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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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04/23/24

Message Overview:

EQPT RACK COOL FAULT
(Advisory)

DDG Reference: 21-23
Pilot Action (QRH): AVNC 02-35
System Description: 21-21-00
Schematic Diagram: 21-23-00
Wiring Diagram: 21-23-05

Message Description:

The cyan 'EQPT RACK COOL FAULT' advisory CAS message indicates a fault has been detected in the avionics equipment rack cooling system.

  • The Integrated Air System Controller (IASC) handles all failures of the system automatically. The IASC 1 is the primary controller (normal operation) and IASC 2 ensures the backup control mode (degraded mode).
  • In normal operation, the AVFAN is operated when the aircraft altitude is lower than 25,000 ft or during descent phase. The fan is normally operated at high speed. It operates at a low speed in case of a single bleed operation. Above 25,000 ft, the AV is opened and the fan is switched off.
  • The transition from respectively fan to valve or valve to fan begins with fan shut-off or valve closure.

Possible Causes:

    • Avionics Cooling Fan (AVFAN) (B3)
    • Avionics Cooling Valve (MPE14)
    • Ventilated Temperature Sensor (VENTS) (MT39)
    • Integrated Air System Controller 1 (IASC 1) (A55 - FWD)
    • Integrated Air System Controller 2 (IASC 2) (A56 - AFT)

    Troubleshooting Tips:

    Advisory Wire/Service Bulletin: None

    Forum Articles/Infoservice/Newsletter: None

    NOTE:

    • If no rotation from the avionics cooling fan (B3) is sensed within 10 seconds,the avionics cooling valve (MPE14) in the belly goes to open and all power is lost at the avionics cooling fan motor.. Therefore, no voltage at stud T14 and T15 after 10 seconds. So, the avionics cooling fan (B3) is faulty.

    Quick Links:

    Operational Test of the Avionics Cooling System AMM 21-23-00-710-801
    Removal of the Equipment-Rack Vent Temperature-Sensor AMM 21-23-01-000-801
    Installation of the Equipment-Rack Vent Temperature-Sensor AMM 21-23-01-400-801
    Removal of the Avionics Cooling Fan AMM 21-23-05-000-801
    Installation of the Avionics Cooling Fan AMM 21-23-05-400-801
    Removal of the Avionics Cooling Valve AMM 21-23-09-000-801
    Installation of the Avionics Cooling Valve AMM 21-23-09-400-801
    Operational Test of the Avionics Cooling Valve AMM 21-23-09-710-801
    Removal of the Integrated Air System (IAS) Controller AMM 21-31-01-000-801
    Installation of the Integrated Air System (IAS) Controller AMM 21-31-01-400-801
    Operational Test of the Integrated Air System (IAS) Controller AMM 21-31-01-710-801
    Wiring - Maintenance Practices - ALL SPM 20-12-00-02
    Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02

    Troubleshooting Recommendations:

    1. Determine when the condition had happened, in flight above 25,000 ft or below.

      1. Below 25,000 ft a fan failure is detected by low rotational speed generating a discrete output to the IASC, or the avionics cooling valve is not closed. Above 25,000 ft the valve should be open with the fan off. Position switches on the valve provide discrete outputs to the IASC for position verification.
      2. Select the MDC fault or equation from the drop down below to provide additional information to assist in troubleshooting.

    10_iasc2_cha_avionics_valve_fan_status_pageeqpt_rack_cool_fault_eicas

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