06/28/19
Message Overview:
Fault Message:
DCPC PRIMARY LOGIC CARD #1-A9 FAIL
Fault Code:
2460409DCP
Associated CAS:
| Reporting LRU: | DC Power Center (DCPC) |
| System Description: | 24-60-00 |
| Schematic Diagram: | 24-32-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 24-32-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
- If one of the three Primary Logic Cards does not agree then a Primary Logic Card fault will be generated.
- If capacity of the Avionic Battery is weak then a Primary Logic Card(s) fault will be generated.
Possible Causes:
- Primary Logic Card (PLC) (p/o A63)
- Avionics Battery (A182)
- Battery/Ram-Air Turbine Interface (BATT/RAT I/F) Card (p/o A20)
- DC Power Center (DCPC) (A63)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
Quick Links:
| Restoration of the Avionics Battery | AMM 24-32-01-610-802 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Avionics Battery | AMM 24-32-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Avionics Battery | AMM 24-32-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the DC Power Center (DCPC) | AMM 24-61-00-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the DC Power Center (DCPC) | AMM 24-61-00-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the DC Power Center (DCPC) Primary Logic | AMM 24-61-09-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the DC Power Center (DCPC) Primary Logic | AMM 24-61-09-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the DC Power Center (DCPC) Battery/Ram-Air-Turbine Interface Unit | AMM 24-61-33-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the DC Power Center (DCPC) Battery/Ram-Air-Turbine Interface Unit | AMM 24-61-33-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| DC Power Center (DCPC) Assembly | CMM 24-61-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- On the PMAT, gain access to CAIMS active faults. Are any of the following messages posted?
- If YES, troubleshoot CAIMS message first.
- If NO, continue with next step.
- Swap PLC 1 with PLC 2. Did the fault follow to PLC 2?
- If YES, replace PLC 1 and do close out.
- If NO, continue with next step.
- Does the fault occur during APU start?
- If NO, go to step 5.
- If YES, continue with next step.
- Remove avionics battery and install a serviceable Avionic Battery for test purposes. Start APU and monitor the fault. Is the fault resolved?
- If YES, send the avionics battery to the battery shop and service the avionics battery.
- If NO, continue with next step.
- Remove PLC 1 and the BATT/RAT card in the DCPC. Perform a continuity check between both cards as follows:
From To Result P110C-50 P410A-46 - If there is no continuity, go to step 8.
- If there is continuity, continue with next step.
DCP DCPC PRIMARY LOGIC CARD
- Perform a continuity check as follows:
From To Result P110C-50 Ground - If there is continuity, go to step 8.
- If there is no continuity, continue with next step.
- Replace the BATT/RAT Interface card. Is the fault resolved?
- If YES, do close out.
- If NO, continue with next step.
- Replace DCPC.
- Do close out.