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

08/05/19

Message Overview:

Fault Message:

DAU 4B POWER FAULT

Fault Code:

3148169DAU

Associated CAS:

None

Reporting LRU: Data Acquisition Unit (DAU) 4
System Description: 31-40-00
Schematic Diagram: 31-42-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 31-42-04 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

The Data Acquisition Unit (DAU) 4 senses a fault in the System that supplies its power.

Possible Causes:

  • Secondary-Power Distribution Assembly (SPDA) 4 (A16)
  • Data Acquisition Unit (DAU) 4 (A31)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Connect Electrical Power to the Aircraft AMM 24-00-00-861-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Remove the Electrical Power from the Aircraft AMM 24-00-00-861-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Opening of Non-Thermal Circuit Breakers AMM 24-00-00-863-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Closing of Non-Thermal Circuit Breakers AMM 24-00-00-863-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Electrical/Electronic Safety Precautions AMM 24-00-00-910-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Electrostatic Discharge Safety Precautions AMM 24-00-00-910-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Operational Test of the Secondary-Power
Distribution Assembly 4
AMM 24-62-01-710-804 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Data Acquisition Units (DAU) AMM 31-42-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Data Acquisition Units (DAU) AMM 31-42-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Access to Active Faults AMM 45-45-00-970-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the External Avionics-Compartment
Access-Panel (140BB)
AMM 52-45-11-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the External Avionics-Compartment
Access-Panel (140BB)
AMM 52-45-11-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Safety Precautions - Maintenance Practices - ALL SPM 20-00-01-02 [ 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 EMS CDU, make sure that DAU CH 4B is set to "IN".

    1. If the circuit breaker is not set to "IN", investigate the reason and if possible, set it to "IN" and do close out.
    2. If the circuit breaker is set to "IN", continue with next step.

  2. Remove the DAU 3 and perform a 28 VDC voltage check on DAU 4 connector A31BP1 as follows:

    DAU 4 Expected Result Result
    A31BP1-A14 28 VDC

    1. If there is no 28 VDC, go to step 4.
    2. If there is 28 VDC, continue with next step.

  3. Perform a continuity check as follows:

    From To Result
    A31BP1-A15 Ground
    A31BP1-K15 Ground

    1. If there is continuity, go to step 6.
    2. If there is no continuity, repair or replace defective wiring as required and do close out.

  4. Perform a continuity check as follows:

    From To Result
    A31BP1-A14 A16P1-B
    A31BP1-A15 Ground
    A31BP1-K15 Ground

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

  5. Perform a continuity check as follows:

    From To Result
    A31BP1-A14 Ground

    1. If there is continuity, repair or replace defective wiring as required and do close out.
    2. If there is no continuity, investigate the SPDA power source and do close out.

  6. Replace DAU 4.
  7. Do close out.
Registered and/or unregistered trademarks of Bombardier Inc. or its subsidiaries. © 2015 Bombardier Inc. All rights reserved.