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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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Quick Links

06/22/21

Message Overview:

Message Name:

AUDIO PANEL 1 MALFUNCTIONS

Message Code: 235OBS001
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 Switch
  • Audio Control Panel 1 (A8)
  • 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 1 with Audio Panel 2. Is the fault still present?

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

  2. Disconnect Audio Panel 1 connector (A8P1) and perform a voltage check as follows:

    Audio Panel 1 Expected Result Result
    A8P1-V 28 VDC
    A8P1-U 28 VDC
    A8P1-M Ground

    1. If the power and/or ground value is not as specified above, investigate power sources (SPDA 1 or SPDA 4) or interface wiring and do close out.
    2. If the power and/or ground value is as specified above, 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
    A8P1-d A1P1-56
    A8P1-p A1P1-70
    A8P1-d A3BP1-42
    A8P1-p A3BP1-29
    A8P1-c A2P1-56
    A8P1-n A2P1-70
    A8P1-c A4BP1-42
    A8P1-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 1 connector A8P2. Disconnect RMU 1 connector (A25P1) and RMU 2 connector (A26P1). Perform a continuity check as follows:

    From To Result
    A8P2-L A25P1-h
    A8P2-L A26P1-h

    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
    A8P2-B A11BP1-77
    A8P2-W A11BP1-76
    A8P2-X A10CP1-32
    A8P2-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
    A8P1-G A2P1-31
    A8P1-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
    A8P2-t A7EP1-3F
    A8P2-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
    A8P2-m A64BP1-C13
    A8P2-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
    A8P2-V A51P1-43
    A8P2-r A51P1-41

    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, refer 235OBS005.
  11. Remove Audio panels 1, 2 and 3. Perform a resistance check of the Audio Bus Thermistors as follows:

    From To Expected result Result
    A8P1-d A8P1-p R20 & R22=50 Ohms
    A8P1-c A8P1-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 1.
  13. Do close out.
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