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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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12/11/19

Message Overview:

ALL ADC MISCMP
(Caution)

DDG Reference: None
Pilot Action (QRH): AVNC 02-3
System Description: 34-11-00
Schematic Diagram: 34-11-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 34-11-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

The data from the three MADCs do not agree. (This is an external fault or probe fault that causes the autopilot and yaw damper to automatically disengage).

Possible Causes:

  • Air Data System is not calibrated correctly
  • Pitot-Static System has a leak
  • Temperature Probe
  • Pitot-Static Probe
  • Probe Heaters

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter:

Quick Links:

Functional Test of the Air Data Computer, (RVSM Qualified A/C) AMM 34-11-00-720-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Functional Test of the Pitot-Static Systems AMM 34-11-00-720-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Leak Test of the Pitot-Static System 1 AMM 34-11-00-790-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Leak Test of the Pitot-Static System 2 AMM 34-11-00-790-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Leak Test of the Pitot-Static System 3 AMM 34-11-00-790-803 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Leak Test of the Standby Pitot-Static System AMM 34-11-00-790-804 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Detailed Inspection of the Pitot-Static Probes AMM 34-11-01-220-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Pitot Line P1 Contamination Removal AMM 34-11-01-100-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Pitot Line P2 Contamination Removal AMM 34-11-01-100-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Pitot Line P3 Contamination Removal AMM 34-11-01-100-803 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Pitot Line P STBY Contamination Removal AMM 34-11-01-100-804 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Static Line P1 S1/P STBY S2 Contamination Removal AMM 34-11-01-100-805 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Static Line P2 S1/P3 S2 Contamination Removal AMM 34-11-01-100-806 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Static Line P3 S1/P2 S2 Contamination Removal AMM 34-11-01-100-807 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Static Line P STBY S1/P1 S2 Contamination Removal AMM 34-11-01-100-808 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Cleaning of the Pitot-Static Probes AMM 34-11-01-160-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Servicing of the Visual Drains AMM 34-11-03-616-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Do the procedures that follow until the fault of the ADC system is isolated:

    1. Functional test of the ADC system.
    2. Detailed inspection of the pitot-static probes.
    3. All Pitot system contamination removal tasks (see Quick Links: section above)
      NOTE: This step should be performed, regardless if contamination is found in the moisture traps.
    4. Functional test of the pitot-static systems.
    5. Leak test of the pitot-static system 1.
    6. Leak test of the pitot-static system 2.
    7. Leak test of the pitot-static system 3.

  2. Do close out.
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