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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

07/04/19

Message Overview:

Fault Message:

AIR DATA COMPTR #2 FAULT [FCU 1]

Fault Code:

27654241SX

Associated CAS:

RUD AUTHORITY HIGH
(Caution)

Reporting LRU: Flight Control Unit (FCU) 2
System Description: 34-11-00
Schematic Diagram: 34-11-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 34-11-03 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

Flight Control Unit (FCU) 1 does not receive data from Air Data Computer (ADC) 2.

Possible Causes:

  • Air Data Computer (ADC) 2 (A28)
  • Flight Control Unit (FCU) 1 (A65)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Connect Electrical Power to the Aircraft AMM 24-00-00-861-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Remove the Electrical Power from the Aircraft AMM 24-00-00-861-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Opening of Non-Thermal Circuit Breakers AMM 24-00-00-863-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Closing of Non-Thermal Circuit Breakers AMM 24-00-00-863-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Electrical/Electronic Safety Precautions AMM 24-00-00-910-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Side Console Trim-Panels
(221EZ/222EZ, 221FZ/222FZ, 221TZ/222TZ)
AMM 25-12-05-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Side Console Trim-Panels
(221EZ/222EZ, 221FZ/222FZ, 221TZ/222TZ)
AMM 25-12-05-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Flight-Control Units AMM 27-61-05-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Flight-Control Units AMM 27-61-05-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Access to System Diagnostics AMM 45-45-00-970-804 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the External Avionics-Compartment
Access-Panel (140BB)
AMM 52-45-11-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the External Avionics-Compartment
Access-Panel (140BB)
AMM 52-45-11-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Safety Precautions - Maintenance Practices - ALL SPM 20-00-01-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Remove FCU 1 to get access to electrical connector A65AP1. Disconnect ADC 2 connector A28P1. Perform a continuity check as follows:

    From To Result
    A65AP1-11G A28P1-60
    A65AP1-11F A28P1-61

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

  2. Perform a continuity check as follows:

    From To Result
    A65AP1-11G Ground
    A65AP1-11F Ground

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

  3. Swap FCU 1 with FCU 2. Is the fault still present?

    1. If NO, replace FCU 1 and do close out.
    2. If YES, continue with next step.

  4. Replace ADC 2.
  5. Do close out.
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