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(WARNING)
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(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

08/06/24

Message Overview:

R COWL A/ICE FAULT
(Advisory)

DDG Reference: None
Pilot Action (QRH): ADVISORY 10-2
System Description: 30-21-00
Schematic Diagram: 30-21-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 36-11-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Message Description:

Right Cowl Anti-Ice Valve has fault.

  • The cowl anti-ice valve does not control the bleed air.
  • The cowl anti-ice valve is failed closed with the engine stopped.
  • The cowl anti-ice valve position indication is failed.

Possible Causes:

  • Right Cowl Anti-Icing Valve (CAIV)
  • Bleed Management Controller (BMC) (A69)

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

  • AW700-36-0365 - Bleed Monitoring Controller - Data Gathering to Reduce No Fault Found (NFF) rate

Forum Articles/Infoservice/Newsletter: None

Flight Operation Notifications Manual (FONM):

NOTES:

  • BMC NFF Action:
    -To support the technical investigation, FSRs and Service Centers are requested to perform an NVM download and complete a condition report and (BMC) PN GG546-1017-XX questionnaire when troubleshooting or removing a Bleed Management Controller (BMC) PN GG546-1017-XX.
  • To avoid the display of any Bleed related CAS nuisance message after replacement of BMC due to internal failure, follow AW700-36-0365 instructions.

Quick Links:

Removal of Bleed Management Controller (BMC) AMM 36-11-33-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of Bleed Management Controller (BMC) AMM 36-11-33-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of Cowl Anti-Icing Valve AMM 30-21-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of Cowl Anti-Icing Valve AMM 30-21-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Access to Active Faults AMM 45-45-00-970-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Access to Stored Faults AMM 45-45-00-970-803 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Did the R COWL A/ICE FAULT cyan CAS message appear during or after engine shutdown?

    1. If YES, continue with next step.
    2. If NO, go to step 9.

  2. Ensure the engine has been shut down for at least 1 minute and the Cowl Anti-Ice Valve (CAIV) is selected OFF.
  3. Check the actual position of the CAIV by using the BLEED/AINTI-ICE synoptic page.
  4. Is the CAIV displayed as OPEN on the synoptic page?

    1. If YES, continue with next step.
    2. If NO, go to step 6.

  5. Is the R COWL A/ICE FAULT advisory CAS message still present?

    1. If YES, continue with next step.
    2. If NO, no further action is required. Do close out.

  6. Open the COWL doors and locate the CAIV.
  7. Check the CAIV V-Band clamps position.

    1. If the V-Band clamps are installed 90° offset from each other, continue with next step.
    2. If the V-Band clamps are not installed 90° off-set from each other, re-orientate the V-Band clamps so that they are oriented 90° from each other.

  8. Verify the valve butterfly position by observing the Output Shaft (OPS) position.

    1. If the OPS is retracted and the CAIV is displayed CLOSED on the Bleed Air/Anti-Ice synoptic page, go to step 10.
    2. If the OPS is fully extended, replace the CAIV and do close out.

  9. Check the Pressure Transducer vent hole for installation clamp obstruction. Obstructing the Pressure Transducer vent hole will result in false pressure measurements and the display of CAI error messages.

    1. If the Pressure Transducer vent hole is covered by the installation clamps, rectify as required (see image below) and do close out.
    2. If the Pressure Transducer vent hole is not obstructed, continue with next step.

  10. Using the PMAT, access the Active Faults/Stored Faults as per AMM Tasks.
  11. Select related CAIMS message below:
  12. Do close out.
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