08/14/24
Message Overview:
Fault Message:
GEN1 DRIVE SHAFT FAIL/INVALID % N2
Fault Code:
2421200LPS
Associated CAS:
| Reporting LRU: | Generator Control Unit (GCU) 1 |
| System Description: | 24-21-00 |
| Schematic Diagram: | 24-21-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 24-21-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Message Description:
Variable Frequency Generator (VFG) 1 has tripped off-line or will not come on-line.
Possible Causes:
- Generator Control Unit (GCU) 1 (A56)
- Variable Frequency Generator (VFG) 1 (G1)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin:
- AW700-24-0598 - Variable Frequency Generator (VFG) GL511-1103-9 - Failure
Forum Articles/Infoservice/Newsletter:
- Reference Instruction Letter (RIL) GX-0198 - Return to service following VFG bearing failure and/or VFG housing rupture.
Flight Operation Notifications Manual (FONM): None
NOTES:
- Prior to T/S procedures, perform a visual of generator 1 for heat distress. Confirm if the heat exchanger is blocked with FOD.
- 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 Variable Frequency Generators (VFG) | AMM 24-21-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Variable Frequency Generators (VFG) | AMM 24-21-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| 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 ] |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- Access CAIMS and check if the following faults messages are active:
- 2421126LPS - GEN1 OIL OVERTEMP FAULT
- 2421124LPS - GEN1 [DIFF PROTECTION FEEDER]
Inspect the VFG for the following:
- VFG oil filter bypass indicator tripped, and/or
- Metal particles in the oil lines, and/or
- VFG end frame cracked or breached, and/or
- Oil sight glass cracked
- If there is a combination of the listed CAIMS fault messages and VFG condition(s) perform RIL GX-0198
- If there is NO combination, continue with next step.
- Interchange GCU #1 with GCU #2 (physically or using the GCU patch cable).
NOTE: Use CAIMS to monitor the fault on GCU.- If system checks are good, replace GCU 1 and do close out.
- If fault remains, continue with next step.
- Disconnect G1P1 (VFG 1) and A56P1 (GCU 1). Do a continuity check as follows:
From To Result A56P1-E Ground A56P1-F Ground A56P1-G Ground - If there is continuity, repair defective wiring as required.
- If there is NO continuity, continue with next step.
- Do a continuity check between GCU 1 and VFG 1 as follows:
From To Result A56P1-E G1P1-G A56P1-F G1P1-C A56P1-G G1P1-L - If there is continuity, continue with next step.
- If there is NO continuity, repair defective wiring as required.
- Disconnect connector A54P6 (ACPC) and connector A56P2 (GCU 1). Perform a wiring check between A56P2 and A54P6 as follows:
From To Result A56P2-9 A54P6-a A56P2-15 A54P6-b - If wiring checks are not good, repair wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Replace VFG 1.
- Do close out.