Operating Limitations |
DA 42 NG AFM |
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2.6 WARNING, CAUTION AND ADVISORY ALERTS
2.6.1 WARNING, CAUTION AND ADVISORY ALERTS ON THE G1000
NOTE
The alerts described in the following are displayed on the
Garmin G1000. Section 7.10 includes a detailed description of the alerts.
The following tables show the color and significance of the warning, caution and advisory alerts lights on the G1000.
Color and Significance of the Warning Alerts on the G1000
Warning alerts |
Meaning / Cause |
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(red) |
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WARNING |
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One of the warnings listed below is being indicated. |
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L/R ENG TEMP |
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Left / Right engine coolant temperature is in the upper red |
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range (too high / >105 °C). |
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L/R OIL TEMP |
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Left / Right engine oil temperature is in the upper red range |
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(too high / >140 °C). |
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L/R OIL PRES |
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Left / Right engine oil pressure is in the lower red range |
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(too low / <1.5 bar). |
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L/R FUEL TEMP |
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Left / Right fuel temperature is in the upper red range (too |
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high / >60 °C) |
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L/R GBOX TEMP |
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Left / Right engine gearbox temperature is in the upper red |
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range (too high / >120 °C). |
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L/R FUEL PRESS |
Left / Right engine fuel pressure is low. |
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Page 2 - 12 |
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Rev. 1 |
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EASA |
Doc. No. 7.01.15-E |
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18-Feb-2009 |
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approved |
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DA 42 NG AFM |
Operating Limitations |
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Warning alerts |
Meaning / Cause |
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(red) |
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L/R ALTN AMPS |
Left / Right engine alternator output is in the upper red range |
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(too high / >70 amps). |
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L/R ENG FIRE |
Left / Right engine fire detected. |
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L/R STARTER |
Left / Right engine starter is engaged. |
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DOOR OPEN |
Front and/or rear canopy and/or baggage door are/is not |
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closed and locked. |
POSN ERROR |
G1000 will no longer provide GPS based navigational |
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guidance. |
ATTITUDE FAIL |
The display system is not receiving attitude reference |
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information from the AHRS. |
AIRSPEED FAIL |
The display system is not receiving airspeed input from the |
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air data computer. |
ALTITUDE FAIL |
The display system is not receiving altitude input from the air |
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data computer. |
VERT SPEED |
The display system is not receiving vertical speed input from |
FAIL |
the air data computer. |
HDG |
The display system is not receiving valid heading input from |
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the AHRS. |
WARN |
RAIM position warning. The nav deviation bar is removed. |
Doc. No. 7.01.15-E |
Rev. 1 |
18-Feb-2009 |
EASA |
Page 2 - 13 |
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approved |
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Operating Limitations |
DA 42 NG AFM |
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Color and Significance of the Caution Alerts on the G1000
Caution alerts |
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Meaning / Cause |
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(amber) |
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A fault has occurred in the left/right engine ECU A (one reset |
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of minor faults is possible) |
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L/R ECU A FAIL |
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or |
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ECU A is being tested during FADEC-test procedure during |
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the 'Before Take-Off Check'. |
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A fault has occurred in the left/right engine ECU B (one reset |
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of minor faults is possible) |
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L/R ECU B FAIL |
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or |
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ECU B is being tested during FADEC-test procedure during |
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the 'Before Take-Off Check'. |
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L/R FUEL LOW |
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Left / Right main tank fuel quantity is low. |
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L/R ALTN FAIL |
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Left / Right engine alternator has failed. |
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L/R VOLTS LOW |
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Left / Right engine bus voltage is too low (< 25 volts). |
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L/R COOL LVL |
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Left / Right engine coolant level is low. |
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PITOT FAIL |
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Pitot heat has failed. |
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PITOT HT OFF |
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Pitot heat is OFF. |
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STAL HT FAIL |
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Stall warning heat has failed. |
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STAL HT OFF |
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Stall warning heat is OFF. |
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STICK LIMIT |
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Control stick limiting system (variable elevator stop) has |
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failed. |
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INTEG RAIM not |
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RAIM (Receiver Autonomous Integrity Monitor) is not |
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available |
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available. |
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AHRS ALIGN: |
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The AHRS (Attitude and Heading Reference System) is |
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Keep Wings Level |
aligning. |
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Page 2 - 14 |
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Rev. 1 |
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EASA |
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Doc. No. 7.01.15-E |
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18-Feb-2009 |
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approved |
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DA 42 NG AFM |
Operating Limitations |
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Caution alerts |
Meaning / Cause |
(amber) |
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L/R AUX FUEL E |
Left / Right auxiliary fuel tank empty (if installed). |
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CHECK GEAR |
Landing gear is not down and locked. |
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DEICE LVL LO |
De-icing fluid level is low (if installed). |
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DEIC PRES HI |
De-icing pressure is high (if installed). |
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DEIC PRES LO |
De-icing pressure is low (if installed). |
Color and Significance of the Advisory Alerts on the G1000 |
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Advisory alerts |
Meaning / Cause |
(white) |
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L/R GLOW ON |
Left / Right engine glow plug active. |
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L/R AUXPUMP |
Fuel transfer from auxiliary to main tank is in progress (if |
ON |
installed). |
PFD FAN FAIL |
Cooling fan for the PFD is inoperative. |
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MFD FAN FAIL |
Cooling fan for the MFD is inoperative. |
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GIA FAN FAIL |
Cooling fan for the GIAs is inoperative. |
2.6.2 OTHER WARNING ALERTS
Warning Alerts on the Instrument Panel
Warning alert |
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Meaning / Cause |
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(red) |
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GEAR UNSAFE |
Illuminates if the landing gear is neither in the final up nor in |
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WARNING LIGHT |
the down & locked position. |
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Doc. No. 7.01.15-E |
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Rev. 1 |
18-Feb-2009 |
EASA |
Page 2 - 15 |
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approved |
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