07/19/19
Message Overview:
| DDG Reference: | 28-21-00 |
| Pilot Action (QRH): | FUEL 09-19 |
| System Description: | 28-21-00 |
| System Schematic: | 28-21-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 28-21-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
Both forward & aft PRI (AC) pumps on the left side have failed.
Possible Causes:
- AC Power Center (ACPC) Solid State Power Controller (SSPC) 1
- ACPC SSPC 6
- Throttle Quadrant Assembly (TQA) (AP41)
- L Engine RUN Switch (1S1)
- Fuel Management Quantity and Gauging Computer (FMQGC) (A47)
- Left Fwd AC Boost Pump (B6)
- Left Aft AC Boost Pump (B7)
- Left Fwd AC Boost Pump Pressure Switch (S9)
- Left Aft AC Boost Pump Pressure Switch (S10)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin:
- AW700-28-0368 - No Fault Found initiative: Fuel Management and Quantity Gauging Computer (FMQGC)
- AW700-28-0469 - Fuel Management and Quantity Gauging Computer Tray Connector Inspection
Forum Articles/Infoservice/Newsletter: None
NOTE: If the Left Primary AC pumps and the Left DC Aux pumps are showing inoperative after engine shutdown, go to Troubleshooting Recommendations step 2.
Quick Links:
| Access to CAIMS Active Faults | AMM 45-45-00-970-802 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the FMQGC | AMM 28-41-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the FMQGC | AMM 28-41-01-400-801 [ 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 ] |
Troubleshooting Recommendations:
- Access CAIMS Active Faults and select displayed message from menu below:
- If the left primary AC pumps and the left DC aux pumps are showing inoperative after engine shutdown, continue with next step
- With the LH FUEL CUTOFF switch in the OFF position, check for continuity to ground between FMQGC connector A47AP1 pin H12 and ground.
- If there is no continuity, continue with next step
- If there is continuity, go to step 7
- On the TQA, check for continuity of the LH FUEL CUTOFF switch (1S1) between connector A41J2 pins 38 and 46.
- If there is continuity, continue with next step
- If there is no continuity, replace the TQA
- Check for continuity between connector A41P2 pin 38 and airframe ground.
- If there is no continuity, check the ground stud or repair defective wiring as required
- If there is continuity, continue with next step
- Perform wiring checks between the FMQGC and the left Engine Fuel Cutoff switch and repair as required
- Remove the FMQGC and rerack the unit fully and perform a test of the system. Is the fault still present?
- If YES, continue with next step.
- If NO, do close out.
- Access the ACPC logic assembly. Swap SSPC 6 (L FWD PRI PUMP) with SSPC 4 (spare card). Is the fault still present?
- If YES, continue with next step.
- If NO, replace defective SSPC card.
- Swap SSPC 1 (L AFT PRI PUMP) with SSPC 4 (spare card). Is the fault still present?
- If YES, continue with next step.
- If NO, replace defective SSPC card.
- Contact the Bombardier Customer Response Center for further troubleshooting.
- Do close out.