06/25/19
Message Overview:
Fault Message:
GEN2 LINE CT OPEN/SHORT FAULT
Fault Code:
2422123LPS
Associated CAS:
| Reporting LRU: | Variable Frequency Generator (VFG) 2 |
| System Description: | 24-21-00 |
| Schematic Diagram: | 24-21-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 24-21-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
Variable Frequency Generator (VFG) 2 has tripped off-line or will not come on-line.
Possible Causes:
- AC Power Center (ACPC) (A54)
- Generator Control Unit (GCU) 2 (A57)
- Line Current Transformer Assembly (LCTA)
- Variable Frequency Generator (VFG) 2 (G2)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
A GCU patch cable (GSE REF # 24X-24-02) can be used to swap GCUs 1, 4 and 5 into position 2 or 3 (for troubleshooting only).
The GCU NVMs can only be downloaded at position #2 or #3.
Quick Links:
| Removal of the Generator Control Units (GCU) | AMM 24-24-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Generator Control Units (GCU) | AMM 24-24-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the AC Power Center (ACPC) | AMM 24-51-00-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the AC Power Center (ACPC) | AMM 24-51-00-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the AC Power Center (ACPC) Line Current Transformers | AMM 24-51-49-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the AC Power Center (ACPC) Line Current Transformers | AMM 24-51-49-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- Swap GCU 2 with GCU 3 (physically or using the GCU patch cable).
NOTE: Use PMAT to monitor the fault on GCU.- If system checks are good, replace GCU 2 and do close out.
- If fault remains, continue with next step.
- Disconnect connector PL2 on LCTA 2.
- Perform continuity checks (open circuit = failure) within LCTA 2 as follow:
From To Result PL2-1 PL2-4 PL2-2 PL2-4 PL2-3 PL2-4 - If there is continuity, go to step 5.
- If there is no continuity, continue with next step.
- Replace LCTA 2.
- If system checks are good, do close out.
- If fault remains, continue with next step.
- Disconnect connector A57P2 (GCU 2).
- Perform continuity checks between GCU2 and LCTA2 as follow:
From To Result A57P2-62 PL2-4 A57P2-63 PL2-3 A57P2-57 PL2-2 A57P2-49 PL2-1 - If there is continuity, go to step 10.
- If there is no continuity, continue with next step.
- Disconnect connector A54P7 (ACPC).
- Perform continuity checks (open circuit = failure) between GCU 2 and A54P7 as follow:
From To Result A57P2-62 A54P7-H A57P2-63 A54P7-G A57P2-57 A54P7-F A57P2-49 A54P7-E - If there is continuity, go to step 12.
- If there is no continuity, continue with next step.
- Repair aircraft wiring between GCU 2 and ACPC as follows:
From To Result A57P2-62 A54P7-H A57P2-63 A54P7-G A57P2-57 A54P7-F A57P2-49 A54P7-E - If system checks are good, do close out.
- If fault remains, continue with next step.
NOTE: Call Bombardier for decision to repair ACPC wiring or replace ACPC.
- Disconnect connector A54P7 (ACPC) and leave PL2 disconnected.
- Perform wiring checks (short circuit = failure) at connector A54P7 between pins H, G, F and E.
- If wiring checks are not good, repair wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Replace ACPC.
- Do close out.