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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 R-IOC-1 BUS OUTPUT

Message Code:

B3-006963

Associated CAS:

None

Reporting LRU: IOC 2
System Description: 31-45-00
Schematic Diagram: 31-45-00
Wiring Diagram: 31-45-01
31-45-13

Message Description:

R-IOC-1 data absent at 2-of (R-PFD, R-MFD, L-PFD, L-MFD).

Possible Causes:

  • Adaptive Flight-Display (PFD 1) (A27)
  • Adaptive Flight-Display (PFD 2) (A26)
  • Adaptive Flight-Display (PFD 1) (A29)
  • Adaptive Flight-Display (PFD 2) (A28)
  • Junction Box 2 (JB2)
  • Right Input/Output Concentrator Unit (IOC) 2 (A4-IOC)
  • 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 Junction Box JB2 AMM 24-63-05-000-803
Installation of the Junction Box JB2 AMM 24-63-05-400-803
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
Removal of the Adaptive Flight-Display Unit AMM 31-61-01-000-801
Installation of the Adaptive Flight-Display Unit AMM 31-61-01-400-801
Standard Practices - Replace Wiring SPM 20-12-00-02
Standard Practices - Wire Repair SPM 20-12-10-02

Troubleshooting Recommendations:

  1. Reset 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. Swap right IOC with left IOC. Is the fault message still present.

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

  3. Disconnect one Adaptive Flight-Display Unit at the time (3 must be connected) and verify if the fault message is still present.
    1. If NO, replace the defective Adaptive Flight-Display Unit.
    2. If YES, repeat this step until all 4 Adaptive Flight-Display Units are confirmed not causing the fault message.

  4. Do wiring check between all Adaptive Flight-Display Units, through JB2, and the IAPS Card Cage (ICC).

    From To Result
    Conn. A27P2 - 21 Conn. A2P101 - 15
    Conn. A27P2 - 22 Conn. A2P101 - 16
    Conn. A29P2 - 21 Conn. A2P101 - 15
    Conn. A29P2 - 22 Conn. A2P101 - 16
    Conn. A26P2 - 21 Conn. A2P101 - 15
    Conn. A26P2 - 22 Conn. A2P101 - 16
    Conn. A28P2 - 21 Conn. A2P101 - 15
    Conn. A28P2 - 22 Conn. A2P101 - 16

    1. If the check is satisfactory, continue with next step.
    2. If the check is not satisfactory, repair defective wire or replace defective JB2.

  5. Replace Integrated Avionics-Processor System (IAPS) Card Cage (ICC) (A4).
  6. Do close out.
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