background
x
loader
Troubleshooting
arrow By ATA By Message Color By Observed Faults by MDCBy Tips

Select color for CAS message that you wish to troubleshoot

(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.

This page includes :

For AOG assistance contact:

CRC Montreal (YUL)
Quick Links

01/28/21

Message Overview:

WING A/ICE LOOP FAIL
(Advisory)

DDG Reference: 36-20
Pilot Action (QRH): ICE 12-12
System Description: 30-12-00
Schematic Diagram: 30-12-00
L WING A/ICE LOOP SCHEMATIC
R WING A/ICE LOOP SCHEMATIC
Wiring Diagram: 30-12-05

Message Description:

The cyan 'WING A/ICE LOOP FAIL' advisory CAS message is posted by either IASC #1B or IASC #2B when both loops of the wing anti-ice ducting are detected failed, (shorted or open). The two wing anti-ice lead detection loops have failed.

10_iasc2_chb_menu_page

Possible Causes:

  • Both loops of the Wing Anti-Ice Ducting are detected failed

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

NOTE: If the bleed loop resistance value is within limits, try cleaning the bleed loop connections per AMM 51-25-00-110-801 and then reapply lubrication to the connections per AMM WM 20-20-00. Lubrication part number is called out in each bleed loop installation procedure. Run the aircraft after the cleaning and applying lubing procedure and see if the BLEED LOOP FAULT clears.

Quick Links:

Component Location AMM 36-21-00-992-801
Operational Test of the Wing Anti-ice system AMM 30-10-00-710-801
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 Wing−Root Leak−Detection Element AMM 36-21-17-000-801
Installation of the Wing−Root Leak−Detection Element AMM 36-21-17-400-801
Removal of the Wing−Middle Leak−Detection Element AMM 36-21-17-000-802
Installation of the Wing−Middle Leak−Detection Element AMM 36-21-17-400-802
Removal of the Wing−Outboard Leak−Detection Element AMM 36-21-17-000-803
Installation of the Wing−Outboard Leak−Detection Element AMM 36-21-17-400-803
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. 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.

45_current_faults45_advance_diagnostics

Registered and/or unregistered trademarks of Bombardier Inc. or its subsidiaries. © 2015 Bombardier Inc. All rights reserved.