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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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09/27/19

Message Overview:

Fault Message:

R VSVA CH B WRG/VSVA[LVDT] RNG

Fault Code:

7326017RBR

Associated CAS:

R FADEC FAIL
(Caution)

Reporting LRU: Right Engine Electronic Controller (EEC)
System Description: 75-30-00
Schematic Diagram: 75-31-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 71-50-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]
75-31-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

There is an error of resistance or an open or short circuit in the Linear Variable Differential Transformer (LVDT) of the Variable Stator Vane Actuator (VSVA) for the Engine Electronic Controller (EEC) 2 channel B. Inhibited during Take-off and Landing.

Possible Causes:

  • Right Variable Stator Vane Actuator (VSVA)
  • Right Engine Electronic Controller (EEC)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

NOTE: The VSVA circuits are continuously monitored during engine operation and during power-up of the FADEC.

Quick Links:

Opening of the Cowls AMM 71-10-00-010-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Closing of the Cowls AMM 71-10-00-410-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Bypass-Duct Access Panels (451AL/461AL,
451BL/461BL, 451CL/461CL, 451DL/461DL,
451EL/461EL, 452FR/462FR, 452GR/462GR,
452HR/462HR, 452JR/462JR, 452KR/462KR)
AMM 72-71-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Bypass-Duct Access Panels (451AL/461AL,
451BL/461BL, 451CL/461CL, 451DL/461DL,
451EL/461EL, 452FR/462FR, 452GR/462GR,
452HR/462HR, 452JR/462JR, 452KR/462KR)
AMM 72-71-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Deactivation of the Thrust Reverser (for Maintenance) AMM 78-30-00-040-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Activation of the Thrust Reverser (for Maintenance) AMM 78-30-00-440-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Compressor Fairings EMM 72-03-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Compressor Fairings EMM 72-03-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Engine Electronic Controller (EEC) EMM 73-21-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Engine Electronic Controller (EEC) EMM 73-21-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Variable Stator-Vane Actuator EMM 75-31-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Variable Stator-Vane Actuator EMM 75-31-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

CAUTION: DO NOT DO ELECTRICAL CHECKS INTO THE ENGINE ELECTRONIC CONTROLLER (EEC). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE EEC CAN OCCUR.

  1. Perform a deactivation of the Thrust Reverser (TR) and open the cowls.
  2. Remove the applicable bypass-duct access panel and remove the applicable compressor fairing.
  3. Perform wiring check between EEC 2 (P1047), the bypass duct (J1032) and the VSVA (P1010).

    1. If wiring checks are not good, repair defective wiring as required and go to step 6.
    2. If wiring checks are good, continue with next step.

  4. Replace the VSVA.

    1. If system checks are good, go to step 6.
    2. If fault remains, continue with next step.

  5. Replace EEC 2.
  6. Install the applicable bypass-duct access panel and the applicable compressor fairing.
  7. Close the cowls and activate the thrush reverser.
  8. Do close out.
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