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(WARNING)
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WHITE MESSAGE 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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05/16/25

Message Overview:

Message Name:

DCPC RIGHT MICROPROCESSOR CARD-A14

Message Code:

2460414DCP

Reporting LRU: DC Power Center (DCPC)
Associated CAS: ELEC SYS FAULT (Advisory)
System Description: 24-60-00 - DC Electrical Load Distribution
Schematic Diagram: [ G5000 ]  [ Global Express ]  [ Global XRS ] SSM 24-61-00-101 - Primary DC Power Distribution System - Electrical Schematic
Wiring Diagram: [ G5000 ]  [ Global Express ]  [ Global XRS ] WM 24-61-00-1_001 - Sheet 1 - Primary DC Power Distribution System - ALL
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 24-61-01-1_001 - Sheet 1 - DCPC - [9127-9139]
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 24-61-01-1_001 - Sheet 1 - Distribution - ALL

Message Description:

The DC Power Center (DCPC) has detected a malfunction with the Microprocessor Card.

Possible Causes:

  • DC Power Center (DCPC) (A63)/Microprocessor
  • DC Power Center (DCPC) (A63)/Left Microprocessor Card
  • DC Power Center (DCPC) (A63)/Supervisor Card

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Full Throttle Blog/Forum Articles/Infoservice/Newsletter: None

Flight Operation Notifications Manual (FONM): None

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 DC Power Center (DCPC) Fault-Tolerant Supervisor [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-61-01-000-801
Installation of the DC Power Center (DCPC) Fault-Tolerant Supervisor [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-61-01-400-801
Operational Test of the DC Power Center (DCPC) Fault-Tolerant Supervisor [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-61-01-710-801
Removal of the DC Power Center (DCPC) Fault-Tolerant Microprocessor [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-61-05-000-801
Installation of the DC Power Center (DCPC) Fault-Tolerant Microprocessor [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-61-05-400-801
Operational Test of the DC Power Center (DCPC) Fault-Tolerant Microprocessor [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-61-05-710-801
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
Wire Repair - Maintenance Practices - ALL [ G5000 ]  [ Global Express ]  [ Global XRS ] SPM20-12-10-02

Troubleshooting Recommendations:

  1. Interchange the DCPC left microprocessors card with the right microprocessor card.

    1. If system checks are good, replace the defective DCPC microprocessor and do close out.
    2. If fault remains, continue with next step.

  2. On EMS CDU 1, perform a Virgin Start Procedure on the DCPC. DCPC component should be selected at step 4 to only perform the Virgin Start on this component.

    1. If system checks are good, do close out.
    2. If fault remains, continue with next step.

  3. Replace DCPC supervisor card.
  4. Do close out.

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