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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

08/06/24

Message Overview:

STALL WARN ADVANCE
(Caution)

DDG Reference: None
Pilot Action (QRH): ADVISORY 7-5
System Description: 27-32-00
Schematic Diagram: 27-32-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 27-32-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Message Description:

SPC - Channel A or Channel B is in advance mode.

Possible Causes:

  • Stall Protection Computer (SPC)
  • The pilot or copilot makes an advance mode selection from the EMS CDU
  • There is a flap failure
  • There is a slat failure
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

  • AW700-24-0174 - Intermixing SPDA -13 or -15 with SPDA -9 or-11
  • AW700-27-0363 - No Fault Found Initiative: Stall Protection Computer

Forum Articles/Infoservice/Newsletter: None

Flight Operation Notifications Manual (FONM):

NOTES:

  • If you can confirm that a -13 SPDA is indeed physically installed in the #3 position and that you only have one -13 unit installed whereas the other three SPDAs are a mix of -7 and -9 units, then you can re-position the -13 SPDA to the #1 or #4 position per AW recommendation.

Quick Links:

Removal of Stall Protection Computer AMM 27-32-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of Stall Protection Computer AMM 27-32-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of Slat Flap Control Unit (SFCU) AMM 27-51-05-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of Slat Flap Control Unit (SFCU) AMM 27-51-05-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Access to Active Faults AMM 45-45-00-970-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Access to Stored Faults AMM 45-45-00-970-803 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair SPM 20-12-10 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Using the PMAT, access the Active Faults/Stored Faults as per AMM Tasks.
  2. Select related CAIMS message below:

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