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(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.

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Quick Links

07/05/19

Message Overview:

Fault Message:

FCM NOT POWERED [FCU #1]

Fault Code:

27657151SX

Associated CAS:

FLT SPOILERS FAULT
(Advisory)

Reporting LRU: Flight Control Unit (FCU) 1
System Description: 27-60-00
Schematic Diagram: 27-60-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 27-60-05 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

A Flight Control Module in Flight Control Unit (FCU) 1 does not receive power during the CAIMS Interface Test.

Possible Causes:

  • Flight-Control Unit (FCU) 1 (A65)
  • Secondary Power Distribution Assembly (SPDA) 2 (A14)
  • Secondary Power Distribution Assembly (SPDA) 4 (A16)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None.

Forum Articles/Infoservice/Newsletter: None

CAIMS interface test can be initated as follows:

  1. SYSTEM DIAG
  2. 27-00 FLIGHT CONTROLS
  3. FLIGHT CONTROL UNIT #1
  4. LRU TEST
  5. FLT CONTROL UNIT #1 INTERFACE TEST
  6. Confirm

Quick Links:

Removal of the DC Power Center (DCPC) Secondary-Power
Distribution Assembly (SPDA) Feeder		 AMM 24-61-37-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the DC Power Center (DCPC) Secondary-Power
Distribution Assembly (SPDA) Feeder		 AMM 24-61-37-400-801 [ 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 ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Re-rack FCU 1.

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

  2. Swap FCU 1 with FCU 2.

    1. If system checks are good, replace FCU 1. Reset FCUs latched faults and do close out.
    2. If fault remains, continue with next step.

  3. Measure for 28 VDC at FCU 1 and confirm voltage is not fluctuating.

    FCU 1 Expected Result Result
    A65CP1-11 28 VDC
    A65CP1-7 28 VDC
    A65FP1-11 28 VDC
    A65FP1-7 28 VDC

    1. If checks are good, do close out.
    2. If any of the checks fails, continue with next step.

  4. Confirm/Measure steady 28 VDC from corresponding SPDA by removing pin from SPDA's connector as follows:

    From To Expected Result Result
    A65CP1-11 A14P2-k 28 VDC
    A65CP1-7 Ground 28 VDC
    A65FP1-11 A16P2-g 28 VDC
    A65FP1-7 Ground 28 VDC

    1. If check fails, go to step 6.
    2. If checks are good, continue with next step.

  5. Perform wiring checks between FCU and corresponding SPDA.

    1. If wiring checks are not good, repair defective wiring as required and do close out.
    2. If wiring checks are good, continue with next step.

  6. Replace defective SPDA.
  7. Do close out.

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