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(WARNING)
RED MESSAGE (CAUTION)
AMBER MESSAGE (ADVISORY)
CYAN MESSAGE (STATUS)
WHITE MESSAGE Require immediate crew attention. These messages are accompanied by flashing master warning, triple chime attenson with or without voice message or dedicated tone. Require immediate crew awareness and future crew action may be required in the form of alternate system selection or performance limitation. These message are accompanied by flashing master caution and a single chime. Indicate safe or normal system operation which require crew awareness, over and above the dark cockpit philosophy. Indicate minor failures or reduction in systems capability, which require no crew action.

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03/03/21

Message Overview:

Message Name:

HYDRAULIC SOLENOID 6

Message Code:

B3-305874

Associated CAS:

R ENGINE FAULT
(Advisory)

Reporting LRU: R ENG HYD BYP
System Description: 29-15-00
Schematic Diagram: 76-11-00
Wiring Diagram: None

Message Description:

A fault in the harness between the hydraulic bypass control valve and the ECU A or B was sensed. Right engine hydraulic bypass solenoid fault 6. MCID 1609

Possible Causes:

  • Aircraft Circuit Breakers
  • W1 Wiring Harness
  • W4 Wiring Harness
  • W6 Wiring Harness
  • Aircraft Wiring Harness from the Pylon Interface to the Aircraft Power Circuit Breaker
  • Hydraulic Pump By-pass Solenoid
  • Full Authority Digital Engine Control (FADEC) Electronic Control Unit A (ECU) (A40)
  • Full Authority Digital Engine Control (FADEC) Electronic Control Unit B (ECU) (A42)
  • Aircraft 28 VDC Power Source
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

None

Troubleshooting Recommendations:

  1. MCID 1609 fault present, troubleshoot using the following steps for aircraft and engine fault isolation with reference to the Light Engine Maintenance Manual TASK 72-00-00-810-341.

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