07/31/25
Message Overview:
Message Name:
AFT REFUEL/DEFUEL SOV/WRG
Message Code:
284463CPK
Associated CAS:
| Reporting LRU: | Fuel Management and Quantity Gauging Computer (FMQGC) |
| System Description: | 28-23-00 - Refuel/Defuel System |
| Schematic Diagram: | [ Global Express ] [ G5000 ] [ Global XRS ] - 28-23-00 - Refuel/Defuel System |
| Wiring Diagram: | [ Global Express ] [ G5000 ] [ Global XRS ] - 28-23-03 - Refuel/Defuel System |
Message Description:
AFT REFUEL/DEFUEL VALVE/WRG FAULT shows when the conditions that follow occur:
- The Aft Refuel/Defuel Valve is commanded to close
- The open feedback-signal of the Aft Refuel/Defuel Valve is true or the close feedback-signal is false
OR,
- The Aft Refuel/Defuel Valve is commanded to open
- The open feedback-signal of the Aft Refuel/Defuel Valve is false or the close feedback-signal is true
Possible Causes:
- Fuel Management and Quantity Gauging Computer (FMQGC) (A47)
- Aft Refuel Shut-off Valve (L4)
- Junction Box (JB6)
- Junction Box (JB6)/PCB1
- Junction Box (JB6)/PCB2
- Junction Box (JB6)/PCB3
- Auxiliary Power Unit (APU) Start Contactor Assembly (ASCA) (A48)
- Auxiliary Power Unit (APU) Main Battery
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Full Throttle Blog/Forum Articles/Infoservice/Newsletter: None
Flight Operation Notifications Manual (FONM): None
Quick Links:
| Standard Aircraft Configuration for Maintenance | [ G5000 ] [ Global Express ] [ Global XRS ] AMM12-00-00-867-801 |
| Connect Electrical Power to the Aircraft | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-861-801 |
| Electrical/Electronic Safety Precautions | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-910-801 |
| Electrostatic Discharge Safety Precautions | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-910-802 |
| Removal of the Junction Box JB6 | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-13-000-801 |
| Installation of the Junction Box JB6 | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-13-400-801 |
| Removal of the Junction Box JB6 Circuit-Cards | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-14-000-801 |
| Installation of the Junction Box JB6 Circuit-Cards | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-14-400-801 |
| Removal of the Aft Refuel Shutoff-Valve | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-23-33-000-801 |
| Installation of the Aft Refuel Shutoff-Valve | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-23-33-400-801 |
| Removal of the Computer | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-01-000-801 |
| Installation of the Computer | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-01-400-801 |
Troubleshooting Recommendations:
- Disconnect the Aft Refuel/Defuel SOV connector L4P1. Perform the following:
- Apply power to the aircraft
- Set the MASTER switch on the REFUEL/DEFUEL control panel to "ON"
- Set the REFUEL/AUTO REFUEL DEFUEL switch to "REFUEL"
- Set the MANUAL/AFT switch to "CLOSE"
- On Aft R/D SOV connector L4P1, perform a voltage and ground check as follows:
From To Expected Result Result L4P1-B Ground 28 +/-2 VDC L4P1-A Ground Continuity - If all checks are good, go to step 5.
- If there is no continuity on L4P1-A, repair defective wiring as required and do close out.
- If there is no voltage on L4P1-B, continue with next step.
- Access JB6 test points. Perform a voltage and ground check as follows:
From To Expected Result Result JB6 PCB1 TP-92 Ground 28 +/-2 VDC JB6 PCB1 TP-19 Ground Open - If there is continuity on TP-19, investigate wiring and go to step 7.
- If there no voltage on TP-92, use System Schematic 28-23-00 to investigate the power source.
- If all checks are good, continue with next step.
- Perform a voltage check as follows:
From To Expected Result Result JB6 PCB2 TP-36 Ground 28 +/-2 VDC JB6 PCB2 TP-35 Ground 28 +/-2 VDC JB6 PCB3 TP-37 Ground 28 +/-2 VDC JB6 PCB3 TP-36 Ground 28 +/-2 VDC - If all checks are good, investigate wiring between the Aft R/D SOV and JB6 and do close out.
- If PCB3 has no voltage, replace PCB3 and do close out.
- If only PCB2 has no voltage, replace PCB2 and do close out.
- Set the MANUAL/AFT switch to "OPEN". On Aft R/D SOV connector L4P1, perform a voltage check as follows:
From To Expected Result Result L4P1-D Ground 28 +/-2 VDC - If there is voltage, replace the Aft R/D SOV and do close out.
- If there is no voltage, continue with next step.
- Access JB6 test points. Perform a voltage and ground check as follows:
From To Expected Result Result JB6 PCB1 TP-92 Ground 28 +/-2 VDC JB6 PCB1 TP-19 Ground Continuity - If all checks are good, replace JB6 PCB1 and do close out.
- If there no voltage on TP-92, use System Schematic 28-23-00 to investigate the power source.
- If there is no continuity on TP-19, investigate wiring and continue with next step.
- Replace the FMQGC.
- Do close out.