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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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CRC Montreal (YUL)
Quick Links

07/06/21

Message Overview:

Message Name:

ENGINE TEMPERATURE IS TOO HIGH AT HIGH POWER WITH A TOO HIGH N1 SPEED IN FORWARD THRUST

Message Code: 771OBS002
Effectivity: All
System: Power
System Description: 77-10-00
Schematic Diagram: None
Wiring Diagram: None

Message Description:

The Engine temperature at high power and the speed of the N1 Rotor in forward thrust are more than the permitted limits. During Engine operation the Engine temperature and Rotor speeds are continuously monitored by the Full-Authority Digital Engine-Controller (FADEC).

Possible Causes:

None

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Electrical/Electronic Safety Precautions AMM 24-00-00-910-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Engine Safety Precautions AMM 71-00-00-910-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Opening of the Cowls AMM 71-10-00-010-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Closing of the Cowls AMM 71-10-00-410-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Deactivation of the Thrust Reverser
(for Maintenance)
AMM 78-30-00-040-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Activation of the Thrust Reverser
(for Maintenance)
AMM 78-30-00-440-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Perform the fault isolation for the engine overtemperature at high power with N1 overspeed in forward thrust by performing the fault isolation procedures:

  2. Do close out.
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