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(WARNING)
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(CAUTION)
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(ADVISORY)
CYAN MESSAGE
(STATUS)
WHITE MESSAGE
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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01/28/21

Message Overview:

L BLEED LOOP FAIL
(Caution)

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:

  1. If no fault is shown or the system is intermittent, do the following steps:

    1. 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.
    2. 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
    3. If a loop fails, or a fault has been logged into the MDC, use the steps below to further isolate the condition.
    4. Interrogate the MDC as follows:

      1. 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.
      2. 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.
      3. Select the MDC fault or equation from the drop down below to provide additional information to assist in troubleshooting.
      4. 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.
      5. 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.
      6. 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.
      7. If the L Leak Detection loop does not meet resistance checks then replace LDE.
      8. LOOP VALUE (OHMS)
        LH and RH Bleed 75Ω

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