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Edition - Rev. 0
Section 3 – EMERGENCY PROCEDURES
AVIONIC SYSTEM FAILURES
P-Mentor – Aircraft Flight Manual Page 3 - 18
4.10. Garmin GDU(s) failure
In case of one GDU Failure:
The G3X Touch System automatically switches to reversionary mode.
In reversionary mode, the information is presented on the
remaining display in the split-screen configuration. In
reversionary mode, all important flight information is presented
on the remaining display in the same format as in normal
operating mode. The change to backup path is completely
automated for all LRUs and no pilot action is required.
In case of both GDU Failure:
INSTRUCTION: revert to standby instrument.
4.11. COM failure
If Complete communication failure occurred and no other COM sources are
available on board:
1. Transponder …………………………….
2. Land as soon as possible
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