a
speed slightly
higher
than
normal,
then pulled
off
abruptly
to
prevent
possible
settling
back
to the
runway while
drifting.
When clear of
the
ground,
make a coordinated
turn into the
wind
to correct for drift.
CLIMB.
CLIMB DATA.
--
---
For
detailed
data,
refer
to
the Maximum
Rate-Of-Climb
Data chart
o
in
Section
V.
CLIMB
SPEEDS.
Normal climbs are performed
at 80 to 90 MPH with flaps
up
and full
throttle
for
best
engine
cooling. The
mixture
should be full rich
below
5000 feet and
may
be leaned
above 5000 feet for smoother engine
opera-
tion. The maximum
rate-of-climb
speeds range
from
82
MPH at
sea
level to 79 MPH at 10,
000
feet.
If
an o.bstacle dictates
the use of a
steep
climb
angle,
the best
angle-of-climb
speed
should be
used with
flaps
up
and
full throttle. These speeds vary
from
68
MPH
at
sea level
to
74
MPH
at
10, 000
feet.
NOTE
o
Steep
climbs
at these
low
speeds
should
be
of
short
duration to improve
engine
cooling.
2
5
- - --- - --
-
CRUISE.
- --
O
coo
coo coo
Normal
cruising
is
done
between
65% and 75% power.
The
power
Ë
$
settings
required to obtain
these
powers
at various altitudes
and outside
---- ---
---- ----
5
air temperatures can be
determined
by using
your Cessna
Power
Com-
o
puter
or
the
OPERATIONAL
DATA,
Section
V.
Cruising
can be done more efficiently
at
high
altitudes
because of
lower
air
density
and
therefore higher
true airspeeds for
the
same
power.
ogg
"
"
ËR
This is
illustrated
in the following
table
which
shows performance at
75%
power
at various altitudes.
All
figures are based
on lean
mixture, 38 gallons of fuel (no
re-
serve),
zero
wind,
standard
atmospheric
conditions,
and
2300 pounds
gross
weight.
2-10
5-3
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