DA 40 NG AFM
General
Doc. # 6.01.15-E
Rev. 3
01-Jul-2014
Page 1 - 11
Moment Arm:
The horizontal distance from the Datum Plane to the Center of Gravity of a
component.
Moment: The mass of a component multiplied by its moment arm.
Usable Fuel:
The quantity of fuel available for flight planning.
Unusable Fuel:
The quantity of fuel remaining in the tank which cannot be used for flight.
Useful Load:
The difference between take-off mass and empty mass.
(e) Engine
CT:
Coolant Temperature.
EECU:
Electronic Engine Control Unit.
GT:
Gearbox Temperature.
LOAD:
Engine output power in percent of take-off power.
MED:
Main Engine Display.
OP:
Oil Pressure (oil pressure in the lubrication system of the engine).
OT:
Oil Temperature (oil temperature in the lubrication system of the engine).
RPM:
Revolutions per minute (rotational speed of the propeller).
SED:
Secondary Engine Display.
FT:
Fuel Temperature.
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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 287: ...DA 40 NG AFM Airplane Description Doc 6 01 15 E Rev 3 01 Jul 2014 Page 7 27 7 9 4 FUEL SYSTEM Standard Tank Schematic...
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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