON A/C 062-099, 106-149, 151-199, 201-299, 301-399, 401-499,
 This function is based on the monitoring and the fault analysis during the flight and enables consultation of the ATIMS failure recordings. The ATSU peripheral monitoring and internal cyclic tests are used in order to detect transient failures.
 (f) TROUBLE SHOOTING DATA page 
R  **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 022) 
R  **ON A/C 062-099, 106-149, 151-199, 201-299, 301-399, 401-499,
 This function provides correlation parameters and snapshot data concerning the failure displayed in the LAST LEG REPORT and the PREVIOUS LEGS REPORT pages.
 (g) CLASS 3 FAULTS page 
R  **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 023) 
R  **ON A/C 062-099, 106-149, 151-199, 201-299, 301-399, 401-499,
 This menu enables to display the Class 3 faults recorded during the last flight leg.
 (h) SYSTEM TEST page 
R  **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 024) 

R 1EFF : 062-099, 106-149, 151-199, 201-299, 1 46-21-00Page 87 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 ATIMS - TROUBLE SHOOTING DATA Page
 Figure 022

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 ATIMS - CLASS 3 FAULT Page
 Figure 023

R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 46-21-00Page 89 1401-499, 1Aug 01/05 1 1 1CES 1

 ATIMS - SYSTEM TEST Page Figure 024 (SHEET 1)
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 46-21-00Page 90 1401-499, 1Aug 01/05 1 1 1CES 1

 ATIMS - SYSTEM TEST Page Figure 024 (SHEET 2)
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 46-21-00Page 91 1401-499, 1Aug 01/05 1 1 1CES 1

R  **ON A/C 062-099, 106-149, 151-199, 201-299, 301-399, 401-499,
 The ATIMS BITE test is initiated when pressing the line key adjacent to the SYSTEM TEST indication. The test ends with the display of the following message on the MCDU: - TEST OK indication when all the tests are completed and no failure has been detected - or the failure message(s) when one or more failures have been detected.
 (i) GROUND REPORT page 
R  **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 025) 
R  **ON A/C 062-099, 106-149, 151-199, 201-299, 301-399, 401-499,
 This function is used to present Class 1, 2 or 3 internal failures when they are detected on ground. The relevant trouble shooting data are displayed by pressing the line key adjacent to the failure indication. These failures differ from those displayed on the LAST LEG REPORT page.
 (j) SPECIFIC DATA page 
R  **ON A/C 106-149, 151-156, 159-199, 201-299, 301-399, 401-499, 
R  Post SB  46-1013 For A/C 151-156,201-209,
R  (Ref. Fig. 026) 
R  **ON A/C 062-099, 106-149, 151-199, 201-299, 301-399, 401-499,
 This menu enables acces to different functions: - 1L : LOAD STATUS (available in Pre-FANS+ configuration only) - 2L : PIN PROGRAMMING to check the ATSU configuration with its parity validity. 

R 1EFF : 062-099, 106-149, 151-199, 201-299, 1 46-21-00Page 92 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 ATIMS - GROUND REPORT Page
 Figure 025

R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 46-21-00Page 93 1401-499, 1Aug 01/05 1 1 1CES 1

 ATIMS - SPECIFIC DATA Page R Figure 026
R 1EFF : 106-149, 151-156, 159-199, 201-299, 1 46-21-00Page 94 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1 NOTE : The order of the pin programming display is in accordance

____ with the one of the ATSU input connector:
 -a pin programming not defined (spare) is displayed with a zero value.
 -an active pin programming is displayed with a 1 value.
 -3L : DUMP TSD
 -4L : SW P/N PRINT OUT
　
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