03/03/21
Message Overview:
Message Description:
Right engine hydraulic bypass solenoid fault 5. A fault in the hydraulic bypass control valve or some other location common to the Electronic Control Unit (ECU) A or B was sensed. MCID 1608
Possible Causes:
- W1 Wiring Harness
- W4 Wiring Harness
- W6 Wiring Harness
- Aircraft 28 VDC Power Source
- Hydraulic Pump By-pass Switch Circuit Breaker
- Hydraulic Pump By-pass Solenoid
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
Quick Links:
None
Troubleshooting Recommendations:
- MCID 1608 fault present, troubleshoot using the following steps for aircraft and engine fault isolation with reference to the Light Engine Maintenance Manual TASK 72-00-00-810-340.