Operating Limitations DA 42 AFM
Page 2 - 14 Rev. 8 15-Dec-2017
EASA
approved
Doc. No. 7.01.05-E
Color and Significance of the Caution Alerts on the G1000
Caution Alerts
(amber)
Meaning / Cause
L/R ECU A FAIL
* A fault has occurred in the left/right engine ECU A (one reset
of minor faults is possible)
or
* ECU A is being tested during FADEC-test procedure during
the 'before take-off check'.
L/R ECU B FAIL
* A fault has occurred in the left/right engine ECU B (one reset
of minor faults is possible)
or
* ECU B is being tested during FADEC-test procedure during
the 'before take-off check'.
L/R FUEL LOW Left / Right main tank fuel quantity is low.
L/R ALTN FAIL Left / Right engine alternator has failed.
L/R VOLTS LOW Left / Right bus voltage is less than 25 Volts.
L/R COOL LVL Left / Right engine coolant level is low.
PITOT FAIL Pitot heat has failed.
PITOT HT OFF Pitot heat is OFF.
STAL HT FAIL Stall warning heat has failed.
STAL HT OFF Stall warning heat is OFF.
STICK LIMIT Control stick limiting system (variable elevator stop) has failed.
INTEG RAIM not
available
RAIM (Receiver Autonomous Integrity Monitor) is not available.
AHRS ALIGN:
Keep Wings
Level
The AHRS (Attitude and Heading Reference System) is aligning.
L/R AUX FUEL E Left / Right auxiliary fuel tank empty (if installed).
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