06/12/19
Message Overview:
Fault Message:
HUMIDIFIER OUTPUT DISAGREE
Fault Code:
2163614ECS
Associated CAS:
| Reporting LRU: | Humidifier Control Unit (HCU) |
| System Description: | 21-71-00 |
| Schematic Diagram: | 21-71-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 21-71-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
The Humidifier Control Unit (HCU) has detected that the H_TAV OR HWSOV OR HWFV OR HDV commands are in disagree with their feedback. This is an HCU internal failure.
Possible Causes:
- Humidifier Control Unit (HCU) (A248)
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter:
Quick Links:
| Functional Test of the Humidifier System | AMM 21-71-00-720-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Humidifier Control Unit | AMM 21-71-17-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Humidifier Control Unit | AMM 21-71-17-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- Replace HCU.
- Do close out.
NOTE: Perform Functional Test of the Humidifier System (TASK 21-71-00-720-801) to confirm the system integrity.This task is the approved Return to Service (RTS) Test for the Humidifier System.
If the operator which to operate the humidifier on the ground as it operates in flight, then use the following attached procedure. Please note that the attached procedure is not approved for RTS and can only be used for troubleshooting purpose. Please note that the 3.5 hours delay can not be bypassed in this procedure.
Humidifier Operation with Aircraft W off W (3.5 hours delay activation).