Piper CHEROKEE ARCHER II Pilot Operating Handbook page 116

PIPER
AIRCRAFT
C
ORPO
RATION
PA.28.18I, CIIEROKEE ARCHER
II
SECTION
7
DESC
RITTTON A"\iD
OPE
RATION
FUGHT CONIROL
CONSOLE
Figure
7-3
7.9
FLIGTIT CONTROLS
Dual controls are provided
as
standard equipment,
with
a
cable system used
between the controls
and
the
surfaces. The
horizontal tail (stabilator) is of
the all-movable
slab
type
with
a
trim tab mounted on
the
trailing
edge
of
the stabilator
to
reduce the control system forces. This tab is actuated by
a
control wheel
on the
floor
between the
front
seats
(Figurc 7-3).
A
rudder
trim
adjustment
is
mounted on the rieht
side
of the
pedestal below the
throttle quadrant
and
permits directional
trim
as
needed
in
fii$t
(refer to
Figure 7-5).
The flaps are manually operated and
sprindoaded to return
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.
The flap
will
not support
a step
load except when in the
full
up position,
so
it
must
be
completely retracted when used as
a
step. The flaps have three extended positions,
10,25
and 40
degrees.
REBORT: VB-790
7_5
ISILJED:
JLJNE
lt,
1976