DA 62 AFM
Emergency
Procedures
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
precautionary landing on the nearest suitable airfield. Prepare
for an engine failure in accordance with 3.7.6 - ENGINE
FAILURES IN FLIGHT.
END OF CHECKLIST
Doc. No. 11.01.05-E
Rev. 0
11-Jan-2019
Page 3 - 11
Summary of Contents for DA 62
Page 2: ...DA 62 AFM Introduction Intentionally left blank Page 0 0a Rev 0 11 Jan 2019 Doc 11 01 05 E ...
Page 36: ...DA 62 AFM General 1 7 THREE VIEW DRAWING Doc No 11 01 05 E Rev 0 11 Jan 2019 Page 1 19 ...
Page 363: ...Performance DA 62 AFM Intentionally left blank Page 5 92 Rev 0 11 Jan 2019 Doc No 11 01 05 E ...
Page 438: ...Airplane Description DA 62 AFM Page 7 46 Rev 0 11 Jan 2019 Doc No 11 01 05 E ...
Page 496: ...Handling Care Maintenance DA 62 AFM Page 8 10 Rev 0 11 Jan 2019 Doc No 11 01 05 E 1 4 5 2 3 ...