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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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06/26/19

Message Overview:

Fault Message:

ADC2 429/ SFCU/ WIRING

Fault Code:

2750005STD

Associated CAS:

SLAT-FLAP BIT
(Advisory)

Reporting LRU: Slat/Flap Control Unit (SFCU)
System Description: 27-51-00
Schematic Diagram: 27-50-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
34-11-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 27-50-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]
27-50-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]
34-11-03 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

Slat/Flap Control Unit (SFCU) does not receive input from Micro Air-Data Computer (MADC 2) or the data is not correct.

Possible Causes:

  • Micro Air-Data Computer (MADC) 2 (A28)
  • Junction Box (JB3) PCB4
  • Junction Box (JB6) PCB4
  • Slat/Flap Control Unit (SFCU) 1 (A124)
  • Slat/Flap Control Unit (SFCU) 2 (A95)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

Forum Articles/Infoservice/Newsletter: None

Performing a SLAT FLAP RESET on the EMS CDU may clear this fault.

NOTE: Wait at least one minute after SFCU reset to allow self test to run.

This fault may be posted due to the SFCU powering up prior to the LGECU. This fault will clear automatically when the LGECU powers up and provides an input.

Quick Links:

Removal of the Junction Box JB3 AMM 24-00-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Junction Box JB3 AMM 24-00-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Junction Box JB3 Circuit-Cards AMM 24-00-02-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Junction Box JB3 Circuit-Cards AMM 24-00-02-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Junction Box JB6 AMM 24-00-13-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Junction Box JB6 AMM 24-00-13-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Junction Box JB6 Circuit-Cards AMM 24-00-14-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Junction Box JB6 Circuit-Cards AMM 24-00-14-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Slat/Flap Control Unit (SFCU) AMM 27-51-05-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Slat/Flap Control Unit (SFCU) AMM 27-51-05-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Micro Air-Data Computers AMM 34-11-09-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Micro Air-Data Computers AMM 34-11-09-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. On the EMS CDU, select CTRL function and SLAT/FLAP RESET.
    NOTE: Wait at least one minute after SFCU reset to allow self-test to run.
  2. Cycle power to the ADC 1.

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

  3. Confirm SFCU 1 and SFCU 2 report the same fault.

    1. If reporting the same fault, go to step 6.
    2. If not reporting the same fault, continue with next step.
      NOTE:

      1. CPC and SFCU 2 are getting the ADC 1 Bus 3 information.
      2. SPC, GPS and SFCU 1 are getting the ADC 1 Bus 4 information.

  4. Reseat SFCUs.

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

  5. Perform wiring checks between SFCU 1 and JB3, SFCU 2 and JB6.
    Reported by SFCU 1:

    From To Result
    A124AP1-59 JB3FP1-8H
    A124AP1-72 JB3FP1-8J

    NOTE: The wiring check can also be do through the test point on the PC Board 4 inside the JB3.

    For 93 pins Test point Connector (JB3 PCB5 P/N 00514-0069-0002)
    TP-90 High
    TP-91 Low
    For 96 pins Test point Connector (JB3 PCB5 P/N 00514-0069-0001)
    TP-93 High
    TP-92 Low

    NOTE: The test point’s references inside the junction boxes in the wiring diagram are not necessarily accurate. (Reference CMM24-00-01)
    Reported by SFCU 2:

    From To Result
    A95AP1-59 JB6FP1-7H
    A95AP1-72 JB6FP1-7J

    NOTE: The wiring check can also be do through the test point on the PC Board 5 inside the JB3.

    For 93 pins Test point Connector (JB3 PCB5 P/N 00514-0069-0002)
    TP-4 High
    TP-35 Low
    For 96 pins Test point Connector (JB3 PCB5 P/N 00514-0069-0001)
    TP-4 High
    TP-36 Low

    NOTE: The test point’s references inside the junction boxes in the wiring diagram are not necessarily accurate. (Reference CMM24-00-01)

    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. Swap MADC 2 with MADC 1.

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

  7. Perform wiring checks between MADC 2 and JB3 (SFCU 1) or MADC 2 and JB6 (SFCU 2) corresponding to the bus that is reporting fault.

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

  8. Replace JB3 PCB4 (SFCU 1) or JB6 PCB4 (SFCU 2).

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

  9. Replace Right Wing Flap resolver.
  10. Do close out.
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