07/12/19
Message Overview:
Fault Message:
GROUND RDCP/WRG
Fault Code:
2844604PK
Associated CAS:
| Reporting LRU: | Fuel Management and Quantity Gauging Computer (FMQGC) |
| System Description: | 28-23-00 |
| Schematic Diagram: | 28-23-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 28-23-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
The Fuel Management Quantity and Gauging Computer (FMQGC) cannot sense the REFUEL/DEFUEL Control Panel (RDCP) data busses.
Possible Causes:
- Junction Box (JB6)/PCB1
- Junction Box (JB6)/PCB3
- Auxiliary Power Unit (APU) Start Contactor Assembly (ACSA) (A48)
- Refuel/Defuel Control Panel (RDCP) (A46)
- Refuel/Defuel Control Panel (RDCP) (A213)
- Fuel Management Quantity and Gauging Computer (FMQGC) (A47)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin:
- 700-28-002 - Modification - Refuel/Defuel System - Addition of Refuel/Defuel Control Panel in Flight Compartment
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 ] |
| Removal of the Junction Box JB6 Circuit-Cards | AMM 24-00-14-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Junction Box JB6 Circuit-Cards | AMM 24-00-14-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the REFUEL/DEFUEL Control Panel | AMM 28-23-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the REFUEL/DEFUEL Control Panel | AMM 28-23-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Operational Test of the Refuel/Defuel Control Panel | AMM 28-23-01-710-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Computer | AMM 28-41-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Computer | AMM 28-41-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Access to Active Faults | AMM 45-45-00-970-802 [ 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:
- In the CAIMS PMAT navigate to check the status of the ground Refuel Defuel Control Panel (RDCP).
- CAIMS
- System Diagnostics
- 28-00 Fuel
- Computer (FMQGC CH. A(B))
- LRU TEST
- RDCP AND REFUEL VALVES DATA - CH. A
- Go to page 2 for the RDCP AND REFUEL VALVES DATA - CH. A data page. Turn ON the ground RDCP panel.
- If the CAIMS does the discrete display OFF, go to step 4.
- If the CAIMS discrete displays ON, continue with next step.
- Swap the Cockpit RDCP with the Ground RDCP.
NOTE: If A/C has dual RDCP's then complete this step, If not go to next step.- If system checks are good, replace Cockpit RDCP and do close out.
- If fault remains, continue with next step.
- Disconnect connector A46P1 at the ground RDCP. Add a jumper wire and connect to pins 2 and 3. Perform wiring check as follows:
From To Expected Result Result A46P1-12 A46P1-18 28 VDC A46P1-13 A46P1-17 28 VDC A46P1-18 Airframe Ground Continuity A46P1-17 Airframe Ground Continuity - If wiring checks are good, go to step 6.
- If wiring checks are not good, repair defective wiring as required and continue with next step.
- Reconnect A46P1 at the ground RDCP. Perform wiring check at the APU Start Contactor Assembly (ASCA).
From To Expected Result Result A48J1-T Airframe Ground 28 VDC A48J1-U Airframe Ground 28 VDC - If wiring checks are not good, replace CB-A1 or CB-A3 or suspect the (ASCA) and do close out.
- If wiring checks are good, continue with next step.
- Perform wiring check at JB6 for PCB1.
From To Expected Result Result TP-60 TP-30 28 VDC TP-61 TP-30 28 VDC TP 59 TP-30 28 VDC TP-30 Airframe ground Continuity - If TP-30 does not have a ground, repair GS67 or repair defective wiring and do close out.
- If TP-59 has power and TP-61 does not have power, replace PCB1 in JB6 and do close out.
- If TP-59 does not have 28 VDC, repair wiring to FMQGC or replace FMQGC and do close out.
- If wiring checks are good, continue with next step.
- Perform wiring check at JB6 for PCB3.
From To Expected Result Result TP-31 Airframe ground 28 VDC TP-56 Airframe ground Ground - If wiring checks are not good, replace PCB3 in JB6 or repair defective wiring and do close out.
- If wiring checks are good, continue with next step.
- Turn OFF aircraft power and rerack the FMQGC making sure it is fully and properly pushed into place. Is the fault still present?
- If NO, do close out.
- If YES, continue with next step.
- Replace the FMQGC.
- Do close out.