Tecnam P-Mentor - Page 79

1
st
Edition - Rev. 0
Section 3 – EMERGENCY PROCEDURES
AVIONIC SYSTEM FAILURES
P-Mentor – Aircraft Flight Manual Page 3 - 15
4.3. ADC Failure
Annunciation window
Alert window
ADC FAIL
ADC Unit Failure
Display system is not receiving input from Air Data Computer. The following
information will be lost (large red X on the display field):
Airspeed
Altitude
Vertical Speed
INSTRUCTION: revert to stand-by instrument
4.4. EIS Failure
Annunciation window
Alert window
EIS FAIL
Engine Instrument System failure
Display system is not receiving input from Air Data Computer All engine information
are lost and a large red X appears on the engine display fields.
INSTRUCTION: Land as soon as possible