DA 40 NG AFM
Emergency
Procedures
%3.2.3 OIL PRESSURE
%Engine oil pressure is in the lower red range (too low / below 0.9 bar).
%Oil pressures below the limit value of 0.9 bar can lead to a total loss of power due to engine failure.
-Reduce power.
-Expect loss of oil.
WARNING
Land at the nearest suitable airfield. Prepare for an engine failure in accordance with 3.3.4 - ENGINE FAILURE IN
FLIGHT.
END OF CHECKLIST
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
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Emergency
DA 40 NG AFM
Procedures
%3.2.4 GEARBOX TEMPERATURE
%Engine gearbox temperature is in the upper red range (too high / above 120 °C).
Gearbox temperatures above the limit value of 120 °C can lead to a total loss of power due to engine failure.
-Reduce power.
-Increase airspeed.
CAUTION
At high ambient temperature conditions and/or at low airspeeds with high power settings, it can be assumed that there is no technical defect in the gearbox and that the above mentioned procedure will decrease the temperature(s). This might not be the case if the gearbox temperature does not return to the green range. In this case perform a precautionary landing on the nearest suitable airfield. Prepare for an engine failure in accordance with 3.3.4 - ENGINE FAILURE IN FLIGHT.
END OF CHECKLIST
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Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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DA 40 NG AFM
Emergency
Procedures
%3.2.5 L/R FUEL TEMPERATURE
%Fuel temperature is in the upper red range (too high / above 60 °C).
Fuel temperatures above the limit value of 60 °C can lead to a noticeable reduction of the high pressure pump efficiency.
-Reduce power.
-Increase airspeed.
CAUTION
At high ambient temperature conditions and/or at low airspeeds with high power settings and low fuel quantities, it can be assumed that the above mentioned procedure will decrease the temperature(s). If the fuel temperature does not return to the green range, perform a precautionary landing on the nearest suitable airfield.
NOTE
Increased fuel temperature can occur when the fuel quantity in the main tank is low. The fuel temperature can be decreased by transferring fuel from the auxiliary to the main tank.
END OF CHECKLIST
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 3 - 11 |
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Emergency
DA 40 NG AFM
Procedures
%3.2.6 FUEL PRESSURE
%Engine fuel pressure is low.
1. |
Fuel quantity . . . . . . . . . . . . . . . . . . . . . . . . . |
check |
2. |
Fuel valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
check ON |
3. |
Fuel pumps . . . . . . . . . . . . . . . . . . . . . . . . . . |
ON |
%If FUEL PRESS (if G1000 is installed) or FUELPRESS (if SED is installed) Warning
Remains:
4. Fuel valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . EMERGENCY 5. Fuel pumps . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
%If FUEL PRESS (if G1000 is installed) or FUELPRESS (if SED is installed) Warning Still
Remains:
WARNING
Imminent engine failure must be expected. Prepare for an engine failure in accordance with 3.3.4 - ENGINE FAILURE
IN FLIGHT.
END OF CHECKLIST
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Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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