07/12/19
Message Overview:
Fault Message:
LH FWD AC BOOST PUMP/PRESS SW/WRG
Fault Code:
284460BPK
Associated CAS:
| Reporting LRU: | Fuel Management Quantity and Gauging Computer (FMQGC) |
| System Description: | 28-21-00 |
| Schematic Diagram: | 28-21-00 [ Global Express ] [ G5000 ] [ Global XRS ] 28-22-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 28-21-01 [ Global Express ] [ G5000 ] [ Global XRS ] 28-41-01 [ Global Express ] [ G5000 ] [ Global XRS ] 24-51-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
L FWD AC BST PMP/PRES SWITCH/WRG FL shows on the CAIMS PMAT when the conditions that follow occur:
- The L WING FEED INHIBIT PRI PUMP Push-Button on the FUEL Control Panel is not set to OFF
- The Left Engine is on, the Right Engine is on when the Cross-Feed Valve is open, or the Auxiliary Power Unit (APU) is on when the Cross-Feed Valve is open
- The Left Fwd Boost-Pump Pressure-Indication is low
- The Electrical Management System (EMS)/ AC Power Center (ACPC) has not failedor,
- The L WING FEED INHIBIT PRI PUMP Push-Button on the Fuel Control Panel is set to OFF
- The Left Fwd Boost-Pump Pressure-Indication is high
- The EMS/ACPC has not failedor,
- The Left Engine is off, the Right Engine is off when the Cross-Feed Valve is open, and the APU is off when the Cross-Feed Valve is open
- The Left Fwd Boost-Pump Pressure-Indication is high
- The EMS/ACPC has not failed
Possible Causes:
- Left Fwd AC Boost-Pump Cartridge (B6)
- AC Boost-Pump Canister
- Left Fwd AC Boost-Pump Pressure-Switch (S9)
- Fuel Management and Quantity Gauging Computer (FMQGC) (A47)
- Throttle Quadrant (AP41)
- Fuel Control Panel (AP5)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
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 ] |
| Fuel-System Safety Precautions | AMM 28-00-00-910-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Wing-Tank Access Panels | AMM 28-11-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Wing-Tank Access Panels | AMM 28-11-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the FUEL Control Panel | AMM 28-20-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the FUEL Control Panel | AMM 28-20-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Operational Test of the AC Boost Pumps | AMM 28-21-00-710-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the AC Boost-Pump Cartridges | AMM 28-21-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the AC Boost-Pump Cartridges | AMM 28-21-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the AC Boost-Pump Canisters | AMM 28-21-05-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the AC Boost-Pump Canisters | AMM 28-21-05-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the AC Boost-Pump Pressure-Switches | AMM 28-21-09-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the AC Boost-Pump Pressure-Switches | AMM 28-21-09-400-801 [ 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 System Diagnostics | AMM 45-45-00-970-804 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Leading Edge Panels (BL52.45 to L/E STA 134.818) | AMM 57-41-05-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Leading Edge Panels (BL52.45 to L/E STA134.818) | AMM 57-41-05-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Throttle Quadrant | AMM 76-10-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Throttle Quadrant | AMM 76-10-01-400-801 [ 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:
- Make the following verifications and settings:
- Make sure all APU FADEC, Engine FADEC and AFT PRI PUMP circuit breakers are set to "IN"
- Check that the L WING FEED INHIBIT PRI PUMPS push-button on the Fuel control panel is not off
- On the PMAT, in CAIMS, select the COCKPIT FUEL PANEL PAGE 2
- On the throttle quadrant, put the left ENGINE RUN switch to ON
- On the COCKPIT FUEL PANEL PAGE 2, is the FWD PUMP PRESSURE "Not Low"?
- If YES, go to step 14.
- If NO, continue with next step.
- Check if the message L FUEL LO PRESS
(Caution) displays on the EICAS.- If the message does not display, go to step 17.
- If the message displays, continue with the next step.
- Check if there is 118 ±3 VAC at B6P1 as follows:
Pin Expected Result Result B6P1-A 118 ±3 VAC B6P1-B 118 ±3 VAC B6P1-C 118 ±3 VAC - If there is 118 ±3 VAC, replace the left fwd ac boost-pump cartridge and go to step 19.
- If there is no 118 ±3 VAC, continue with the next step.
- Check if there is a short and open circuit to ground from connector A54P7 as follows:
From To Expected Result Result A54P7-P Ground Continuity A54P7-L Ground Open - If the results are as described in the table above, go to step 20.
- If the results are not as described in the table above, continue with next step.
- Perform a continuity check as follows:
From To Result AP5P1-56 Ground - If there is continuity, go to step 21.
- If there is no continuity, continue with the next step.
- Perform a continuity check as follow:
From To Result AP41P2-38 AP41P2-39 AP41P2-38 AP41P2-46 - If there is no continuity, replace the throttle quadrant and do close out.
- If there is continuity, continue with the next step.
- Put the left ENGINE RUN switch to OFF on the throttle quadrant. Is the FWD PUMP PRESSURE "Low" on the COCKPIT FUEL PANEL PAGE 2 in CAIMS?
- If YES, go to step 12.
- If NO, continue with next step.
- Check if the message L FUEL LO PRESS
(Caution) displays on the EICAS.- If the L FUEL LO PRESS message displays, go to step 22.
- If the L FUEL LO PRESS message does not display, continue with next step.
