background
x
loader
Troubleshooting
arrow By ATA By Message Color By Observed Faults By CAIMS By Tips

Select color for CAS message that you wish to troubleshoot

(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.

This page includes :

For AOG assistance contact:

CRC Montreal (YUL)
Quick Links

08/16/19

Message Overview:

BLEED MISCONFIG
(Advisory)

DDG Reference: None
Pilot Action (QRH): ADVISORY 2-3
System Description: 36-11-00
Schematic Diagram: 36-11-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 36-11-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

Engine start configuration does not operate.

Possible Causes:

  • Left Regulating Valve (PRV) failed in the open position
  • Right Regulating Valve (PRV) failed in the open position
  • Left Wing-Anti Ice Valve (WAIV) failed in the open position
  • Right Wing-Anti Ice Valve (WAIV) failed in the open position
  • Cross Bleed Valve
  • Left Bleed Leak Detection Loops
  • Right Bleed Leak Detection Loops
  • Bleed Management Controller
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

Forum Articles/Infoservice/Newsletter:

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:

Bleed Air Leak Detection System - Maintenance Practices AMM 36-12-00-910-801 [ 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 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 ]
Removal of Bleed Pressure Regulating and Shutoff Valve AMM 36-11-09-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of Bleed Pressure Regulating and Shutoff Valve AMM 36-11-09-400-801 [ 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:
     

Registered and/or unregistered trademarks of Bombardier Inc. or its subsidiaries. © 2015 Bombardier Inc. All rights reserved.