background
x
loader
Troubleshooting
arrow By ATA By Message Color By Observed Faults By CAIMS By 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

12/22/25

Message Overview:

Message Name:

R WAIT SENSOR INSTALLATION

Message Code:

3616418BMC

Associated CAS:

WING A/ICE OVHT
(Warning)

Reporting LRU: Bleed Management Controller (BMC) 2
System Description: 30-12-00 - Wing Anti-ice System
Schematic Diagram: [ Global Express ]  [ G5000 ]  [ Global XRS ] 30-11-00 - Wing Anti-ice System - Electrical Schematic
Wiring Diagram: [ Global Express ]  [ G5000 ]  [ Global XRS ] 30-11-02 - Anti-icing System Distribution (Right)

Message Description:

When a Wing Leading-Edge Over-Temperature condition is detected and the condition is not related to the Wing Anti-Ice Valve (WAIV).

Possible Causes:

  • Bleed Management Controller (BMC) 2 (A70)
  • Data Acquisition Unit (DAU) 4 (A31)
  • Right Inboard Anti-Icing Temperature Sensor (E41)
  • Right Outboard Anti-Icing Temperature Sensor (E40)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Full Throttle Blog/Forum Articles/Infoservice/Newsletter:

  • Forum Article 2011-VOL 8 issue 23 - Bleed Management Controller (BMC) Top 10 No Fault Found (NFF) vs. Reliability Improvement Modification Program (RIMP) implementation
  • Questionnaire for replacing the BMC. Follow instructions using this (Fill out form)

Flight Operation Notifications Manual (FONM): None

Quick Links:

Removal of the Anti-Icing Temperature Sensors AMM 30-11-05-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Anti-Icing Temperature Sensors AMM 30-11-05-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Data Acquisition Units (DAU) AMM 31-42-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Data Acquisition Units (DAU) AMM 31-42-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Bleed Management Controller AMM 36-11-33-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Bleed Management Controller AMM 36-11-33-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Perform wiring checks between Right INBD WAITS, Right OUTBD WAITS, DAU 4 and BMC 2.

    1. If wiring checks are not good, repair defective wiring as required and do close out.
    2. If wiring checks are good, continue with next step.

  2. Measure resistance of the INBD and OUTBD WAITS sensing elements. Resistance values are listed in the chart as follows:

    Temperature (in centigrade) Resistance (in ohms)
    -60 381.54
    -50 401.50
    -40 421.32
    -30 441.07
    -20 460.77
    -10 480.42
    +0 500.00
    10 519.52
    20 538.97
    30 558.37
    40 577.71
    50 596.99
    60 616.21
    70 635.37
    80 654.47
    90 673.51
    100 692.50
    110 711.43
    120 730.30
    130 749.11
    140 767.86
    150 786.56
    160 805.19
    170 823.78
    180 842.30
    190 860.77
    200 879.17
    210 687.53
    220 915.82
    230 934.06
    240 952.24
    250 970.36
    260 988.43

    1. If the resistance values is different from the table above, replace the faulty WAITS sensing elements and do close out.
    2. If the resistance values are same as the table above, continue with next step.

  3. Interchange DAU 4 with DAU 2.

    1. If system checks are good, replace DAU 4 and do close out.
    2. If fault remains, continue with next step.

  4. Replace BMC 2.
  5. Do close out.

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