01/28/21
Message Overview:
| DDG Reference: | 36-20 |
| Pilot Action (QRH): | ENVR 06-7 |
| System Description: | 36-20-00 30-12-00 |
| Schematic Diagram: | 36-21-00 L BLEED SCHEMATIC |
| Wiring Diagram: | 36-21-11 |
Message Description:
The 'L BLEED LOOP FAIL' (Caution) CAS message indicates that the left bleed leak detection loops in the pack inlet ducting have failed during the power-up self-test.
- The IASC system has detected problems with the left bleed air leak loops in the pack inlet. Through ARINC bus to the DCU the EICAS has displayed the 'L BLEED LOOP FAIL' caution message.
Possible Causes:
- Plumbing Leak
- Bleed Loop Routing
- LH Bleed Loop (MT67)
Troubleshooting Tips:
Advisory Wire/Service Bulletin:
- AW300-36-0310 - Bleed Loop Connector Cleaning Tool
- AW300-30-0354 - Potential Piccolo Tube Damage When Replacing a Bleed Loop Element
Forum Articles/Infoservice/Newsletter: None
Troubleshooting Guide for Bleed Loops
Abbreviation Guide:
| ACS | Air Conditioning System |
| AIPS | Airframe Ice Protection System |
| APU | Auxiliary Power Unit |
| ATS | Air Turbine Starter |
| CBIT | Continuous Built-In-Test |
| CBW | Wing Cross-Bleed Valve |
| CBV | Cross-Bleed Valve |
| CH | Channel |
| DCU | Data Concentrator Unit |
| Element | Hot Air Leak Detection Sensor with a connector on each end |
| F.S. | Fuselage Station |
| FCV | Flow Control Valve |
| HARSOV | Hot Air Regulating and Shut-off Valve |
| HPGC | High Pressure Ground Connection |
| HPV | High Pressure Valve |
| IASC | Integrated Air System Controller |
| IBIT | Initiated Built-In-Test |
| IPV | Intermediate Pressure Valve |
| Loop | Assembly of several elements connected together in series to detect Hot air leaks in a given system |
| MDC | Maintenance Diagnostic Computer |
| PBIT | Power Up Built-In-Test |
| PCV | Pre-cooler Crossover Valve |
| TCV | Temperature Control Valve |
| WAIV | Wing Anti-ice Valve |
| W.S. | Wing Station |
- The ducting has a insulation cover that will contain the air leaking from the ducting routing it to a insulation vent hole.
- The loop elements are electrically connected in series and the concentric outer conductor is connected to the aircraft ground. The layer of eutectic salt compound insulates the outer conductor from the inner conductor. When hot bleed-air gets on the loop element, the eutectic salt compound becomes conductive and lets the outer conductor make contact with the inner conductor. The IASC controller senses that the outer conductor is grounded and supplies the inner conductor with alternating current for its resistance measurement. The IASC controller measures this resistance and shows the correct message on the EICAS.
- The intermediate pressure system loop element senses a bleed-air leak when the temperature is more than 255°F (123.90°C).
Quick Links:
| Component Location | AMM 36-21-00-992-801 |
| Operational Test of the Bleed-Air Leak-Detection and Warning System | AMM 36-21-00-710-801 |
| Initiation Test of the Bleed-Air Leak-Detection Loops | AMM 36-21-00-740-801 |
| Resistance Check of the Bleed-Air Leak-Detection Loops | AMM 36-21-00-760-801 |
| Removal of the Left Bleed Loop Element | AMM 36-21-01-000-801 |
| Installation of the Left Bleed Loop Element | AMM 36-21-01-400-801 |
| Wiring - Maintenance Practices - ALL | SPM 20-12-00-02 |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 |
| Electrical Connectors - Maintenance Practice - ALL | SPM 20-20-00-02 |
Troubleshooting Recommendations:
- If no fault is shown or the system is intermittent, do the following steps:
- Go into the system diagnostics to the IASC #1 channel B (Left Bleed Loop) to display the IASC Channel B menu. The IASC LRU test page will provide pages to perform a leak detection system test and check past event locations. The test will check all of the loops the IASC is monitoring and pass or fail them. This test may fail if there is a lot of action going on in the IASC, retesting may pass the failed loops. This test is disabled with the wing heat system on. Perform the test of the bleed air leak detection loops IAW AMM 36-21-00-710-801.
- Perform Initiation Test of the Bleed-Air Leak-Detection Loops.This test will identify if the respective loop has a short or open. Per AMM 36-21-00-740-801
- If a loop fails, or a fault has been logged into the MDC, use the steps below to further isolate the condition.
- Interrogate the MDC as follows:
- On the cursor control panel, ensure the toggle switch is to the right and select Anti-Ice, ECS and Fuel buttons simultaneously. The MDC main menu should now be displayed on Display Unit #3.
- Using the joystick, select Current Faults (if the fault is active) or Aircraft History to research stored faults. From Aircraft History you can then select Fault Message History and locate the fault. Going into advanced diagnostics will provide an equation id for the fault identified.
- Select the MDC fault or equation from the drop down below to provide additional information to assist in troubleshooting.
- Determine which loop is posting the B3, then use a Tegam meter to check capacitance and inductance between the inner and outer conductor of the corresponding loop. Perform the impedance check per the Leak detection how to.
- LH Bleed loop schematic and information (MT67).
NOTE: Before replacing a loop always look at the loop for routing, ensure loop is not too close to the plumbing or the bleed hole on a valve. Review AMM 36-21-00-992-801 for component location. See individual loops for specific routing information. - The test will identify if the respective LH loop has a short or open (greater than 75Ω). MT67 (LH system loop). Perform resistance checks on the applicable loop per AMM 36-21-00-760-801.
- If the L Leak Detection loop does not meet resistance checks then replace LDE.
LOOP VALUE (OHMS) LH and RH Bleed 75Ω