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

03/10/21

Message Overview:

Message Name:

NO R-CLOCK BUS OUTPUT

Message Code:

B3-397681

Associated CAS:

None

Reporting LRU: CLOCK
System Description: 31-21-00
Schematic Diagram: 31-21-00
Wiring Diagram: 31-21-01

Message Description:

Remote Data Concentrator (RDC) B CHANNEL is reporting the RIGHT CLOCK BUS input absent.

Possible Causes:

  • Digital Clock (A121)
  • Remote Data Concentrator (RDC) (A13)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Removal of the Digital Clock AMM 31-21-01-000-801
Installation of the Digital Clock AMM 31-21-01-400-801
Removal of the Remote Data Concentrator (RDC) AMM 31-41-05-000-802
Installation of the Remote Data Concentrator (RDC) AMM 31-41-05-400-802
Wiring - Maintenance Practices - ALL SPM 20-12-00-02
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02

Troubleshooting Recommendations:

  1. Reset CLOCK PWR (CB3-F9) and CLOCK (CB3-F8) circuit breakers.

    1. If system check passes, do close out.
    2. If fault remains, continue with next step.

  2. Confirm presence of the 28 VDC and Grounds at the Clock connector A121P1. Repair/replace as required.

    1. If system check passes, do close out.
    2. If fault remains, continue with next step.

  3. Verify the bus speed strapping (pin C & P) at clock connector A121AP1. Repair as required.

    1. If system check passes, do close out.
    2. If fault remains, continue with next step.
      NOTE: Aircraft pre S/B100-34-36 and Aircraft 20407 and below: Pin C & P are connected. Aircraft post S/B 100-34-36 and Aircraft 20408 and up: Pin C & P are NOT connected.

  4. Do the wiring check of the ARINC 429 data bus CLK-1 from the Clock connector A121P1 to the RDC connector A130DP1. Repair/replace as required.

    1. If system check passes, do close out.
    2. If fault remains, continue with next step.

  5. Replace the Clock.

    1. If system check passes, do close out.
    2. If fault remains, continue with next step.

  6. Replace the RDC.
  7. Do close out.
Registered and/or unregistered trademarks of Bombardier Inc. or its subsidiaries. © 2015 Bombardier Inc. All rights reserved.