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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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01/25/21

Message Overview:

GEAR BAY DET FAIL
(Caution)

DDG Reference: 26-14
Pilot Action (QRH): SMK 14-11
System Description: 26-14-00
Schematic Diagram: 26-14-00
Wiring Diagram: 26-11-05
26-13-01

Message Description:

The amber 'GEAR BAY DET FAIL' caution CAS message indicates the single loop MWW detection element monitored by the FIREX Control Unit has failed, short, open or loss of power.

  • If the resistance drops to zero or fall instantly, the CU will report a shorted MWW loop and produce an amber (Caution) 'GEAR BAY DET FAIL' indication.
  • The MDC will identify the three options through unique fault equations.

Possible Causes:

  • None

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

  • AW300-26-0249 - Landing GEAR BAY DET FAIL EICAS Message (20501 - 20999)

Forum Articles/Infoservice/Newsletter: None

Numerous FIREX Control Unit Internal failures (cyan 'FIRE SYS FAULT' advisory CAS message) and Gear Bay detection failures (amber 'GEAR BAY DET FAIL' caution CAS message) are reported on in-service aircraft. The failure remains until the FIREX Control Unit is shutdown or replaced. Once cleared, failure cannot be repeated.

  • In all cases the faults were cleared after replacing the FIREX Control Unit. Subsequent bench testing however declared the FIREX Control Units to be NFF and as a result, the root cause of these events remains unknown.
  • Kiddie Aerospace suspects that the FIREX Control Unit operational environment may have an influence on the system operation.

Pilot Action: Airspeed....250 KIAS maximum, LANDING GEAR switch....DN, After 5 minutes: LANDING GEAR switch...UP, continue flight.

Quick Links:

Removal of the FIREX Control Unit AMM 26-11-01-000-801
Installation of the FIREX Control Unit AMM 26-11-01-400-801
Electrical Bonding Test SPM 51-80-00-760-801
Wiring - Maintenance Practices - ALL SPM 20-12-00-02
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02
Electrical Connectors - Maintenance Practice - ALL SPM 20-20-00-02

Troubleshooting Recommendations:

  1. Interrogate the MDC as follows:

    1. On the cursor control panel, ensure the toggle switch is to the right and select Anti-Ice, ECS and Fuel buttons simultaneously. The MDC main menu should now be displayed on Display Unit #3.
    2. Using the joystick, select Current Faults (if the fault is active) or Aircraft History to research stored faults. From Aircraft History you can then select Fault Message History and locate the fault. Going into advanced diagnostics will provide an equation id for the fault identified.
    3. Select the MDC fault or equation from the drop down below to provide additional information to assist in troubleshooting.

45_current_faults

45_advance_diagnostics

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