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(CAUTION)
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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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02/02/21

Message Overview:

Message Name:

CH A&B FAULT

Message Code:

B3-006662

Associated CAS:

TRIM AIR FAIL
(Caution)

Reporting LRU: CKPT 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 COCKPIT DUCT TEMPERATURE SENSOR are detected failed. Check for the sensor failure.

Possible Causes:

  • Cockpit Duct Temperature Sensor (MT35)
  • Integrated Air System (IAS) Controller(IASC1) (A55)
  • Integrated Air System (IAS) Controller(IASC2) (A56)
  • 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 Compressor Discharge Temperature-Sensor AMM 21-52-17-000-801
Installation of the Compressor Discharge Temperature-Sensor AMM 21-52-17-400-801
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 MT35P1. Check continuity between pins 1 to 3 (channel A) and 4 to 5 (channel b) on the Cockpit Temp Sensor. Ref chart for resistance values.
  2. Reconnect MT35P1 and gain access to IASC #1.
  3. Disconnect A55P1 and check resistance between pins 28 and 29. Compare to readings recorded between pins 1 and 3 of step 1. If resistance is substantially higher verify wiring between the IASC #1 and DTS.
  4. Disconnect A56P1 and check resistance between pins 28 and 29. Compare to readings recorded between pins 4 and 5 of step 1. If resistance is substantially higher verify wiring between the IASC #2 and Compressor Discharge Temperature Sensor.
  5. If the DTS is checking normal and fault still exists, recommend swapping IASCs for further troubleshooting.
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

60_duct_temp_sensor

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