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

06/22/21

Message Overview:

Message Name:

AUDIO PANEL 2 MALFUNCTIONS

Message Code: 235OBS002
Effectivity: All
System: Audio Integrating System
System Description: 23-51-00
Schematic Diagram: 23-51-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 23-51-55 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Message Description:

One or more audio panel functions do not operate correctly.

Possible Causes:

  • Audio Panel 2 (A9)
  • Secondary Power Distribution Assembly (SPDA) 1 (A13)
  • Secondary Power Distribution Assembly (SPDA) 4 (A16)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Removal of the Audio Panels AMM 23-51-05-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Audio Panels AMM 23-51-05-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Secondary-Power Distribution Assemblies AMM 24-62-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Secondary-Power Distribution Assemblies AMM 24-62-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Swap Audio Panel 2 with Audio Panel 1. Is the fault still present?

    1. If NO, go to step 12.
    2. If YES, continue with next step.

  2. Disconnect Audio Panel 2 connector (A9P1) and perform a continuity check as follows:

    Audio Panel 2 Expected Result Result
    A9P1-V 28 VDC
    A9P1-U 28 VDC
    A9P1-M Ground

    1. If the power and/or ground value is not as specified, repair defective wiring as required and do close out.
    2. If the power and/or ground value is as specified, continue with next step.

  3. For Audio Bus, disconnect VHF COMM units 1 and 2 and VHF NAV units 1 and 2. Perform a continuity check as follows:

    From To Result
    A9P1-d A1P1-56
    A9P1-p A1P1-70
    A9P1-d A3BP1-42
    A9P1-p A3BP1-29
    A9P1-c A2P1-56
    A9P1-n A2P1-70
    A9P1-c A4BP1-42
    A9P1-n A4BP1-29

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  4. For Marker Sensitivity, disconnect Audio Panel 2 connector A9P2. Disconnect RMU 1 connector A25P1 and RMU 2 connector A26P1. Perform a continuity check as follows:

    From To Result
    A9P2-L A25P1-i
    A9P2-L A26P1-i

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  5. For IAC Aural Warnings, remove IAC 1 and IAC 2. Perform a continuity check as follows:

    From To Result
    A9P2-B A11BP1-77
    A9P2-W A11BP1-76
    A9P2-X A10CP1-32
    A9P2-G A10CP1-33

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  6. For Emergency Audio, remove VHF COMM unit 2. Perform a continuity check as follows:

    From To Result
    A9P1-G A2P1-31
    A9P1-m A2P1-29

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  7. For TCAS Voice, remove the TCAS unit. Perform a continuity check as follows:

    From To Result
    A9P2-t A7EP1-3F
    A9P2-Z A7EP1-3G

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  8. For GPWS Audio, remove the GPWS unit. Perform a continuity check as follows:

    From To Result
    A9P2-m A64BP1-C13
    A9P2-J A64BP1-D13

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  9. For CVR Interface, remove the CVR unit. Perform a continuity check as follows:

    From To Result
    A9P2-V A51P1-37
    A9P2-r A51P1-35

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  10. For Cockpit Loudspeakers, perform a check for the cockpit loudspeakers. Refer COCKPIT LOUDSPEAKERS INOP.

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

  11. Remove Audio panels 1, 2 and 3. Perform a resistance check of the Audio Bus Thermistors as follows:

    From To Expected result Result
    A9P1-d A9P1-p R20 & R22 = 50 Ohms
    A9P1-c A9P1-n R21 & R23 = 50 Ohms

    1. If the resistance values are not as specified, repair defective wiring as required or replace the bus-termination resistors and do close out.
    2. If the resistance values are as specified, continue with next step.

  12. Replace Audio Panel 2.
  13. Do close out.
Registered and/or unregistered trademarks of Bombardier Inc. or its subsidiaries. © 2015 Bombardier Inc. All rights reserved.