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Require immediate crew attention. These messages are accompanied by flashing master warning, triple chime attenson with or without voice message or dedicated tone. Require immediate crew awareness and future crew action may be required in the form of alternate system selection or performance limitation. These message are accompanied by flashing master caution and a single chime. Indicate safe or normal system operation which require crew awareness, over and above the dark cockpit philosophy. Indicate minor failures or reduction in systems capability, which require no crew action.

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12/07/23

Message Overview:

Message Name:

TS2R - SENSOR FUEL TEMP/WRG

Message Code:

284466EPK

Reporting LRU: Fuel Management and Quantity Gauging Computer (FMQGC)
Associated CAS: FUEL TEMP SENSOR (Caution)
System Description: 28-41-00 - Fuel Management and Quantity Gauging System
Schematic Diagram: [ G5000 ]  [ Global Express ]  [ Global XRS ] SSM 28-41-00-101 - Fuel Management and Quantity Gauging System (FMQGS)
Wiring Diagram: [ G5000 ]  [ Global Express ]  [ Global XRS ] WM 28-41-00-1_002 - Sheet 2 - Fuel Monitoring - [9002-9084 PRE SB 700-28-029]
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 28-41-02-1_001 - Sheet 1 - Fuel Monitoring - ALL

Message Description:

TS2R SENSOR, FUEL TEMP/WRG FAULT shows when:

  • The TS2R Temperature Sensor or interface is out of range
  • There is an open circuit or
  • There is a short circuit

Possible Causes:

  • Right Wing Fuel Tank Temperature Sensor (E37)
  • Fuel Management and Quantity Gauging Computer (FMQGC) (A47)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Flight Operation Notifications Manual (FONM): None

Quick Links:

Suction Defueling [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM12-11-05-650-801
Connect Electrical Power to the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-861-801
Remove the Electrical Power from the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-861-802
Opening of Non-Thermal Circuit Breakers [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-863-801
Closing of Non-Thermal Circuit Breakers [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-863-802
Electrical/Electronic Safety Precautions [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-910-801
Fuel-System Safety Precautions [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM28-00-00-910-801
Removal of the Wing-Tank Access Panels
(183AZ/183BZ, 520AB/620AB, 520BB/620BB, 520CB/620CB,
520DB/620DB, 520EB/620EB, 530AB/630AB, 530BB/630BB,
530CB/630CB, 530DB/630DB, 530EB/630EB, 540AB/640AB,
540BB/640BB, 540CB/640CB, 540DB/640DB, 540EB/640EB,
540FB/640FB, 540GB/640GB, 540HB/640HB, 540JB/640JB)
[ G5000 ]  [ Global Express ]  [ Global XRS ] AMM28-11-01-000-801
Installation of the Wing-Tank Access Panels [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM28-11-01-400-801
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
Removal of the Temperature Sensors [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM28-41-25-000-801
Installation of the Temperature Sensors [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM28-41-25-400-801
Operational Test of the Temperature Sensors [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM28-41-25-710-801
Access to System Diagnostics [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-804
Safety Precautions - Maintenance Practices - ALL [ G5000 ]  [ Global Express ]  [ Global XRS ] SPM20-00-01-02
Wire Repair - Maintenance Practices - ALL [ G5000 ]  [ Global Express ]  [ Global XRS ] SPM20-12-10-02

Troubleshooting Recommendations:

  1. Remove the FMQGC and inspect all connectors and pins on the unit and A/C side. Rerack the FMQGC and make sure it is fully and properly pushed into place. Is the fault still present?

    1. If NO, do close out.
    2. If YES, continue with next step.

  2. Remove the FMQGC and perform a resistance check as follows and compare results to the resistance chart below:

    From To Result Expected Result
    A47DP1-D4 A47DP1-E4 See resistance chart
    A47DP1-D4 Ground Open
    A47DP1-E4 A47DP1-F4 Continuity
    A47DP1-E4 Ground Open

    1. If the resistance values are within tolerance, replace the FMQGC and do close out.
    2. If the resistance values are not within tolerance, continue with next step.
      TIPS: Better results are obtained if aircraft has been allowed to reach ambient temperature inside a hangar. Resistance results can be compared with the other fuel temperature sensors, they should be very close with each other.

  3. Perform a wiring check between the right Temperature Sensor TS2R and the FMQGC. Look for continuity, short circuit and high resistance.

    1. If wiring checks are not good, repair defective wiring as required and do close out.
    2. If wiring checks are good, continue with next step.
      TIP: It is recommended to start with the wiring checks that can be performed outside the fuel tank first. If a wiring defect is found outside the fuel tank, it will prevent you from having to prepare the fuel tank for access.

  4. Perform a visual inspection of the Temperature Sensor. Make sure it is exempt of damage, corrosion or contamination. Pay attention to the electrical connections.

    1. If defects are found, rectify as required and do close out.
    2. If checks are good, continue with next step.

  5. Interchange Temperature Sensor 2 with Temperature Sensor 1. Is the fault message still present?

    1. If NO, replace the defective Temperature Sensor and do close out.
    2. If YES, replace the FMQGC and continue with next step.

  6. Do close out.
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