07/12/19
Message Overview:
Fault Message:
RH FWD AC BOOST PUMP/PRESS SW/WRG
Fault Code:
284460EPK
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: | 28-21-02 [ Global Express ] [ G5000 ] [ Global XRS ] 28-41-01 [ Global Express ] [ G5000 ] [ Global XRS ] 24-51-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
R FWD AC BST PMP/PRES SWITCH/WRG FL shows on the CAIMS PMAT when the conditions that follow occur:
- The R WING FEED INHIBIT PRI PUMP Push-Button on the FUEL Control Panel is not set to OFF
- The Right Engine is on, the Auxiliary Power Unit (APU) is on, or the Left Engine is on when the Cross-Feed Valve is open
- The Right Fwd Boost-Pump Pressure-Indication is low
- The EMS/ACPC has not failed
or,
- The R WING FEED INHIBIT PRI PUMP Push-Button on the FUEL control panel is set to OFF
- The right fwd boost-pump pressure-indication is high
- The Electrical Management System (EMS)/AC Power Center (ACPC) has not failed
or,
- The Right 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 Right Fwd Boost-Pump Pressure-Indication is high
- The EMS/ACPC has not failed
Possible Causes:
- AC Boost-Pump Canister
- Right FWD AC Boost-Pump Cartridge (B22)
- Right FWD AC Boost-Pump Pressure-Switch (S15)
- Fuel Management and Quantity Gauging Computer (FMQGC) (A47)
- Throttle Quadrant (AP41)
- Fuel 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 R WING FEED INHIBIT PRI PUMPS pushbutton on the FUEL control panel is not off.
- On the PMAT, in CAIMS, select the COCKPIT FUEL PANEL PAGE 3.
- On the throttle quadrant, put the right ENGINE RUN switch to ON.
- On the COCKPIT FUEL PANEL PAGE 3, is the FWD PUMP PRESSURE "Not Low"?
- If YES, go to step 14.
- If NO, continue with next step.
- Check if the message R FUEL LO PRESS (Caution) displays on the EICAS.
- If the message does not displays, go to step 17.
- If the message displays, continue with the next step.
- Check for the voltage of 118±3 VAC at connector B22P1 as follows:
Pin Expected Result Result B22P1-A 118±3 VAC B22P1-B 118±3 VAC B22P1-C 118±3 VAC - If there is 118±3 VAC, replace the Right 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 A54P3 as follows:
From To Expected Result Result A54P3-P Ground Continuity A54P3-L Ground Open - If the results are not as described in the table above, go to step 20.
- If the results are as described in the table above, continue with the next step.
- Perform a continuity check as follows:
From To Result AP5P2-56 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 AP41P3-38 AP41P3-39 AP41P3-38 AP41P3-46 - If there is no continuity, replace the throttle quadrant and do close out.
- If there is continuity, repair or replace the defective wiring as required between the FUEL control panel and the throttle quadrant and continue with the next step.
- Put the right ENGINE RUN switch to OFF on the throttle quadrant. Is the FWD PUMP PRESSURE "Low" on the COCKPIT FUEL PANEL PAGE 3 in CAIMS?
- If YES, go to step 12.
- If NO, continue with next step.
- Check if the message R FUEL LO PRESS (Caution) displays on the EICAS.
- If the R FUEL LO PRESS message displays, go to step 22.
- If the R FUEL LO PRESS message does not display, continue with next step.
- Perform a continuity check as follows:
From To Result AP5P2-32 Ground AP5P2-57 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 AP5P2-56 Ground - If there is no continuity, replace the FUEL control panel and do close out.
- If there is continuity, continue with next step.
- Perform continuity check as follows:
From To Result AP41P3-38 AP41P2-46 AP41P3-38 AP41P2-39 - If there is no continuity, replace the throttle quadrant and do close out.
- If there is continuity, repair or replace the defective wiring as required between the throttle quadrant and the FUEL control panel and do close out.
- Set the R 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 3 in CAIMS?
- If YES, go to step 25.
- If NO, continue with the next step.
- Perform a continuity check as follows:
From To Result AP5P2-32 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 RIGHT PRIMARY PUMPS PANEL SWITCH status "INHIBIT" on the COCKPIT FUEL PANEL PAGE 3 in CAIMS?
- If NO, replace Right 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 AP5P2-47 Ground - If there is continuity, replace the FUEL control panel and do close out.
- If there is no continuity, continue with the next step.
- Perform a continuity check as follows:
From To Result A47DP1-E15 Ground - If there is no continuity, replace the FMQGC and do close out.
- If there is continuity, repair or replace the defective wiring as required between the fuel control panel and the FMQGC and do close out.
- Check if there is continuity within Right FWD AC Boost-Pump Pressure-Switch as follows:
From To Expected Result Result S15P1-G S15P1-H Continuity S15P1-A S15P1-H No Continuity - If the results are not as described in the table above, replace the Right Fwd AC Boost-Pump Pressure-Switch and do close out.
- If the results are as described in the table above, continue with the next step.
- Check for the short and open circuit to ground from FMQGC as follow:
From To Expected Result Result A47DP1-A15 Ground Continuity A47DP1-B15 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 the defective wiring as required between the Right 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 Right Fwd AC Boost-Pump Canister and do close out.
- If the operational test is satisfactory, do close out.
- Check for the voltage of 118±3 VAC at connector A54P9 as follow:
Pin Expected Result Result A54P9-A 118±3 VAC A54P9-B 118±3 VAC A54P9-C 118±3 VAC - If there is 118±3 VAC, repair or replace the defective wiring as required between the Right Fwd AC Boost-Pump and the ACPC and do close out.
- If there is no 118±3 VAC, perform the applicable troubleshooting for the ACPC and continue with next step.
- Check for the short and open circuit to ground from Fuel Panel as follow:
From To Expected Result Result AP5P2-57 Ground Continuity AP5P2-32 Ground Open - If the results are as described in the table above, repair or replace the defective wiring as required 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 for the continuity within Right Fwd AC Boost-Pump pressure-Switch as follow:
From To Expected Result Result S15P1-A S15P1-H Continuity S15P1-G S15P1-H No Continuity - If the results are not as described in the table above, replace the Right 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 A47DP1-B15 Ground Continuity A47DP1-A15 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 the defective wiring as required between the Right Fwd AC Boost-Pump Pressure-Switch and the FMQGC and do close out.
- Perform a continuity check as follows:
From To Result A54P3-L Ground A54P3-P Ground - If there is continuity, repair or replace the defective wiring as required between the FUEL control panel and the ACPC and do close out.
- If there is no continuity, perform the applicable troubleshooting for the ACPC.
- Is the RIGHT PRIMARY PUMPS PANEL SWITCH status "INHIBIT" on the COCKPIT FUEL PANEL PAGE 3 in CAIMS?
- If YES, do close out.
- If NO, continue with the next step.
- Perform a continuity check as follows:
From To Result AP5P2-47 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-E15 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 A54P3-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.
- Replace ACPC.
- Do close out.