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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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12/07/23

Message Overview:

Message Name:

CH A FAULT
(Service Message)

Message Code:

B3-006458

Associated CAS:

AIR COND FAULT
(Advisory)

Reporting LRU: CKPT T SEL PNL
System Description: 21-61-00
Schematic Diagram: SMM 21-61-00-101 - Temperature Control and Indication
Wiring Diagram: 21-61-00 - Cabin/Cockpit Temperature Control - ALL

Message Description:

The Channel A of the COCKPIT TEMPERATURE SELECTOR located on the bleed/air conditioning panel is detected failed.

Possible Causes:

  • Cockpit Temperature Selector (CKSEL) (R02)
  • Air Cond/Bleed Control Panel (PL17)
  • Integrated Air System Controller (IASC1) (A55)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Fault Confirmation Procedure:
{Term Definitions}

  • IAS1A-56 XX 353 00 EXCT XXXX-XXXX XXTX-XXXX XXXX-XXXX 353A: 22; COCKPIT TEMP SELECTOR A
  • IAS2A-61 XX 353 10 EXCT XXXX-XXXX XXTX-XXXX XXXX-XXXX 353A: 22; COCKPIT TEMP SELECTOR B

Quick Links:

Standard Aircraft Configuration for Maintenance AMM 12-00-00-867-803
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
Electrical/Electronic Safety Precautions AMM 24-00-00-910-801
Electrostatic-Discharge Safety Precautions AMM 24-00-00-910-802
Connect Electrical Power to the Aircraft AMM 24-00-00-861-801
Remove the Electrical Power from the Aircraft AMM 24-00-00-861-802
Removal of the Bleed-Air Control Panel AMM 36-11-57-000-801
Installation of the Bleed-Air Control Panel AMM 36-11-57-400-801
General SPM20-20-00-02-01
Connector Integrity After a Disconnect and Re-Connection SPM20-20-00-02-06

Troubleshooting Recommendations:

  1. Check resistance of cockpit temp selector at connector PL17J1 between pin 33 and 35. Expected result 9.5 kΩ. If resistance value is other than 9.5 kΩ, replace the potentiometer R2.
  2. Check resistance of cockpit temp selector at connector PL17J1 between pin 34 and 35 while rotating the knob. Expected result, linear variant from 0 to 9.5 kΩ. If the resistance is not linear up to 9.5 kΩ replace the potentiometer R2.
  3. Do a continuity check between connector PL17P1 pin 35 to connector A55P2 pin 71.
  4. Do a continuity check between connector PL17P1 pin 34 to connector A55P2 pin 70.
  5. Do a continuity check between connector PL17P1 pin 33 to connector A55P2 pin 78.
  6. If all the above is good, swap IASC 1 with IASC 2.
  7. If fault follows, replace faulty IASC.
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