DA 40 NG AFM
Airplane
Description
Doc. # 6.01.15-E
Rev. 3
01-Jul-2014
Page 7 - 21
7.9
POWER PLANT
7.9.1 ENGINE, GENERAL
The installed Austro Engine E4-A engine has the following specifications:
-
Liquid-cooled four-cylinder four-stroke engine with wet sump lubrication
-
Inline construction
-
Common rail direct injection
-
Propeller speed reducing gear 1:1.69
-
Digital engine control with integrated propeller governor (using the gearbox oil
system)
-
Turbo charger with intercooler
Displacement:
Max. power:
123.5 kW (165.6 DIN-HP) at 2300 RPM
at sea level and ISA
Max. continuous power: 114.0 kW (152.8 DIN-HP) at 2100 RPM
at sea level and ISA
The indications for monitoring important engine parameters during operation are integrated
within the Garmin G1000 display (if installed) or on the MED and SED (if installed). The
engine can only be operated with the ENGINE MASTER switch ON. The engine has an
EECU (Electrical Engine Control Unit) which receives its electrical power from the
generator when the engine is running. When the engine is not running, the ECU receives
its electrical power from the battery.
Содержание DA 40 NG
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Страница 240: ...Mass Balance DA 40 NG AFM Page 6 8 Rev 3 01 Jul 2014 Doc 6 01 15 E 6 4 2 LOADING DIAGRAM...
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Страница 288: ...Airplane Description DA 40 NG AFM Page 7 28 Rev 3 01 Jul 2014 Doc 6 01 15 E Long Range Tank Schematic...
Страница 316: ...Handling DA 40 NG AFM Page 8 8 Rev 3 01 Jul 2014 Doc 6 01 15 E...
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