09/16/19
Message Overview:
Fault Message:
OPEN CKT- IMPDG BYPASS VLV & SW/WRG
Fault Code:
4960174APU
Associated CAS:
| Reporting LRU: | Full-Authority Digital Engine-Controller (FADEC) |
| System Description: | 49-60-00 |
| Schematic Diagram: | 49-61-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 49-12-01 [ Global Express ] [ G5000 ] [ Global XRS ] 49-61-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
The signals from the Impending Bypass Valve and Switch to the Full-Authority Digital Engine-Controller (FADEC) show a bypass condition before the Auxiliary Power Unit (APU) is ON. This shows a possible defective Impending Bypass Valve and Switch.
Possible Causes:
- Auxiliary Power Unit (APU) Full-Authority Digital Engine-Controller (FADEC) (A108)
- Impending Bypass Valve and Switch (S4)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
Quick Links:
| Removal of the Engine Branched Wiring-Harness | AMM 49-12-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Engine Branched Wiring-Harness | AMM 49-12-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Impending Bypass Valve-and-Switch | AMM 49-30-09-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Impending Bypass Valve-and-Switch | AMM 49-30-09-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Full-Authority Digital Engine-Controller (FADEC) | AMM 49-61-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Full-Authority Digital Engine-Controller (FADEC) | AMM 49-61-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- On the CAIMS PMAT, get access to the active faults.
- If the fault message FADEC CONTROLLER shows on the CAIMS PMAT, go to step 9.
- If the fault message FADEC CONTROLLER still shows on the CAIMS PMAT, continue with next step.
- Examine the engine branched wiring-harness for bare wiring, kinks, worn areas and other damage (WM 49-12).
- If the engine branched wiring-harness is not acceptable, go to step 7.
- If the engine branched wiring-harness is acceptable, continue with next step.
- Examine the impending bypass valve-and-switch (S4) receptacle for contamination and damage.
- If the impending bypass valve-and-switch (S4) receptacle is contaminated or damaged, go to step 8.
- If the impending bypass valve-and-switch (S4) receptacle is acceptable, continue with next step.
- Perform a continuity check within impending bypass valve-and-switch (S4) receptacle as follows:
From To Expected Result Result S4P1-A S4P1-B 50 ohms - If resistance check fails, go to step 8.
- If resistance checks good, continue with next step.
- Perform a wiring check between P1 (APU) and S4P1 (impending bypass valve-and-switch).
- If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Perform a wiring check between J802 (aircraft wiring harness) and A108BP1 (FADEC).
- If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Replace engine branched wiring-harness.
- If system checks are good, do close out.
- If fault remains, continue with next step.
- Replace Impending Bypass valve-and-switch (S4).
- If system checks are good, do close out.
- If fault remains, continue with next step.
- Replace FADEC.
- Do close out.