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Require immediate crew attention. These messages are accompanied by flashing master warning, triple chime attenson with or without voice message or dedicated tone. Require immediate crew awareness and future crew action may be required in the form of alternate system selection or performance limitation. These message are accompanied by flashing master caution and a single chime. Indicate safe or normal system operation which require crew awareness, over and above the dark cockpit philosophy. Indicate minor failures or reduction in systems capability, which require no crew action.

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Quick Links

02/21/24

Message Overview:

Message Name:

STORED FAULTS AND SYSTEM DIAGNOSTIC PAGES MISSING FROM CAIMS

Message Code: 454OBS001
Effectivity: All
System: Central Aircraft-Information Maintenance System (CAIMS)
System Description: 45-45-00 - Central Aircraft Information Maintenance System (CAIMS)
Schematic Diagram: [ G5000 ]  [ Global Express ]  [ Global XRS ] SSM 45-45-00-101 - Central Aircraft-Information Maintenance-System (CAIMS)
Wiring Diagram: [ G5000 ]  [ Global Express ]  [ Global XRS ] WM 45-45-01-1_001 - Sheet 1 - CAIMS to IAC 1 - ALL
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 45-45-01-1_001 - Sheet 1 - CAIMS to IAC 1 - [9002-9139]

Message Description:

After the Central Aircraft-Information Maintenance System (CAIMS) function starts on the Portable Maintenance-Access Terminal (PMAT), the STORED FAULTS and SYSTEM DIAG pages are not available because there is a problem with the interlocks.

Possible Causes:

  • Portable Maintenance Access Terminal (PMAT) (AM-200)
  • Junction Box 3 (JB3)
  • Integrated Avionics Computer 1 (IAC) (A11)
  • Integrated Avionics Computer 2 (IAC) (A10)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Flight Operation Notifications Manual (FONM): None

NOTES:

CAIMS PAGE Displayed on PMAT
Normal Page Missing Menu

Quick Links:

Grounding of the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM10-11-00-867-801
Removal of the Covers and Plugs [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM10-12-00-020-801
Installation of the Covers and Plugs [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM10-12-00-420-801
Standard Aircraft Configuration for Maintenance [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM12-00-00-867-801
Aircraft Walkaround (for Maintenance) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM12-00-00-867-802
Connect Electrical Power to the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-861-801
Remove the Electrical Power from the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-861-802
Electrical/Electronic Safety Precautions [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-910-801
Electrostatic Discharge Safety Precautions [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-910-802
Removal of the Junction Box JB3 [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-01-000-801
Installation of the Junction Box JB3 [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-01-400-801
Removal of the Junction Box JB3 Circuit-Cards [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-02-000-801
Installation of the Junction Box JB3 Circuit-Cards [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-02-400-801
Removal of the Integrated Avionics Computers (IAC) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM31-41-01-000-801
Installation of the Integrated Avionics Computers (IAC) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM31-41-01-400-801
CAIMS PMAT General Instructions [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-801
Access to Active Faults [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-802
Access to Stored Faults [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-803
Access to System Diagnostics [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-804
Flight Deck Effect to Fault Correlations [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-821
PMAT Shutdown [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-01-840-801
Removal of the Portable Maintenance-Access Terminal (PMAT) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-01-000-801
Installation of the Portable Maintenance-Access Terminal (PMAT) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-01-400-801
Wire Repair - Maintenance Practices - ALL [ G5000 ]  [ Global Express ]  [ Global XRS ] SPM20-12-10-02

Troubleshooting Recommendations:

  1. Make sure the CAIMS interlock conditions are met.

    • Aircraft Weight-on-wheels
    • Wheel speed less than 50 knots

  2. Access CAIMS. At the top of the CAIMS window, select "View" and then "Environment Settings". Are both Interlock conditions active (marked with a black dot)?

    1. If only one of the conditions is not met, troubleshoot the related system (WOW or wheel speed) and do close out.
    2. If both conditions are met or are not met, continue with next step.

  3. On the center pedestal reversion control panel, set the SG1 switch to ALTN. Is the fault resolved?

    1. If NO, go to step 7.
    2. If YES, continue with next step.

  4. Remove IAC 1 and Junction Box 3. Perform a continuity check as follows:

    From To Result
    JB3DP1-11F Ground
    JB3DP1-9G Ground

    1. If there is continuity, repair defective wiring as required and do close out.
    2. If there is no continuity, continue with next step.

  5. Perform a continuity check as follows:

    From To Result
    JB3DP1-11F A11AP1-40
    JB3DP1-9G A11AP1-41

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  6. Interchange IAC 1 with IAC 2. Is the fault resolved?

    1. If YES, replace defective IAC and do close out.
    2. If NO, go to step 11.

  7. Remove JB3. Access and disconnect PMAT connector P251. Perform a continuity check as follows:

    From To Result
    P251-13 Ground
    P251-15 Ground

    1. If there is continuity, repair defective wiring as required and do close out.
    2. If there is no continuity, continue with next step.

  8. Perform a continuity check as follows:

    From To Result
    P251-13 JB3DP1-11G
    P251-15 JB3DP1-9H

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  9. Remove PCB1 from JB3. Perform a continuity check inside JB3 as follows:

    From To Result
    JB3DJ1-11G Ground
    JB3DJ1-9H Ground

    1. If there is continuity, replace JB3 and do close out.
    2. If there is no continuity, continue with next step.

  10. Perform a continuity check inside JB3 as follows:

    From To Result
    JB3DJ1-11G P1-57
    JB3DJ1-9H P1-38

    1. If there is no continuity, replace JB3 and do close out.
    2. If there is continuity, continue with next step.

  11. Replace JB3 PCB1. Is the fault resolved?

    1. If YES, do close out.
    2. If NO, continue with next step.

  12. Replace PMAT.
  13. Do close out.
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