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

01/11/22

Message Overview:

Message Name:

TRU 1 FAN FAILED

Message Code:

2460460DCP

Associated CAS:

ELEC SYS FAULT
(Advisory)

Reporting LRU: DC Power Center (DCPC)
System Description: 24-31-00
Schematic Diagram: [ Global Express ]  [ G5000 ]  [ Global XRS ] 24-31-00 DC Power Conversion System
[ Global Express ]  [ G5000 ]  [ Global XRS ] 24-51-00 AC Load Distribution AC Power Center (ACPC) System
[ Global Express ]  [ G5000 ]  [ Global XRS ] 24-52-00 AC Load Distribution Cockpit Circuit Breaker Panel (CCBP) System.
Wiring Diagram: [ Global Express ]  [ G5000 ]  [ Global XRS ] 24-31-01 Transformer Rectifiers
[ Global Express ]  [ G5000 ]  [ Global XRS ] 24-51-00 ACPC Distribution Left
[ Global Express ]  [ G5000 ]  [ Global XRS ] 24-51-00 ACPC Distribution Right
[ Global Express ]  [ G5000 ]  [ Global XRS ] 24-52-01 Cockpit Circuit Breaker Panel (CCBP)

Message Description:

The Transformer Rectifier Unit (TRU) 1 Fan Speed Sensor is low or no Fan output to the DC Power Center (DCPC).

Possible Causes:

  • DC Power Center (DCPC) (A63)
  • DC Power Quality Monitor (DCPQM) Card 1
  • Transformer Rectifier Unit (TRU) 1 (A73)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

NOTE: The TRU 1 fan fail will show on the DC synoptic page, as the TRU 1 outline will be amber and the TRU output voltage is approximately 28 VDC.
NOTE: If the TRU voltage displayed on the DC synoptic page is different than 28 VDC, check that all three 115 VAC input phases are present. A missing phase could result in the fan not spinning.
NOTE: Verify C/B status on both pilot and copilot EMS CDUs. This Fault Message will post if either of the following circuit breaker or Smart Contactor status is OUT or Tripped.

LOCATION CB NO. NAME
CCBP (A54) CB-G12 TRU BAY FAN
ACPC (A35) SC-K15 AC 1 FEED

Quick Links:

Removal of the Transformer Rectifier Units AMM 24-31-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Transformer Rectifier Units AMM 24-31-01-400-801 [ 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) DC Power Quality Monitor AMM 24-61-13-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the DC Power Center (DCPC) DC Power Quality Monitor AMM 24-61-13-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Access to Active Faults AMM 45-45-00-970-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Access to Stored Faults AMM 45-45-00-970-803 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Check status of AC 1 FEED on EMS CDU, the AC 1 Feed being out or tripped can drive multiple CAS to post.
    BUS > AC 1 > AC 1 FEED.

    1. If AC 1 FEED CB is IN go to step 3.
    2. If AC 1 FEED CB is OUT, set to IN.

      AC 1 FEED
      CB SYSTEM PHASE CAS
      CB-G6 ESS TRU 1 3 AC BUS 1 FAIL (Caution)
      CB-G3 EVS FAIRING HEAT 3 EVS HEAT FAIL (Caution)
      CB-G9 SLAT/FLAP PWR 1 3 SLAT-FLAP HALFSPD (Advisory)
      CB-H5 EVS WINDOW HEAT 1 EVS HEAT FAIL (Caution)
      CB-H6 A/T CTLR 1 A/T 1 FAIL (Advisory)
      A/T 2 FAIL (Advisory)
      CB-H7 PITOT 1 HT A 1 PITOT 1 HT FAIL (Caution)
      CB-H8 R ICE DETECTOR 1 ICE DETECTOR FAULT (Advisory)
      CB-H9 R AOA HEAT A 1 R AOA HEAT FAIL (Caution)
      CB-H10 L WSHLD HEAT 1 1 L WSHLD HEAT FAIL (Caution)
      CB-H11 L WSHLD HEAT 2 1 L WSHLD HEAT FAIL (Caution)
      CB-G12 TRU BAY FAN 3 ELEC SYS FAULT (Advisory)
      2460460DCP TRU 1 FAN FAILED
      CB-B6 STAB TRIM CH1 3 STAB CH 1 FAIL (Advisory)

  2. Did the CAIMS Fault & CAS messages clear after setting AC 1 FEED CB to IN.

    1. If YES, do close out.
    2. If NO, go to next step.
    3. Get Access to the FWD bay to check for the airflow of the TRU 1 and confirm if the fan is rotating or not.

      1. If the fan is not rotating, replace TRU 1 and do close out.
      2. If the fan is rotating, continue with next step.

    4. Interchange TRU 1 with another TRU. Is the fault still present?

      1. If YES, continue with next step.
      2. If NO, replace defective TRU.

    5. Disconnect TRU 1 connector A73P1 and DCPC connector A63P1. Perform a continuity check as follows:

      From To Result
      A73P1-D 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.

    6. Perform a continuity check as follows:

      From To Result
      A73P1-D A63P1-A

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

    7. Access the DCPC Logic assembly and remove the DCPQM 1 card. Perform a continuity check as follows:

      From To Result
      A63P1-A Ground

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

    8. Perform a continuity check as follows:

      From To Result
      A63P1-A P121A-10

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

    9. Replace the DCPQM 1 card.

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

    10. Replace DCPC.
    11. Do close out.

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