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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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For AOG assistance contact:

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01/17/25

Message Overview:

Message Name:

R HYDRAULIC INPUT FAIL

Message Code:

B3-007927

Associated CAS:

SPOILERS FAULT
(Advisory)

Reporting LRU: SPOILER ECU 1
System Description: 27-61-00 - Control and Indication (Spoilers)
Schematic Diagram: 27-61-00 - Flight Spoiler Control and Indication System
Wiring Diagram: 27-61-05 - Sheet 1 - Spoiler Electronic-Control Unit (SECU) No. 1 - 20501 TO 20806
27-61-05 - Sheet 2 - Spoiler Electronic-Control Unit (SECU) No. 1 - 20501 TO 20806
27-61-05 - Sheet 3 - Spoiler Electronic-Control Unit (SECU) No. 1 - 20501 TO 20806
27-61-05 - Sheet 1 - Spoiler Electronic-Control Unit (SECU) No. 1 - 20807 TO 20829
27-61-05 - Sheet 1 - Spoiler Electronic-Control Unit (SECU) No. 1 - 20830 TO 20874
27-61-05 - Sheet 1 - Spoiler Electronic-Control Unit (SECU) No. 1 - 20875 TO 20936
27-61-05 - Sheet 2 - Spoiler Electronic-Control Unit (SECU) No. 1 - 20875 TO 20936
27-61-05 - Sheet 1 - Spoiler Electronic-Control Unit (SECU) No. 1 - 20937 AND SUBS
27-61-05 - Sheet 2 - Spoiler Electronic-Control Unit (SECU) No. 1 - 20937 AND SUBS

Message Description:

No Right Hydraulic 2 System Input to Spoiler Electronic Control Unit 1 (SECU1).

Possible Causes:

  • Spoiler Electronic-Control Unit 1 (SECU 1) (A118)
  • Right Hydraulic System
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

Full Throttle Blog/Forum Articles/Infoservice/Newsletter: None

Flight Operation Notifications Manual (FONM): None

Quick Links:

Standard Aircraft Configuration for Maintenance AMM 12-00-00-867-803
Electrical/Electronic Safety Precautions AMM 24-00-00-910-801
Electrostatic-Discharge Safety Precautions AMM 24-00-00-910-802
Connect Electrical Power to the Aircraft AMM 24-00-00-861-801
Remove the Electrical Power from the Aircraft AMM 24-00-00-861-802
Removal of the Spoiler Electronic-Control Unit (SECU) AMM 27-61-05-000-801
Installation of the Spoiler Electronic-Control Unit (SECU) AMM 27-61-05-400-801
Electronic Rigging of the Spoiler Electronic-Control Unit (SECU) AMM 27-61-05-820-802
Functional Test of the Engine Driven Hydraulic Pump Auto Depressurization and Firewall Hydraulic Shutoff Valve Circuitry AMM 29-12-00-720-801
Visual Check of the Differential Pressure Indicators for the Pressure, Return, and Case-Drain Filter Manifolds AMM 29-12-00-210-801
Wiring - Maintenance Practices - ALL SPM 20-12-00-02
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02
Electrical Connectors - Maintenance Practice - ALL SPM 20-20-00-02

Troubleshooting Recommendations:

  1. Switch to Hydraulic synoptic page and check for any abnormal indications, magenta dashes for the hydraulic indication pages.
  2. Hydraulic pressure data is supplied to the SECU on the R-GP-5 bus, if the hydraulic information is good on the displays, troubleshoot the R-GP-5 ARINC databus.
  3. Additional troubleshooting on this condition, refer to AW300-29-0079.

30_pressure_transducer

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