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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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09/19/24

Message Overview:

R BLEED FAULT
(Advisory)

DDG Reference: None
Pilot Action (QRH): ENVR 06-20
System Description: 36-12-00 - Bleed-Air Leak-Detection System
Schematic Diagram: [ G5000 ]  [ Global Express ]  [ Global XRS ] SSM 36-12-00-101 - Bleed Air Leak Detection System - Electrical Schematic
Wiring Diagram: [ G5000 ]  [ Global Express ]  [ Global XRS ] WM 36-12-00-1_002 - Sheet 2 - Right Wing Leading Edge - [9004-9024]
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 36-12-00-1_003 - Sheet 3 - Center/AFT Fuselage - [9004-9024]
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 36-12-00-2_002 - Sheet 2 - Right Wing Leading Edge - [9003, 9025-9158]
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 36-12-00-2_003 - Sheet 3 - Center/AFT Fuselage - [9003, 9025-9158]
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 36-12-00-3_002 - Sheet 2 - Right Wing Leading Edge - [9002]
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 36-12-00-3_003 - Sheet 3 - Center/Aft Fuselage - [9002]
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 36-12-02-1_001 - Sheet 1 - Wing Leading Edge (Right) - ALL
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 36-12-03-1_001 - Sheet 1 - Centre/Aft Fuselage - ALL

Message Description:

There is a failure in the Right Bleed System.

Possible Causes:

  • Right Bleed Leak Detection Loops
  • Air Conditioning System Controller 2 (ACSC) (A88)
  • Data Acquisition Units 3 (DAU) (A30)
  • Data Acquisition Units 4 (DAU) (A31)
  • Right Pressure Regulating Valve (PRV)
  • Right High Pressure Valve (HPV)
  • Right Bleed Pressure Transducer (BPT) (MT112)
  • Right Intermediate Pressure Transducer (IPT)
  • Bleed Management Controller 1 (BMC) (A69)
  • Bleed Management Controller 2 (BMC) (A70)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

  • AW700-36-0365 - Bleed management controller - Data Gathering to reduce No Fault Found (NFF) rate
  • AW700-36-0826 - Kidde Bleed Leak Detection Loops Notice of Escape
  • SB 700-31-020 - Flight Data Recording (FDR) System – Installation Of The Force Transducer Units (FTU) And Activation Of The Crew Force Measuring System (CFMS) 2002 

Full Throttle Blog/Forum Articles/Infoservice/Newsletter:

Flight Operation Notifications Manual (FONM):

  • G5000 ]  [ Global Express ]  [ Global XRS ] FON 01-10 ENVR-001 [L BLEED FAULT] (Advisory/Cyan) or [R BLEED FAULT] (Advisory/Cyan) On Ground

NOTES:

  • R BLEED FAULT may be posted if the aircraft is operated outside the AFM 02-08-1 and FCOM1 07-06 Hot Weather Operation limitations.
  • Auxiliary Power Unit (APU) should not be used for Bleed Extraction to operate air conditioning above 45 C OAT.
  • 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):
    -BMC NVM download
    -IAC CAS messages download

Quick Links:

Grounding of the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM10-11-00-867-801
Removal of the Covers and Plugs [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM10-12-00-020-801
Installation of the Covers and Plugs [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM10-12-00-420-801
Standard Aircraft Configuration for Maintenance [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM12-00-00-867-801
Aircraft Walkaround (for Maintenance) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM12-00-00-867-802
Connect Electrical Power to the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-861-801
Remove the Electrical Power from the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-861-802
Electrical/Electronic Safety Precautions [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-910-801
Electrostatic Discharge Safety Precautions [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-910-802
Leak Test of the Bleed Air System [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-00-790-801
Removal of the High-Pressure-Bleed Shutoff Valve [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-01-000-801
Installation of the High-Pressure-Bleed Shutoff Valve [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-01-400-801
Operational Test of the High-Pressure-Bleed Shutoff Valve [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-01-710-801
Removal of the Bleed-Pressure Regulating-and-Shutoff Valve [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-09-000-801
Installation of the Bleed-Pressure Regulating-and-Shutoff Valve [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-09-400-801
Operational Test of the Bleed-Pressure Regulating-and-Shutoff Valve [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-09-710-801
Removal of the Bleed Pressure Transducer [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-25-000-801
Installation of the Bleed Pressure Transducer [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-25-400-801
Operational Test of the Bleed Pressure Transducer [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-25-710-801
Removal of the Cross-Bleed Valve [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-29-000-801
Installation of the Cross-Bleed Valve [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-29-400-801
Operational Test of the Cross-Bleed Valve [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-29-710-801
CAIMS PMAT General Instructions [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-801
Access to Active Faults [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-802
Access to Stored Faults [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-803
Access to System Diagnostics [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-804
Flight Deck Effect to Fault Correlations [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-821

Troubleshooting Recommendations:

  1. Inspect the Bleed synoptic page.

    1. If the R PRSOV is not in the commanded position or shows amber continue with next step.
    2. If R PRSOV position and status is good, go to step 3.

  2. Inspect the R PRSOV installation. Refer to AMM TASK 36-11-09-400-801.
    NOTE: To prevent distortion of the valve body during installation follow the instructions regarding the orientation of the couplings in AMM task "36-11-09-400-801 - Installation of the Bleed-Pressure Regulating-and-Shutoff Valve".
  3. Select displayed message from the menu below:
  4. Do close out.
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