09/27/19
Message Overview:
Fault Message:
R SAV CH A WRG/SAV [SOL] RNG
Fault Code:
7326116RBR
Associated CAS:
| Reporting LRU: | Right Engine Electronic Controller (EEC) |
| System Description: | 80 -11-00 |
| Schematic Diagram: | 80-11-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 71-50-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
An electrical fault in the Starter Air Valve (SAV) Solenoid circuit CH A has been detected.
Possible Causes:
- Starter Air Valve (SAV)
- Right Engine Electronic Controller (EEC)
- Secondary Power Distribution Assembly (SPDA) 3 (A15)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
- Both CH A and CH B SAV Solenoid circuits faults must be detected to set the L ENG SAV FAIL (Caution) CAS message
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 ] |
| Opening of the Cowls | AMM 71-10-00-010-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Closing of the Cowls | AMM 71-10-00-410-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Eng Electronic Controller (EEC) Mod 73-101559 |
EMM 73-21-01-000-801-B00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Eng Electronic Controller (EEC) Mod 73-101559 |
EMM 73-21-01-400-801-B001 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Starter Air Valve | EMM 80-11-03-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Starter Air Valve | EMM 80-11-03-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- Check SAV solenoid channel A for power (P1065-1), 28 VDC should be present when SAV is commanded open.
- If there is 28 VDC, go to step 5.
- If there is no 28 VDC, continue with next step.
- Check for power 28 VDC at right engine disconnect 2JA2-32.
- If there is 28 VDC, go to step 4.
- If there is no 28 VDC, continue with next step.
- Perform wiring checks on the interface wiring between SPDA 3 and the Right Engine disconnect as follow:
From To Result A15P1-N 2JA2-32 - If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Swap SPDA 3 with SPDA 1. Is the fault still present?
- If NO, replace SPDA 3 and do close out.
- If YES, investigate the power input to SPDA 3 and continue with next step.
- Perform a continuity check for SAV solenoid winding at P1065 as follows:
From To Result P1065-1 P1065-5 - If there is no continuity, replace defective SAV and do close out.
- If there is continuity, continue with next step.
- Perform wiring checks between the SAV and the EEC.
- 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 wiring checks between the engine pylon disconnect 2PA2 and the EEC.
- If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Swap SAV between engines. Is the fault still present?
- If NO, replace defective SAV and do close out.
- If YES, continue with next step.
- Replace Right EEC.
- Do close out.