07/22/19
Message Overview:
| DDG Reference: | 28-40-02 |
| Pilot Action (QRH): | STATUS - 3 |
| System Description: | 28-21-00 |
| Schematic Diagram: | 28-21-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 28-41-08 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
L PRI PUMPS OFF (Status) shows when the conditions that follow occur:
- The L WING FEED INHIBIT PRI PUMPS switch on the FUEL control panel is set to OFF.
- The left aft boost-pump pressure is low.
- The left forward boost-pump pressure is low.
This troubleshooting applies when it is not under normal conditions.
Possible Causes:
- L WING FEED INHIBIT PRI PUMPS Switch (SDS2)
- Fuel Control Panel (AP5)
- Fuel Management and Quantity Gauging Computer (FMQGC) (A47)
- Ground Stud (GS852)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
Quick Links:
| Removal of the Fuel Management and Quantity Gauging Computer (FMQGC) | AMM 28-41-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Fuel Management and Quantity Gauging Computer (FMQGC) | AMM 28-41-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the fuel control panel (AP5) | AMM 28-20-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the fuel control panel (AP5) | AMM 28-20-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair | SPM 20-12-10 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
The L PRI PUMPS OFF (Status) CAS does not display when the L PRI PUMPS switch is turned OFF.
- Turn ON aircraft power and the CAIMS PMAT.
- Access CAIMS.
- Select System Diagnostics.
- Select 28-00 Fuel.
- Select Computer (FMQGC CH A(B))
- Select LRU Test.
- Select Cockpit fuel panel data - CH A(B).
- Scroll through the pages and find Left Primary Pumps Panel Switch:
- On the Fuel control panel (AP5) select the L PRI PUMP switch.
- Does the pump status change from INHIB to ON and ON to INHIB on the CAIMS page?
- If the status changes, then go to step 10.
- If the status does not change, continue with the next step.
- Gain access to the FMQGC (A47) and remove FMQGC from the tray.
- Perform the wiring continuity test per the table below:
SWITCH POSITION FROM TO EXPECTED RESULT RESULT L PRI PUMPS (OFF) A47AP1 - G12 Airframe Ground Continuity - If the wiring check is good, go to step 10.
- If the wiring check is not good, then continue with next step.
- Remove the fuel control panel (AP5), disconnect AP5P1.
- Perform the wiring continuity test per the table below:
FROM TO EXPECTED RESULT RESULT AP5J1 - 47 AP5J1 - 15 Continuity AP5P1 - 15 Airframe Ground Continuity - If the wiring from AP5J1 - 47 to AP5J1 - 15 is not good, suspect the L PRIMARY FUEL PUMP Switch (SDS2), or the Fuel Control Panel.
- If the wiring from AP5P1 - 15 to airframe ground is not good then repair or replace wiring to GS852, or GS852.
- If the wiring check is good then continue with the next step.
- Perform the wiring continuity test per the table below:
FROM TO EXPECTED RESULT RESULT AP5P1 - 47 A47AP1 - G12 Continuity - If the wiring check is good go to next step.
- If the wiring check is not good then repair or replace wiring between Fuel Control Panel and FMQGC.
- Re-install or Re-rack the FMQGC making sure it is fully and properly pushed into place. Is the fault still present?
- If the CAS does not display, go to next step.
- If the CAS displays, then do close out.
- Suspect the FMQGC (A47).
- Do close out.