be necessary
to
retain adequate power. Power changes should be made
cautiously followed
by
prompt adjustment
of
the mixture for smoothest
operation.
ST
ALLS.
The
stall
characteristics
are
conventional and aural warning is
pro-
vided by a
stall
warning horn which sounds between 5 and
10
MPH
above
the
stall
in all configurations.
Power-off
stall
speeds
at
maximum
gross
weight and aft
c.
g.
posi-
tion
are
presented
on
page 6-2
as
calibrated
air~peeds
since indicated
airspeeds
are
unreliable near the stall'. ·.
._
·
SPINS.
Intentional spins
are
approved in this
aircraft
in the Utility Category
only. Although this
aircraft
is inherently resistant
to
sf)ins, the follow-
ing techniques may be used to perform intentional spins
for
training
or
-practice. To obtain a clean
entry~
decelerate the
aircraft
at
a
faster
·
rate
than
is
used for stalls. Then, just
as
. the ,stall occurs, apply full
up
ele-
vator, full rudder in the desired spin. direetion, and momentarily use full
engine power. As the
aircraft
begins to spin, · reduce the power to idle
and maintain full
pro-
spin elevator and rudder deflections. The applica-
tion ·
of
ailerons-in the direction
of
the desired ·spin may
also
~
help
obtain
a clean entry.
During extended spins
~f
two
to
thr~
.
e
turns.
9r
more,
th~
spin will
tend
to
change into a spiral, particula'rly to the right.. This_ will
be
ac.;.
companied by an increase in airspeed and gravity loads .
on
the
aircraft.
U this occurs, recovery should
be
accomplished quickly
by
leveling the
wings and recovering from the resulting dive.
To
recover from an intentional
or
inadvertent spin,
~se
the f9llowing
procedure: · ·
(1)
Retard throttle to idle position.·
(2) Apply full rudder opposite to·the direction
of
rotation. ..
(3)
After one-fourth turn,
move
the control wheel forward
of
neutral
in a
brisk
motion.
2-17
:·
..
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