background
x
loader
Troubleshooting
arrow By ATA By Message Color By Observed Faults By CAIMS By Tips

Select color for CAS message that you wish to troubleshoot

(WARNING)
RED MESSAGE (CAUTION)
AMBER MESSAGE (ADVISORY)
CYAN MESSAGE (STATUS)
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.

This page includes :

For AOG assistance contact:

CRC Montreal (YUL)
Quick Links

07/01/19

Message Overview:

Fault Message:

DCPC TLC3-TTC3 CONTACTOR-K3 PWR UP

Fault Code:

2463008DCP

Associated CAS:

ELEC SYS FAIL
(Caution)

Reporting LRU: DC Power Center (DCPC)
System Description: 24-60-00
Schematic Diagram: 24-61-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 24-61-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

Primary Logic Cards (PLC) detects a discrepancy between coil drive status and auxiliary contact status during Power-up Built-In Test (PBIT).

Possible Causes:

  • DC Power Center (DCPC) Contactor (K3)
  • DC Power Center (DCPC) Motherboard
  • Electromagnetic Interference (EMI) Filter
  • Electronic Module (EM4)
  • Primary Logic Card (PLC) 1
  • Primary Logic Card (PLC) 2
  • Primary Logic Card (PLC) 3
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

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) L-Series Contactor AMM 24-61-53-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the DC Power Center (DCPC) L-Series Contactor AMM 24-61-53-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the DC Power Center (DCPC) Electronic Modules AMM 24-61-65-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the DC Power Center (DCPC) Electronic Modules AMM 24-61-65-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. On the DC synoptic page, make sure ESS TRU2 icon is green and is supplying 28 VDC.
  2. Get access to the DCPC contactor K3.
  3. Disconnect contactor K3 connector P404.
  4. In the cockpit, turn the BATT MSTR SW to ON.
  5. Perform a check for 28 VDC as follows:

    From To Result
    P404-1 Ground
    P404-2 Ground

    1. If there is 28 VDC, go to step 8.
    2. If there is no 28 VDC, continue with next step.

  6. Disconnect EM4 connector P407. Perform a check for 28 VDC as follows:

    From To Result
    P407-23 Ground

    1. If there is 28 VDC, continue with next step.
    2. If there is no 28 VDC, go to step 16.

  7. Perform a continuity check as follows:

    From To Result
    P407-25 P404-1

    1. If there is continuity, replace EM4 and continue with next step.
    2. If there is no continuity, go to step 16.

  8. Perform a continuity check as follows:

    From To Result
    P404-5 Ground
    P404-7 Ground

    1. If there is continuity, repair defective wiring and continue with next step.
    2. If there is no continuity, go to step 16.

  9. Remove PLC 1, PLC 2 and PLC 3.
  10. Perform a continuity check as follows:

    From To Result
    P404-6 Ground
    P404-8 Ground
    P404-22 Ground
    P404-3 Ground

    1. If there is continuity, go to step 16.
    2. If there is no continuity, continue with next step.

  11. Perform a continuity check as follows:

    From To Result
    P404-3 P110C-27
    P404-6 P110A-21
    P404-8 P110B-13
    P404-22 P110C-21
    P404-3 P210C-27
    P404-6 P210A-21
    P404-8 P210B-13
    P404-22 P210C-21
    P404-3 P310C-27
    P404-6 P310A-21
    P404-8 P310B-13
    P404-22 P310C-21

    1. If there is no continuity, go to step 16.
    2. If there is continuity, continue with next step.

  12. Install PLC 2 and PLC 3. Is the fault resolved?

    1. If NO, install PLC 1 and continue with next step.
    2. If YES, replace PLC 1 and do close out.

  13. Remove PLC 2. Is the fault resolved?

    1. If YES, replace PLC 2 and do close out.
    2. If NO, install PLC 2 and continue with next step.

  14. Remove PLC 3. Is the fault resolved?

    1. If YES, replace PLC 3 and do close out.
    2. If NO, continue with next step.

  15. Replace K3.

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

  16. Replace DCPC.
  17. Do close out.

Registered and/or unregistered trademarks of Bombardier Inc. or its subsidiaries. © 2015 Bombardier Inc. All rights reserved.