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Troubleshooting
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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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For AOG assistance contact:

CRC Montreal (YUL)
Quick Links

01/26/21

Message Overview:

SPOILERS FAULT
(Caution)

DDG Reference: None
Pilot Action (QRH): FCTL 07-11
System Description: 27-61-00
Schematic Diagram: 27-61-00
Wiring Diagram: 27-61-01
27-61-03
27-61-05
27-61-07
27-61-09
27-61-13
27-61-17

Message Description:

One or more of the spoiler PCU panels have failed or one or more of the ground spoilers is up prior to touchdown.

  • The spoiler system malfunction detection with automatic fail-safe shutdown and fault annunciation has detected a fault with a PCU or disagreement with command outputs with the PSEU inputs of ground spoiler position.
  • Inhibited on ground when the engines are shutdown except for SECU failure.
  • Also, inhibited when the SPOILERS FAIL (Amber) message is annunciated.

NOTE: A failed Radio Altimeter Transceiver (RAD ALT) can cause a SPOILER FAULT (Amber) CAS message to be posted.

Possible Causes:

  • Data Concentrator Unit (DCU) (A14)
  • Spoiler Electronic Control Unit 1 (SECU1) (A118)
  • Spoiler Electronic Control Unit 2 (SECU2) (A119)
  • Radio Altimeter Transceiver (RAD ALT) (A32)
  • Throttle Quadrant Assembly (TQA) Spoiler Idle Switch (A51)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

  • AW300-27-0037 - Spoiler Electronic Control Unit (SECU) - Circuit Breaker Reset Procedure
  • AW300-27-0077 - Troubleshooting Guide for Spoiler Electronic Control Unit and Horizontal Stabilizer Trim Electronic Control Unit
  • AW300-27-0081 - Spoiler Electronic Control Unit (SECU) and Horizontal Stabilizer Electronic Control Unit (HSTECU) - Cold Temperature Circuit Breaker Reset Procedure
  • AW300-27-0302 - SPOILERS FAULT EICAS Message Caused by TQA Idle Switch
  • AW300-27-0317 - SPOILERS FAULT EICAS message caused by SECU INTERNAL FAULT
  • AW300-27-0322 - Introduction of new SECU software for PN C47330-006/006A, C47330-008/008A and C47330-011

Forum Articles/Infoservice/Newsletter: None

NOTE: If CAS messages SPOILERS FAULT (Caution), SPOILERS FAULT (Advisory) and STAB TRIM FAULT (Advisory) are all displayed at the same time on the EICAS momentarily for few seconds (between 3 to 20 seconds) and possibly MDC messages B3-007899 - XTALK ARINC BUS [SPOILER ECU 1] or B3-007932 - XTALK ARINC BUS [SPOILER ECU 2], B3-007882 - NO L-SECU-1 BUS TO DCU [SPOILER ECU 1], B3-007915 - NO R-SECU-1 BUS TO DCU [SPOILER ECU 2] and B3-007969 - INVALID SECU INPUT [STALL COMPUTER] displayed together in the fault message history at the time of failure, download and send both SECU NVM files to the Bombardier Customer Response Center (CRC) for analysis.

Quick Links:

Removal of the Flight-Spoiler Control Lever AMM 27-61-01-000-801
Installation of the Flight-Spoiler Control Lever AMM 27-61-01-400-801
Operational Test of the Flight-Spoiler Control Lever AMM 27-61-01-710-801
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 27-61-05-820-801
Electronic Rigging of the Spoiler Electronic-Control Unit (SECU) AMM 27-61-05-820-802
Removal of the Multi-Function Spoiler Rotary Variable-Differential Transformer (MFS RVDT) AMM 27-61-11-000-801
Installation of the Multi-Function Spoiler Rotary Variable-Differential Transformer (MFS RVDT) AMM 27-61-11-400-801
Rigging Check of the Multi-Function Spoiler Rotary Variable-Differential Transformer (MFS RVDT) AMM 27-61-11-220-801
Operational Test of the Multi-Function Spoiler System AMM 27-62-00-710-801
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. If you experience a SPOILERS FAULT - Amber or Cyan EICAS message, combined with a B3-007883 and/or B3-007916 MDC fault in the CURRENT FAULTS and/or FAULT HISTORY, in order to prevent an unnecessary removal, ask the crew to perform MDC and SECU NVM download and look if the fault was triggered by "LTQAIdSwID" or "RTQAIdSwID" in the SECU NVM. If this is the case, replacing the TQA will fix the issue.
  2. If the fault is intermittent and is related to one specific SECU, swap the SECU 1 and 2 and perform an electronic rigging. Monitor the condition and if the fault returns and has followed the SECU, remove and replace the unit.
    NOTE: Perform electronic rigging of both SECUs when either SECU is swapped or replaced. The intent is if a SECU that is being installed was previously rigged in a different location in the same aircraft or it is being installed in a different aircraft or the SECU is a spare part it requires electronic rigging per the instructions in AMM TASK 27-61-05-400-801 Installation of the Spoiler Electronic-Control Unit (SECU).
  3. Refer to AW300-27-0037, the radio altimeter system may interfere with the system proper operation. Additional information can be gained from the MDC non-volatile report page by checking the individual SECU for faults.
    NOTE: A metallic or reflective surface (Water, Ice, metal plates, metal grills, etc...) underneath the RA antennas when aircraft is on the ground can cause erratic readings and cause the unit to fail. The first thing that should be attempted is move the A/C a few feet and test the system again.
  4. Retrieve from MDC faults associated to the spoiler system, either nomenclature, or Equation ID #.
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