09/07/19
Message Overview:
Fault Message:
[BMC1] RIGHT WING ANTI-ICING LEAK
Fault Code:
3615514BMC
Associated CAS:
| Reporting LRU: | Bleed Management Controller (BMC) 1 |
| System Description: | 36-12-00 |
| Schematic Diagram: | 36-12-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 36-12-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Message Description:
A leak has been detected by Bleed Management Controller (BMC) 1 Right WING Loops AND has been simultaneously detected by either Right Wing Inboard or Outboard Loops from BMC 2. Inhibited during Take-Off and Landing.
Possible Causes:
- Right Wing Bleed Air
- Bleed Air Leak Detection System
Troubleshooting Tips:
Advisory Wire/Service Bulletin:
- AW700-36-0826 - Kidde Bleed Leak Detection Loops Notice of Escape
Forum Articles/Infoservice/Newsletter: None
NOTE:
- Refer to AIPC 36-12-03 for Right Wing Leak Detection Loops.
Quick Links:
| Leak Test of the Bleed Air System | AMM 36-11-00-790-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Bleed Leak-Detection-Loops and Components Maintenance Practices | AMM 36-12-00-910-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wing Bleed Leak Detection Loop | AIPC 36-12-03 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- To determine the affected area in the right wing, identify which of the following CAIMS faults is reported by BMC 2.
- Make sure the Leak Detection Elements are installed as per Bleed Air Leak Detection System-Maintenance Practices.
- If system checks are good, do close out.
- If fault remains, continue with next step.
- Perform affected area of RIGHT WING DUCT leak check.
- Do close out.