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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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07/24/19

Message Overview:

R WING A/ICE FAIL
(Caution)

DDG Reference: 30-11-03
30-11-03
30-11-04
36-12-01
Pilot Action (QRH): ABNORM 11-4
System Description: 30-12-00
Schematic Diagram: 30-11-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 30-11-03 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

R wing anti-ice system has failed.

Possible Causes:

  • Anti-ice Leak Detection Elements
  • Wing Cross Bleed Valve
  • PRV
  • Bleed Management Controller (BMC)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

  1. Failure of two leak detection elements of the wing anti-ice system.
  2. Low temperature is detected in the wing anti-ice system.
  3. Wing cross bleed valve failed in the not full open position with the right PRV in the closed position.
  4. Wing cross bleed valve failed in the not full open position with the right engine off.
  5. Wing cross bleed valve failed in the not full open position with the failure of the right wing anti-ice valve.

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.
NOTE:  To avoid the display of any Bleed related CAS nuisance message after replacement of BMC due to internal failure, follow AW700-36-0365 instructions.

  • Proceed to a QAR (if available) download of the last three flights (Aircraft meeting FAR part 135.172.), SB 700-31-020
  • BMC NVM download
  • IAC CAS messages download

Quick Links:

Removal of Anti-Icing Temperature Sensors AMM 30-11-05-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of Anti-Icing Temperature Sensors AMM 30-11-05-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
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 Cross Bleed Valve AMM 36-11-29-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of Cross Bleed Valve AMM 36-11-29-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of Wing Anti-Icing Piccolo Ducts AMM 30-12-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of Wing Anti-Icing Piccolo Ducts AMM 30-12-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of Anti-Icing Modulating-and-Shutoff Valves AMM 30-11-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of Anti-Icing Modulating-and-Shutoff Valves AMM 30-11-01-400-801 [ 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 ]
Wire Repair SPM 20-12-10 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Using the PMAT, access the Active Faults/Stored Faults as per AMM Tasks.
  2. Select related CAIMS message below:

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