Diamond Aircraft DA 40 NG, Airplane Flight Manual

Page: 50 / 326

Operating
Limitations
DA 40 NG AFM
Page 2 - 14 Rev. 3 01-Jul-2014
EASA
approved
Doc. # 6.01.15-E
Color and Significance of the Caution Lights (Amber)
Caution Alerts (Amber)
Meaning / Cause
G1000
installed
SED, MED,
White Wire
installed
CAUTION CAUTION One of the cautions below is being indicated.
ECU A FAIL ECU A
A fault has occurred in the engine ECU A
or
ECU A is being tested during FADEC-test
procedure during the 'Before Take-Off Check'.
ECU B FAIL ECU B
A fault has occurred in the engine ECU B
or
ECU B is being tested during FADEC-test
procedure during the 'Before Take-Off Check'.
FUEL LOW LOW FUEL Left fuel quantity is low.
VOLTS LOW LOW VOLTS Engine bus voltage is too low (< 25 V).
COOL LVL WATERLEV Engine coolant level is low.
PITOT FAIL PITOT Pitot heat has failed.
PITOT HT
OFF
- Pitot heat is OFF.
LOI -
GPS integrity is insufficient for the current
phase of flight.
AHRS ALIGN:
Keep Wings
Level
-
The AHRS (Attitude and Heading Reference
System) is aligning.
- ENGINE Engine limit exceeded.