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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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02/12/21

Message Overview:

Message Name:

NO L-GP-4 BUS OUTPUT

Message Code:

B3-006949

Associated CAS:

None

Reporting LRU: IOC 1
System Description: 31-41-00
Schematic Diagram: None
Wiring Diagram: 31-45-01

Message Description:

L-GP-4 bus data not received at 3-OF (L-FADEC, R-FADEC, L-GPS, WXR) Or L-GP-4 bud data not received at L-GPS and WXR. Suspect failed L-GP-4 output or wiring.

Possible Causes:

  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Removal of the Junction Box JB1 AMM 24-63-01-000-802
Installation of the Junction Box JB1 AMM 24-63-01-400-802
Removal of the Integrated Avionics Processor System (IAPS) Card Cage (ICC) AMM 31-45-01-000-801
Installation of the Integrated Avionics Processor System (IAPS) Card Cage (ICC) AMM 31-45-01-400-801
Removal of the Input/Output Concentrator Unit (IOC) AMM 31-45-05-000-801
Installation of the Input/Output Concentrator Unit (IOC) AMM 31-45-05-400-801
Standard Practices - Replace Wiring SPM 20-12-00-02
Standard Practices - Wire Repair SPM 20-12-10-02

Troubleshooting Recommendations:

  1. Field experience has revealed that the MDC may report 'NO R-GP-4 BUS OUTPUT' and/or 'NO L-GP-4 BUS OUTPUT' message(s) as current faults under ATA22-12 IAPS with or without CAS messages.
  2. Bombardier recommends that Operators familiarize themselves with this issue and disregard these nuisance MDC messages prior to FADEC V10B and Avionics V6.0 upgrade. ECU or wiring should be diagnosed as faulty only if other related and nonrelated systems report the GP bus invalid.
  3. Refer to the following documents: AW300-22-0007, AW300-45-0016.

41_iaps_ioc_card

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