09/28/23
Message Overview:
| DDG Reference: | 28-41-01 |
| Pilot Action (QRH): | ABNORM 9-8 |
| System Description: | 28-41-00 |
| Schematic Diagram: | [ Global Express ] [ G5000 ] [ Global XRS ] SSM 28-41-00-101 - Fuel Management and Quantity Gauging System (FMQGS) |
| Wiring Diagram: | [ Global Express ] [ G5000 ] [ Global XRS ] 28-41-00-1_007 - Sheet 7 - Feed Tank - [9002-9084 PRE SB 700-28-029] [ Global Express ] [ G5000 ] [ Global XRS ] 28-41-00-2_008 - Sheet 8 - Feed Tank - [9002-9114 POST SB 700-28-029, AND 9115-9129] [ Global Express ] [ G5000 ] [ Global XRS ] 28-41-00-3_008 - Sheet 8 - Feed Tank - [9085-9114 PRE SB 700-28-029] [ Global Express ] [ G5000 ] [ Global XRS ] 28-41-00-4_008 - Sheet 8 - Feed Tank - [9130-9158] [ Global Express ] [ G5000 ] [ Global XRS ] 28-41-07-1_001 - Sheet 1 - Feed Tank - [9127-9189] [ Global Express ] [ G5000 ] [ Global XRS ] 28-41-07-1_001 - Sheet 1 - Feed Tank - [9159 TO 9189] [ Global Express ] [ G5000 ] [ Global XRS ] 28-41-07-2_001 - Sheet 1 - Feed Tank - [9190-9998] [ Global Express ] [ G5000 ] [ Global XRS ] 28-41-07-2_001 - Sheet 1 - Feed Tank - [9190 AND SUBS] |
Message Description:
FUEL LO QTY (Amber) shows when the following condition occur:
- The left or right or both wing fuel tanks have less than approximately 600 lbs (270 kgs).
- The aircraft is not in a take-off or landing configuration.
Use this troubleshooting only when above conditions are not met.
Possible Causes:
- Left Densitometer (A163)
- Left Compensator (CMPL) (C7)
- Secondary-Power Distribution Assembly (SPDA) 2 (A14)
- Secondary-Power Distribution Assembly (SPDA) 3 (A15)
- Fuel Management and Quantity Gauging Computer (FMQGC) (A47)
- Fuel Quantity Probes
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin:
- AW700-28-0496 - Fuel QTY fluctuation
Forum Articles/Infoservice/Newsletter: None
NOTE:
- As viewed in CAIMS, the Probe Status "GOOD PROBE" indicates the probe is communicating with FMQGC and the probe is reporting a capacitance within a nominal range (between full dry and full wet). The OMS may report the Probe Status as "GOOD PROBE", yet a dry capacitance check per the AMM may find a probe out of AMM limits. The only way to verify if a probe is reporting accurately is to do the Dry Capacitance check IAW AMM task 28−41−00−760−801 Capacitance Test of the Fuel Quantity Probes.

Quick Links:
| Standard Aircraft Configuration for Maintenance | [ G5000 ] [ Global Express ] [ Global XRS ] AMM12-00-00-867-801 |
| Aircraft Walkaround (for Maintenance) | [ G5000 ] [ Global Express ] [ Global XRS ] AMM12-00-00-867-802 |
| Connect Electrical Power to the Aircraft | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-861-801 |
| Electrical/Electronic Safety Precautions | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-910-801 |
| Electrostatic Discharge Safety Precautions | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-910-802 |
| Cleaning of the Fuel Management and Quantity Gauging System (FMQGS) Components | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-00-110-801 |
| Operational Test of the Fuel Quantity Probes | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-00-710-801 |
| Capacitance Test of the Fuel Quantity Probes | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-00-760-801 |
| Resistance Check of the Fuel Management and Quantity Gauging System (FMQGS) Wiring | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-00-760-802 |
| Removal of the Computer | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-01-000-801 |
| Installation of the Computer | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-01-400-801 |
| Self-Test of the Computer | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-01-740-801 |
| Removal of the Fuel Quantity Probes with Compensator | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-05-000-801 |
| Installation of the Fuel Quantity Probes with Compensator | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-05-400-801 |
| Removal of the Aft-Tank Fuel-Quantity Probes | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-13-000-801 |
| Installation of the Aft-Tank Fuel-Quantity Probes | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-13-400-801 |
| Removal of the Densitometer | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-21-000-801 |
| Installation of the Densitometer | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-21-400-801 |
| Operational Test of the Densitometer | [ G5000 ] [ Global Express ] [ Global XRS ] AMM28-41-21-710-801 |
| CAIMS PMAT General Instructions | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-801 |
| Access to Active Faults | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-802 |
| Access to Stored Faults | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-803 |
| Access to System Diagnostics | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-804 |
Troubleshooting Recommendations:
- Using the PMAT, access CAIMS Active Faults. Check if any of the two messages listed below are displayed and select from the menu below:
- If none of these messages are displayed in CAIMS, look for messages for the various probes in the different tanks also. If no messages are present, continue with next step.
- Review the content of AW700-28-0496.
- Do a dry capacitance test of the fuel probes and repair as required and record values on the following data entry form.
- Do close out.