11/19/25
Message Overview:
Message Name:
DISC INTF MOV DCPC/ SFCU#1/WRG
Message Code:
2751249STD
| Reporting LRU: | Slat / Flap Control Unit 1 (SFCU) |
| Associated CAS: | SLAT FLAP BIT (Advisory) |
| System Description: | 27-51-00 - Slats and Flaps Control and Indication System |
| Schematic Diagram: | [ G5000 ] [ Global Express ] [ Global XRS ] SSM 27-50-00-101 - Flaps and Slats System - Electrical Schematic |
| Wiring Diagram: | [ G5000 ] [ Global Express ] [ Global XRS ] WM 27-50-00-1_007 - Sheet 7 - Power Drive Unit (PDU) Motors No. 1 - ALL [ G5000 ] [ Global Express ] [ Global XRS ] WM 27-50-07-1_001 - Sheet 1 - Control Motors No. 1 - ALL |
Message Description:
MOVING 1/FLAPS IN MOTION discrete output from the Slat / Flap Control Unit 1 (SFCU) is defective.
Possible Causes:
- Slat / Flap Control Unit 1 (SFCU) (A124)
- DC Power Center (DCPC) (A63)
- DC Power Center (DCPC) (A63)/Primary Logic Card 1 (PLC)
- DC Power Center (DCPC) (A63)/Primary Logic Card 2 (PLC)
- DC Power Center (DCPC) (A63)/Primary Logic Card 3 (PLC)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Full Throttle Blog/Forum Articles/Infoservice/Newsletter: None
Flight Operation Notifications Manual (FONM): None
NOTES:
- The DCPC provides a 28 Volts DC discrete signal to the SFCU. The SFCU grounds this signal when the flap system is in motion. Performing a SLAT FLAP RESET on the EMS CDU may clear this fault.
- Wait at least one minute after SFCU reset to allow self test to run.
Quick Links:
| Grounding of the Aircraft | [ G5000 ] [ Global Express ] [ Global XRS ] AMM10-11-00-867-801 |
| Removal of the Covers and Plugs | [ G5000 ] [ Global Express ] [ Global XRS ] AMM10-12-00-020-801 |
| Installation of the Covers and Plugs | [ G5000 ] [ Global Express ] [ Global XRS ] AMM10-12-00-420-801 |
| Standard Aircraft Configuration for Maintenance | [ G5000 ] [ Global Express ] [ Global XRS ] AMM12-00-00-867-801 |
| Aircraft Walkaround (for Maintenance) | [ G5000 ] [ Global Express ] [ Global XRS ] AMM12-00-00-867-802 |
| Connect Electrical Power to the Aircraft | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-861-801 |
| Remove the Electrical Power from the Aircraft | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-861-802 |
| Electrical/Electronic Safety Precautions | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-910-801 |
| Electrostatic Discharge Safety Precautions | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-910-802 |
| Removal of the DC Power Center (DCPC) | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-61-00-000-801 |
| Installation of the DC Power Center (DCPC) | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-61-00-400-801 |
| Operational Test of the DC Power Center (DCPC) | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-61-00-710-801 |
| Removal of the DC Power Center (DCPC) Primary Logic | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-61-09-000-801 |
| Installation of the DC Power Center (DCPC) Primary Logic | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-61-09-400-801 |
| Operational Test of the DC Power Center (DCPC) Primary Logic | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-61-09-710-801 |
| Operational Test of the Slat/Flap Control System | [ G5000 ] [ Global Express ] [ Global XRS ] AMM27-51-00-710-801 |
| Removal of the Slat/Flap Control Unit (SFCU) | [ G5000 ] [ Global Express ] [ Global XRS ] AMM27-51-05-000-801 |
| Installation of the Slat/Flap Control Unit (SFCU) | [ G5000 ] [ Global Express ] [ Global XRS ] AMM27-51-05-400-801 |
| Access to Active Faults | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-802 |
| Access to Stored Faults | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-803 |
| Access to System Diagnostics | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-804 |
| Flight Deck Effect to Fault Correlations | [ G5000 ] [ Global Express ] [ Global XRS ] AMM45-45-00-970-821 |
| Safety Precautions - Maintenance Practices - ALL | [ G5000 ] [ Global Express ] [ Global XRS ] SPM20-00-01-02 |
| Electrical Wiring - Continuity Test - Adjustment /Test - ALL | [ G5000 ] [ Global Express ] [ Global XRS ] SPM20-12-01-05 |
| Wire Repair - Maintenance Practices - ALL | [ G5000 ] [ Global Express ] [ Global XRS ] SPM20-12-10-02 |
Troubleshooting Recommendations:
- Interchange SFCU 1 with SFCU 2 and confirm that they are installed properly and securely. Select a different Slat Flap Control Handle position.
- If system checks are good, replace SFCU 1 and do close out.
- If fault remains, continue with next step.
- Remove SFCU 1 and perform voltage check on the connector A124AP1 as follow:
SFCU 1 Expected Result Result A124AP1-16 28 Volt - If there is 28 Volts, do close out.
- If there is no 28 Volts, continue with next step.
- Perform wiring checks as follow:
From To Result A124AP1-16 A63P1-M - If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Remove the Primary Logic Cards one at a time and apply aircraft power.
- If fault clears after removal of any one primary logic card, replace that specific card and do close out.
- If fault remains, continue with next step.
- Remove all three DCPC Primary Logic Cards. Perform wiring check as follows:
From To Result P110B-5 A63P1-M P210B-5 A63P1-M P310B-5 A63P1-M Aircraft Ground A63P1-M - If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
CAUTION: TO PREVENT DAMAGE TO THE ACPC MOTHER BOARD CONNECTORS, ENSURE THAT THE JUMPER WIRE PINS OUTSIDE DIAMETER (OD) DOES NOT EXCEED 0.025 INCH.
- Replace DCPC.
- Do close out.