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Level Text Color Importance Audible Tone
Warning Red May require immediate corrective action Warning chime tone which repeats without delay until acknowledged by the crew
Caution Amber May require future corrective action Single warning chime tone
Annunciation Advisory White None
Message Advisory White None
Safe Operation Annunciation Green Lowest None
Warning alerts Meaning / Cause
L/R ENG TEMP The annunciation is active when the engine coolant temperature is greater than 105 °C.
L/R OIL TEMP The annunciation is active when the engine oil temperature is greater than 140 °C.
L/R OIL PRES The annunciation is active when the engine oil pressure is less than 1 bar.
L/R FUEL TEMP The annunciation is active when the fuel temperature is greater than 75 °C.
L/R GBOX TEMP The annunciation is active when the gearbox oil temperature is greater than 120 °C.
L/R ALTN AMPS The annunciation is active when the alternator load is greater than 60 amps.
L/R ENG FIRE The annunciation is active when an engine fire is detected.
L/R STARTER This annunciation is used to indicate to the pilot that the starter is engaged when it should not be.
DOOR OPEN The annunciation is used to indicate to the pilot if the baggage-, canopy- or rear door is open.
POSN ERROR The annunciation is active when the G1000 will no longer provide GPS based navigational guidance.
ATTITUDE FAIL The annunciation is active when the display system is not receiving attitude reference information from the AHRS.
AIRSPEED FAIL The annunciation is active when the display system is not receiving airspeed input from the air data computer.
ALTITUDE FAIL The annunciation is active when the display system is not receiving altitude input from the air data computer.
VERT SPEED FAIL The annunciation is active when the display system is not receiving vertical speed input from the air data computer.
Warning alerts Meaning / Cause
HDG The annunciation is active when the display system is not receiving valid heading input from the AHRS.
WARN This annunciation constitutes a RAIM position warning. The nav deviation bar is removed.
Warning alerts Meaning / Cause
Landing Gear Retracted A warning chime tone which repeats without delay is active when the landing gear is retracted while the flaps move into the LDG position or when the POWER lever is placed in a position below 25 %.
Caution alerts Meaning / Cause
L/R ECU A FAIL or L/R ECU B FAIL The annunciation is active when a fault in ECU A or ECU B has occurred. In case of minor faults, the annunciation can be reset once by pressing the ECU TEST button for more than 2 seconds. However, the annunciation will re-appear upon the next attempt to start the engine.
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本文链接地址：钻石40系列飞机维护手册 DA 40 SERIES AIRPLANE MAINTENANCE MANUAL 4(32)
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