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(WARNING)
RED MESSAGE (CAUTION)
AMBER MESSAGE (ADVISORY)
CYAN MESSAGE (STATUS)
WHITE MESSAGE 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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For AOG assistance contact:

CRC Montreal (YUL)
Quick Links

09/24/19

Message Overview:

Fault Message:

R EEC [P0 XDCR]

Fault Code:

7325523RBR

Associated CAS:

R FADEC FAIL
(Caution)

R FADEC FAULT
(Advisory)

Reporting LRU: Right Engine Electronic Controller (EEC)
System Description: 73-20-00
Schematic Diagram: None
Wiring Diagram: 71-50-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

Engine Electronic Engine Control (EEC) 2 has an internal failure due to the Pressure Module. The P0 (Pressure Altitude) value of the EEC 1 is out of range or fails the crosscheck with the Air Data Computer (ADC) data. Inhibited during engine start and Reverse Thrust.

Possible Causes:

  • Right Engine Electronic Controller (EEC)

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

NOTE: A staggered EEC power up can lead to a latched Engine P0 failure.

Quick Links:

Removal of the Eng Electronic Controller (EEC)
Mod 73-101559		 EMM 73-21-01-000-801-B00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Eng Electronic Controller (EEC)
Mod 73-101559		 EMM 73-21-01-400-801-B00 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Perform a overall inspection for EEC 2.

    1. If the fault is no longer active or no further maintenance action is required, do close out.
    2. If the fault is active, continue with next step.

  2. Cycle the power to EEC Channel A/B. Is the fault still present?

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

  3. Replace EEC 2.
  4. Do close out.

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