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(WARNING)
RED MESSAGE
(CAUTION)
AMBER MESSAGE
(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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01/27/21

Message Overview:

L WING ANTI-ICE FAIL
(Caution)

DDG Reference: 30-10
30-11
Pilot Action (QRH): ICE 12-8
System Description: 30-12-00
Schematic Diagram: 30-12-00
Wiring Diagram: 30-11-01

Message Description:

The amber 'L WING A/I LOW TEMP' caution CAS messages will appear when a low temperature condition is sensed at the wing and no other fail messages from the air system are present. If other failures from the air system are present, the L WING ANTI-ICE FAIL message will overwrite the L WING A/I LOW TEMP message.

Possible Causes:

  • Integrated Air System Controller (IASC1)
  • Data Concentrator Unit (DCU) (A14)
  • Wing Leading Edge Temperature Sensors
  • Left Anti-Ice Valves
  • Cross-flow Anti-Ice Valves

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Removal of the Integrated Air System (IAS) Controller AMM 21-31-01-000-801
Installation of the Integrated Air System (IAS) Controller AMM 21-31-01-400-801
Operational Test of the Integrated Air System (IAS) Controller AMM 21-31-01-710-801
Operational Test of the Leading-Edge Temperature Sensors AMM 30-11-00-710-801
Removal of the Inboard Leading-Edge Temperature Sensor AMM 30-11-01-000-801
Installation of the Inboard Leading-Edge Temperature Sensor AMM 30-11-01-400-801
Removal of the Outboard Leading-Edge Temperature Sensor AMM 30-11-03-000-801
Installation of the Outboard Leading-Edge Temperature Sensor AMM 30-11-03-400-801
Removal of the Wing Cross-Bleed Valve AMM 30-11-05-000-801
Installation of the Wing Cross-Bleed Valve AMM 30-11-05-400-801
Deactivation of the Wing Cross-Bleed Valve AMM 30-11-05-040-801
Activation of the Wing Cross-Bleed Valve AMM 30-11-05-440-801
Removal of the Wing Cross-Bleed Valve Sense Line AMM 30-11-07-000-801
Installation of the Wing Cross-Bleed Valve Sense Line AMM 30-11-07-400-801
Removal of the Anti-Ice Control Panel AMM 30-11-09-000-801
Installation of the Anti-Ice Control Panel AMM 30-11-09-400-801
Removal of the Wing Anti-Ice Valve AMM 30-12-01-000-801
Installation of the Wing Anti-Ice Valve AMM 30-12-01-400-801
Removal of the Data Concentrator Unit (DCU) AMM 31-41-01-000-802
Installation of the Data Concentrator Unit (DCU) AMM 31-41-01-400-802
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. Perform AMM to verify the proper operation of the wing leading edge temperature sensors.

    1. If any of the sensors fail the above check, replace the sensor.

  2. Entering the system diagnostics LRU tests for IASC 1B and 2B will allow viewing of the wing temperature sensors.

    1. Selecting the wing anti-ice sensor status will bring up the individual temperature sensors.
    2. With wing heat on, the system will try and regulate the inner sensors to 54°C. The AMM has this checked at idle and power settings assuring that the left, right, and cross-flow ANTI-ICE valves operate correctly.
    3. Displayed will be the following parameters on the sub system page:

      1. Left Inboard Leading Edge Temperature °C
      2. Left Outboard Leading Edge Temperature °C
      3. Right Inboard Leading Edge Temperature °C
      4. Right Outboard Leading Edge Temperature °C

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