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

02/02/21

Message Overview:

Message Name:

CH B FAULT
(Service Message)

Message Code:

B3-006666

Associated CAS:

AIR COND FAULT
(Advisory)

Reporting LRU: CAB DUCT T SNSR
System Description: 21-61-00
Schematic Diagram: None
Wiring Diagram: 21-61-13
21-61-29

Message Description:

Both channels of the CABIN DUCT TEMPERATURE SENSOR are detected failed. Check for the sensor failure.

Possible Causes:

  • Cabin Duct Temperature Sensor (MT26)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

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
Removal of the Cabin Duct Temperature-Sensor AMM 21-61-13-000-801
Installation of the Cabin Duct Temperature-Sensor AMM 21-61-13-400-801
Standard Practices - Replace Wiring SPM 20-12-00-02
Standard Practices - Continuity Test SPM 20-12-01-05
Standard Practices - Repair Wiring SPM 20-12-10-02

Troubleshooting Recommendations:

  1. Disconnect connector MT26P1. Check continuity between pins 1 to 3 and 4 to 5 on theCabin Duct Temp Sensor. Ref chart below for resistance values. Replace sensor if out of range.
  2. Reconnect MT26P1 and gain access to IASC #2.
  3. Disconnect A56P1 and check resistance between pins 1 and 2. Compare to readings recorded between pins 1 and 3 of step 1. If resistance is substantially higher verify wiring between the IASC #2 and Duct Temp Sensor.
  4. Disconnect A56P3 and check resistance between pins 4 and 5. Compare to readings recorded between pins 4 and 5 of step 1. If resistance is substantially higher verify wiring between the IASC #2 and Duct Temp Sensor.
  5. If the Cabin Duct Temp Sensor and all wiring appears good recommend swapping IASCs for further troubleshooting.

Contact Field Service for any additional support required.

Temp Temp Ω
°C °F
-75 -103 1414110
-65 -85 419370
-55 -67 289124
-50 -58 201034.5
-45 -49 141586.8
-40 -40 100700.4
-35 -31 72802.5
-25 -13 39125.4
-20 -4 29091.9
-15 5 21886.5
-5 23 12698.1
0.0 32 9795.3
5 41 7617.3
15 59 4713
25 77 3000
30 86 2417.1
Temp Temp Ω
°C °F
40 104 598.1
50 122 1080.9
60 140 746.4
70 158 525.6
80 176 376.5
90 194 274.5
100 212 203.4
110 230 153.3
120 248 117
130 266 90.3
140 284 70.5
150 302 55.8
160 320 44.139
180 356 28.9
200 392 19.6
225 437 12.5
Registered and/or unregistered trademarks of Bombardier Inc. or its subsidiaries. © 2015 Bombardier Inc. All rights reserved.