Specifications

CHEROKEE
SIx.3OO
Console
FUGHT
CONTROLS
Dual controls, with a cable system
between
the controls
and
the
surfaces,
are
installed
as
standard
equipment.
The horizontal tail is
of
the
all-movable
slab type
(stabilator).
The stabilator
provides
extra
stability and
controllability
with less
size,
drag, and weight
than
conventional tail surfaces.
An
anti-servo tab which also acts
as
a
longitudinal
trim
tab, is
located on
the horizontal
tail.
This tail is actuated by a
control
mounted
on the control tunnel
between
the
front seats.
The
ailerons
are
provided
with a differential action
which tends to eliminate
adverse
yaw
in
turning maneuver and
to
reduce
the amount of coordination required
in normal furns.
The flaps are manually
operated,
balanced
for light
operating forces,
and spring-loaded
to
retum
to
the
up
position.
A
past-center
lock
incorporated in
the
actuating
linkage
holds the
flap
when it is
in the up
position
so that
it
may be used as a
step on the
right side. Since
the
flap
will
not support a
step load
except
in
the
full
up
position,
it should
be
completely retracted
when
the
airplane is
on the
ground.
The flaps
have
three
extended
positions,
10, 25, and
40
degrees.
AIRPI.AI{E AI{D SYSTEMS
ISSUED:
JULY
12. 1973
24