1
st
Edition - Rev. 0
Section 3 – EMERGENCY PROCEDURES
ELECTRICAL SYSTEM
P-Mentor – Aircraft Flight Manual Page 3 - 11
2.5. Loss of Main Bus
The loss/failure of main bus will be recognize with the simultaneous loss of the
following equipment:
Table 3-3 – Loss of Main Bus
Fail safe operation of G3X Touch allows pilot to transmit and
use COM1 using headphones only; speakers will not be
available.
For night flights, all instruments and map lights will be lost, but
emergency light will still be available.
1. Land as soon as practical
The loss/failure of avionic bus will be recognize with the simultaneous loss of
the following equipment:
Table 3-4 – Loss of Avionic Bus
1. Avionic Master switch …………………
2. Continue flight with PFD in reversionary mode
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