CF 300 – Flight Manual sect. 1 - General
BY BLACKSHAPE
Rev 3 dtd 03/06/2014 Page 9
1.12.2 Flight Performance and Flight Planning
DEMONSTRATED Crosswind component
The maximum speed of the crosswind component
at
which the maneuverability of the airplane
during
take-off and landing has been
effectively
demonstrated during test flights.
The altitude at which the maximum rate of climb is
0.5 m/s (100 ft/min).
1.12.3. Powerplant
of revolutions per minute:
the number of engine
revolutions per minute
, divide by 2.4286 (912 ULS3)
to obtain the
number of propeller revolutions per minute.
The lever which controls the engine power
, and
therefore the
manifold absolute
pressure (MAP).
Regulation of the propeller pitch setting:
this is a control
lever
that allows to set the propeller pitch
, and as a consequence
.
Indicates the number of revolutions per minute of the engine.
The instrument is connected directly to the engine via a flexible
hose.
Cylinder Head Temp. (CHT)
Indicates the head temperature of the cylinder
n° 3.
Indicates the temperature of the gas that are expelled directly
from the cylinders.
Manifold pressure display
:
Indicates the engine absolute
manifold pressure.
Indicates the battery load
Indicates the cooling water temperature
temperature