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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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02/16/21

Message Overview:

Message Name:

NO OUTPUT

Message Code:

B3-007548

Associated CAS:

None

Reporting LRU: IAPS PWR 2
System Description: 31-45-00
Schematic Diagram: 31-45-00
Wiring Diagram: 31-45-09

Message Description:

Left IOC is reporting power failure for the Right IOC and 4 of the following LRUs are reporting a bus failure for the Right IOC (PFD 1, CDU 1, FMC 1, DCU 1, DCU 2, MFD 1, FGC 2, FMC 1).

Possible Causes:

  • Right Integrated-Avionics Processor System (IAPS) Power Supply (PWR 2) (A4-PWR)
  • Integrated-Avionics Processor System (IAPS) Card Cage (ICC) (A4)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

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 Integrated Avionics Processor System (IAPS) Power Supply (PWR) AMM 31-45-09-000-801
Installation of the Integrated Avionics Processor System (IAPS) Power Supply (PWR) AMM 31-45-09-400-801
Standard Practices - Replace Wiring SPM 20-12-00-02
Standard Practices - Wire Repair SPM 20-12-10-02

Troubleshooting Recommendations:

  1. Reset L IAPS Circuit Breaker CB1-B6, R IAPS Circuit Breaker CB2-B6. Is the fault message still present?

    1. If YES, continue with next step.
    2. If NO, do close out.
      NOTE: Before you open the IAPS circuit breakers, make sure that all Engine FADEC circuit breakers are open. If the Engine FADEC circuit breakers remain closed, Engine Igniters will activate. This can cause injury to persons and damage to equipment.

  2. With a multi-meter, verify presence of 28 VDC and GND for the IAPS PWR at the IAPS Card Cage (A4).

    From To Expected Result Result
    Conn. A4P104 - H Aircraft Ground 28 VDC
    Conn. A4P104 - J Aircraft Ground Approx. 0Ω
    Conn. A4P102 - 21 Aircraft Ground Approx. 0Ω
    Conn. A4P102 - 26 Aircraft Ground Approx. 0Ω

    1. If verification is satisfactory, continue with next step.
    2. If verification is not satisfactory, repair/replace defective component.

  3. Swap right IAPS PWR with left IAPS PWR. Is the fault message still present\?

    1. If YES, continue with next step.
    2. If NO, replace defective IAPS PWR.

  4. Replace IAPS card cage (A4).
  5. Do close out.
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