Operating Limitations DA 62 AFM
Color and Significance of the Caution Alerts on the G1000
Caution Alerts
(Amber)
Meaning/Cause
L/R ECU A FAIL
A fault was detected by 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 was detected by 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 engine bus voltage is too low (< 25 V).
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.
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.
L/R AUX FUEL E Left/Right auxiliary fuel tank empty (if installed).
CHECK GEAR Landing gear is not down and locked.
DEICE LVL LO De-icing fluid level is low (if installed).
Page 2 - 16 Rev. 0 11-Jan-2019
DOT
approved
Doc. No. 11.01.05-E
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