07/01/19
Message Overview:
Fault Message:
SPDA 2 FAILED (LEVEL C)-LEFT FUSE#1
Fault Code:
2463208SPD
Associated CAS:
| Reporting LRU: | Secondary Power Distribution Assembly (SPDA) 2 |
| System Description: | 24-60-00 |
| Schematic Diagram: | 24-61-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 24-62-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
Fuse F1 on left microprocessor in Secondary Power Distribution Assembly (SPDA) 2 is blown as reported by the SPDA 2.
Possible Causes:
- Secondary Power Distribution Assembly (SPDA) 2 (A14)
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
Quick Links:
| Removal of the Secondary-Power Distribution Assemblies | AMM 24-62-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Secondary-Power Distribution Assemblies | AMM 24-62-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- Cycle the aircraft power.
- If system checks are good, do close out.
- If fault remains, continue with next step.
- Replace SPDA 2.
- Do close out.