DA 42 AFM
Airplane Description
Doc. No. 7.01.05-E
Rev. 8
15-Dec-2017
Page 7 - 49
7.9.6 COOLING SYSTEM
Each engine is liquid cooled. The liquid cooling system consists of a radiator and a bypass
to this radiator. The bypass is in operation when coolant temperatures are low. It therefore
allows the engine to warm-up quickly. Upon reaching a certain temperature (approximately
88 °C or 190 °F) the radiator is activated by a thermostat valve. Additionally a coolant
to air heat exchanger is provided for the cabin heat system. The flow through the heat
exchanger is independent of the coolant temperature. An expansion tank helps to adjust
the pressure in the system. The system is protected against over pressure by means of
a pressure relief valve.
Summary of Contents for DA 42
Page 1: ......
Page 20: ...Introduction DA 42 AFM Page 0 18 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 46: ...General DA 42 AFM Page 1 26 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 236: ...Performance DA 42 AFM Page 5 4 Rev 8 15 Dec 2017 Doc No 7 01 05 E ...
Page 237: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 5 ...
Page 247: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 15 ...
Page 251: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 19 ...
Page 257: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 25 ...
Page 268: ...Performance DA 42 AFM Page 5 36 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 277: ...DA 42 AFM Mass and Balance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 6 9 6 4 2 LOADING DIAGRAM ...
Page 390: ...Handling Care Maintenance DA 42 AFM Page 8 12 Rev 8 15 Dec 2017 Doc No 7 01 05 E ...