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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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04/24/25

Message Overview:

Message Name:

[BMC1] RIGHT BLEED LEAK D LOOP /WRG

Message Code:

3615523BMC

Reporting LRU: Bleed Management Controller 1 (BMC)
Associated CAS: R BLEED SYS FAIL (Caution)
R BLEED FAULT (Advisory)
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_003 - Sheet 3 - Center/AFT Fuselage - [9004-9024]
[ G5000 ]  [ Global Express ]  [ Global XRS ] WM 36-12-03-1_001 - Sheet 1 - Centre/Aft Fuselage - ALL

Message Description:

The Right Bleed Loops circuit connected to Bleed Management Controller 1 (BMC) has been detected with an Open Center Conductor or short circuit between the Center Conductor and the Outer Sheath. Inhibited during Take-Off and Landing.

Possible Causes:

  • Uroseals
  • Right Bleed Duct Loop 1A (MT104)
  • Right Bleed Duct Loop 1B (MT199)
  • Right Bleed Duct Loop 1C (MT200)
  • Right Bleed Duct Loop 1D (MT201)
  • Right Bleed Duct Loop 1E (MT202)
  • Bleed Management Controller 1 (BMC) (A69)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

  • AW700-36-0826 - Kidde Bleed Leak Detection Loops Notice of Escape

Full Throttle Blog/Forum Articles/Infoservice/Newsletter:

Flight Operation Notifications Manual (FONM): None

NOTES:

  • [BMC1] RIGHT BLEED LEAK D LOOP /WRG 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.
  • Refer to AIPC 36-12-02 for Right Bleed Leak Detection Loops.
  • The sensing element is used to find a temperature that is too hot. When the eutectic salt is heated to its alarm temperature, it forms a conductive path between the center wire conductor and the outer sheath of the sensing element. This path transmits a signal that gives an alarm signal to the detection circuit.
  • Let the temperature of the sensing element become stable at ambient room temperature. Write the temperature.
  • To prevent damage to the sensing element connector, install test pins in the connectors when you do the continuity and insulation resistance tests.

CAUTION:

  • WHEN PERFORMING THE CONDUCTANCE TEST OF THE LEAK DETECTION LOOPS, DO NOT USE A METER THAT APPLIES DC VOLTAGE. DO NOT USE INSULATION RESISTANCE “MEGGER” TESTERS OR DIELECTRIC VOLTAGE “HYPOT” TESTERS. THESE WILL DAMAGE THE SENSING ELEMENT.
  • DO NOT DO TESTS OF A SENSING ELEMENT THAT IS HEATED TO WITHIN 100°F (55°C) OF ITS ALARM TEMPERATURE.

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 Bleed Management Controller [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-33-000-801
Installation of the Bleed Management Controller [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-33-400-801
Operational Test of the Bleed Management Controller [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-33-710-801
Removal of the UROSEAL Joints [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-61-000-801
Installation of the UROSEAL Joints [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-61-400-801
Leak Test of the UROSEAL Joints [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-61-790-801
Rigging of the UROSEALS [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-11-61-820-801
Bleed Leak-Detection-Loops and Components Maintenance Practices [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-12-00-910-801
Operational Test of the Bleed Leak-Detection-Loops [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM36-12-01-710-801
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
Wire Repair - Maintenance Practices - ALL [ G5000 ]  [ Global Express ]  [ Global XRS ] SPM20-12-10-02

Troubleshooting Recommendations:

NOTE: If the 3615523BMC CAIMS message is present at the same time as 3616523BMC CAIMS message, there is most likely an actual air leak since both distinct circuits (BMC 1 and BMC 2) detect it. Look for loop installation and air leaks.

  1. Disconnect A69P2 from BMC 1.
  2. Measure Insulation resistance and line resistance of the detection loops as per the Leak Detection Elements troubleshooting sheet. Make sure line resistance & insulation values are within the specified limits.

    1. If the values are within specified limits, go to step 4.
    2. If values are not within the specified limits, continue with next step.

  3. Replace faulty elements.

    1. If system checks are good, do close out.
    2. If fault remains, continue with next step.

  4. Make sure the Leak Detection Elements are installed as per Bleed Air Leak Detection System-Maintenance Practices.

    1. If system checks are good, do close out.
    2. If fault remains, continue with next step.

  5. Perform wiring checks of the remaining wires linking the right BLEED Loops circuit to BMC 1.

    1. If wiring checks are not good, repair defective wiring as required and do close out.
    2. If wiring checks are good, continue with next step.
      NOTE: Inspect both ends of each loop to make sure the ceramic Inserts/Shield and Insert Assembly are not damaged. If repairs are necessary refer to CMM 26-14-12.

  6. Interchange BMC 1 with BMC 2 to confirm the failure and replace if necessary.
    NOTE: Refer to the Aft Equipment Bay Bleed Leak Troubleshooting Aid Reference Document for help in identifying leaks, component identification and tooling instructions.
  7. Do the AMM task "36-11-61-790-801 - Leak Test of the UROSEAL Joints".
  8. Are results satisfactory?

    1. If YES, go to step 10.
    2. If NO, continue with next step.

  9. Do the AMM task "36-11-61-820-801 - Rigging of the UROSEALS".
  10. Is the OMS Fault cleared?

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

  11. Do the AMM task "36-11-00-790-801 - Leak Test of the Bleed Air System".
  12. Do close out.
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