09/19/24
Message Overview:
| DDG Reference: | None |
| Pilot Action (QRH): | ENVR 06-6 |
| 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 36-12-00-2_003 - Sheet 3 - Center/AFT Fuselage - [9003, 9025-9158] [ G5000 ] [ Global Express ] [ Global XRS ] WM 36-12-00-3_003 - Sheet 3 - Center/Aft Fuselage - [9002] [ G5000 ] [ Global Express ] [ Global XRS ] WM 36-12-03-1_001 - Sheet 1 - Centre/Aft Fuselage - ALL |
Message Description:
A leak is sensed on the Left Bleed Air System. The system is installed on the left side of the Aft Equipment Compartment and Pylon.
Possible Causes:
- Uroseals
- A Bleed Air Leak is sensed on the Left Bleed Air System
- A loose or incorrect installation of the Sensing Elements of the Left Bleed Leak Detection System
- Left Bleed Management Controller (L BMC) (A69)
Troubleshooting Tips:
Advisory Wire/Service Bulletin:
- AW700-36-0826 - Kidde Bleed Leak Detection Loops Notice of Escape
Full Throttle Blog/Forum Articles/Infoservice/Newsletter:
- Tech Corner Article - Hot weather effects on the bleed air detection system
Flight Operation Notifications Manual (FONM): None
NOTES:
- L BLEED LEAK 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 the Aft Equipment Bay Bleed Leak Troubleshooting Aid Reference Document for help in identifying leaks, component identification and tooling instructions.
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 |
| 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 |
| 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:
- Using the PMAT, access the Active Faults/Stored Faults as per AMM Tasks.
- Select related CAIMS message below:
- Do the close out.