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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
3.5.6 - ENGINE FAILURES IN FLIGHT.
END OF CHECKLIST
Page 3 - 8 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
3.2.4 L/R OIL PRES
L/R OIL PRES Left / Right engine oil pressure is in the lower red range (too low / below 1 bar).
Oil pressures below the limit value of 1 bar can lead to a total loss of power due to engine failure.
-Reduce power on affected engine.
-Expect loss of oil.
WARNING
Land at the nearest suitable airfield. Prepare for an engine failure in accordance with 3.5.6 - ENGINE FAILURES IN FLIGHT.
END OF CHECKLIST
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 3 - 9
3.2.5 L/R GBOX TEMP
L/R GBOX TEMP Left / Right 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 on affected engine.
-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 precaution-ary landing on the nearest suitable airfield. Prepare for an engine failure in accordance with 3.5.6 - ENGINE FAILURES IN FLIGHT.
END OF CHECKLIST
Page 3 - 10 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
3.2.6 L/R FUEL TEMP
L/R FUEL TEMP Left / Right fuel temperature is in the upper red range (too high / above 75 °C).
Fuel temperatures above the limit value of 75 °C can lead to a noticeable reduction of the high pressure pump efficiency.
-Reduce power on affected engine.
-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. If the auxiliary tank is installed the fuel temperature can be decreased by transferring fuel from the auxiliary to the main tank.
END OF CHECKLIST
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 3 - 11
3.2.7 L/R ALTN AMPS
L/R ALTN AMPS Left / Right engine alternator output is in the upper red range (too high / above 60 amps).
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