- Perform a continuity check as follows:
From To Result AP5P1-32 Ground AP5P1-57 Ground - If there is no continuity, go to step 24.
- If there is continuity, continue with next step.
- Perform a continuity check as follow:
From To Result AP5P1-56 Ground - If there is continuity, replace the Fuel control panel and do close out.
- If there is no continuity, continue with next step.
- Perform a continuity check as follows:
From To Result AP41P2-38 AP41P2-46 AP41P2-38 AP41P2-39 - If there is no continuity, replace the throttle quadrant and do close out.
- If there is continuity, repair or replace defective wiring as required between the throttle quadrant and the Fuel control panel and do close out.
- Set the L WING FEED INHIBIT PRI PUMPS push-button on the Fuel control panel to OFF. Is the FWD PUMP PRESSURE "Low" on the COCKPIT FUEL PANEL PAGE 2 in CAIMS?
- If NO, continue with the next step.
- If YES, go to step 25.
- Perform a continuity check as follows:
From To Result AP5P1-32 Ground - If there is no continuity, replace the Fuel control panel and do close out.
- If there is continuity, go to step 28.
- Is the LEFT PRIMARY PUMPS PANEL SWITCH status "INHIBIT" on the COCKPIT FUEL PANEL PAGE 2 in CAIMS?
- If NO, replace Left FWD AC Boost-Pump Pressure-Switch and do close out.
- If YES, continue with next step.
- Perform a continuity check as follows:
From To Result AP5P1-47 Ground - If there is no continuity, continue with the next step.
- If there is continuity, replace the Fuel control panel and do close out.
- Perform a continuity check as follows:
From To Result A47AP1-G12 Ground - If there is no continuity, replace the FMQGC and do close out.
- If there is continuity, repair or replace defective wiring as required between the fuel control panel and the FMQGC and do close out.
- Check if there is continuity between the pins of the connector S9P1 as follow:
From To Expected Result Result S9P1-G S9P1-H Continuity S9P1-A S9P1-H No Continuity - If results are as described in the table above, continue with the next step.
- If the results are not as described in the table above, replace the Left Fwd AC boost-pump pressure-switch and do close out.
- Check for the short and open circuit to ground from FMQGC as follow:
From To Expected Result Result A47AP1-C12 Ground Continuity A47AP1-D12 Ground Open - If the results are as described in the table above, replace the FMQGC and do close out.
- If the results are not as described in the table above, repair or replace defective wiring as required between the Left Fwd AC boost-pump pressure-switch and the FMQGC and do close out.
- Perform the operational test of the ac boost pumps.
- If the operational test is not satisfactory, replace the Left Fwd AC boost-pump canister and do close out.
- If the operational test is satisfactory, do close out.
- Check if there is 118 ±3 VAC on connector A54P10 as follow:
Pin Expected Result Result A54P10-A 118 ±3 VAC A54P10-B 118 ±3 VAC A54P10-C 118 ±3 VAC - If there is no 118 ±3 VAC, go to step 29.
- If there is 118 ±3 VAC, repair or replace the defective wiring between the Left Fwd AC boost-pump and the ACPC and do close out.
- Check if there is a short circuit to ground from AP5P1-57 and an open circuit to ground from AP5P1-32.
From To Expected Result Result AP5P1-57 Ground Continuity AP5P1-32 Ground Open - If the results are as described in the table above, repair or replace the defective wiring between the Fuel control panel and the ACPC and do close out.
- If the results are not as described in the table above, replace the Fuel control panel and do close out.
- Check if there is a continuity between the pins of the connector S9P1 as follow:
From To Expected Result Result S9P1-A S9P1-H Continuity S9P1-G S9P1-H No Continuity - If the results are not as described in the table above, replace the Left Fwd AC boost-pump pressure-switch and do close out.
- If the results are as described in the table above, continue with next step.
- Check if there is a short and open circuit to ground from FMQGC as follow:
From To Expected Result Result A47AP1-D12 Ground Continuity A47AP1-C12 Ground Open - If the results are as described in the table above, replace the FMQGC and do close out.
- If the results are not as described in the table above, repair or replace defective wiring as required between the Left Fwd AC boost-pump pressure-switch and the FMQGC and do close out.
- Perform a continuity check as follows:
From To Result A54P7-L Ground A54P7-P Ground - If there is continuity, repair or replace the defective wiring as required between the Fuel control panel and the ACPC.
- If there is no continuity, go to step 29.
- Is the LEFT PRIMARY PUMPS PANEL SWITCH status "INHIBIT" on the COCKPIT FUEL PANEL PAGE 2 in CAIMS?
- If NO, continue with the next step.
- If YES, do close out.
- Perform a continuity check as follows:
From To Result AP5P1-47 Ground - If there is no continuity, replace the Fuel control panel and do close out.
- If there is continuity, continue with next step.
- Perform a continuity check as follows:
From To Result A47AP1-G12 Ground - If there is continuity, replace the FMQGC and do close out.
- If there is no continuity, repair or replace the defective wiring between the Fuel control panel and the FMQGC.
- Perform a continuity check as follows:
From To Result A54P7-L Ground - If there is no continuity, repair or replace the defective wiring between the Fuel control panel and the ACPC and do close out.
- If there is continuity, continue with next step.
- Perform the applicable troubleshooting for the ACPC.
- Do close out.