04/26/21
Message Overview:
Message Name:
GALLEY CONTROL PANEL DISPLAYS GRAPHICAL ARTIFACTS
| Identifier: | 441OBS011 |
| Effectivity: | Aircraft 20501 - 20999 |
| System: | nice® HD Cabin Management System |
| Associated CAS: | None |
| Reporting LRU: | GCP4110-001-001 |
| System Description: | SmartFix Plus 44-00-00, TUG C-ABT207-UG-001 |
| Schematic Diagram: | TUG C-ABT207-UG-001 |
| Wiring Diagram: | SWDM W1002467113 CMS Power Distribution SWDM W1004411113 CMS Network SWDM W1004411133 CMS Control SWDM W1004421113 Personal Control System |
Message Description:
Galley Control Panel (GCP) graphical artifacts (macro blocking/video quality lines and noises/flickering).
Possible Causes:
- Galley Control Panel (GCP)
- Harness Routing, leading to harness/connector damage near the GCP
- Associated Wiring
Required Conditions:
- Ensure the nice® HD system is booted up completely (power on and wait for about 5 minutes to ensure proper system status reporting).
- On Galley Control Panel (GCP) navigate to home, CMS equipment page, select item "system software" and ensure the aircraft MSN is contained in "current p/n" (e.g. for Challenger C350, MSN 20613: p/n SCDC350-20613-A or p/n SCDC3-20613-04A).
NOTE: If p/n is incorrect, contact the Bombardier Customer Response Center (CRC) for further instructions. - Use the GCP PATCH HARNESS to connect EIU with GCP.
Troubleshooting Tips:
Advisory Wire/Service Bulletin:
- SB 350-44-001 - MODIFICATION - Cabin Management System (CMS) - System Configuration Database Software Update
Forum Articles/Infoservice/Newsletter:
- EIU3009-SIL44-0001 - Ethernet Interface Unit: Increased time required for device update
- EIU Replacement Checklist - Checklist for EIU3009-001-001 replacement
- To check for release of updated System Software - Configuration Server Database (CSDB), please refer to Bombardier CIC webpage technical library, Service Bulletins for Challenger 350.
- Respective Lufthansa Technik "Engineering Bulletin Component" (EBC) documents are provided on this page as well.
More details in the nice® HD CMS/IFE system are available within the Lufthansa Technik document C-ABT207-UG-001, CL350 nice® HD Technical User Guide (TUG).
Quick Links:
| Lufthansa Technik Technical User Guide (TUG) | CL350 nice® HDC-ABT207-UG-001 |
| Lufthansa Technik Software Load Procedure (SLP) | CL350 nice® HDC-ABR142-UG-001 |
Troubleshooting Recommendations:
- On the GCP, ensure the system status is reported "ready".
- In case another system status other than "ready" is reported, go to the related observed fault.
- Gain access to the harness between the GCP and EIU 1. Check routing of the harness for obvious damages (refer to attached pictures "GCP_harness_damage_01" and "GCP_harness_damage_02").
- If inspection is good, continue with next step.
- If defects are found, rectify as required.
- Try to rock the harness near the GCP and observe if distortion is witnessed again.
- If damage is located at the GCP harness, replace the GCP.
- If no damage is found this way, continue with next step.
- Replace harness with a self-built patch cable in reference to "GCP PATCH HARNESS DRAWING".
- If damage is found on the aircraft side wiring, repair defective wiring as required.
- If all steps above do not fix the graphical distortion, contact the Bombardier Customer Response Center (CRC) for further help.
- Do close out.

