RAZAIR
‐
A1
‐
METRO
‐
III
‐
AFM
‐
001
1
‐
9
Fig.
15
Trim
Controls.
Fig.
16
Trim
Controls
and
Indicators
Location.
AILERON
(ROLL)
TRIM
The
trim
tab
of
each
aileron
is
connected
to
the
AILERON
TRIM
wheel
(Fig
15
‐
3)
on
the
pedestal.
Left
or
right
clicking
on
the
trim
wheel
positions
both
tabs
for
lateral
trim.
As
the
outer
wheel
rotates,
the
inner
wheel
rotates
in
the
same
direction
at
a
reduced
rate.
The
aileron
trim
tabs
are
in
the
neutral
position
when
the
index
lines
on
both
the
outer
and
inner
wheels
are
aligned
vertically.
RUDDER
(YAW)
TRIM
The
rudder
trim
tab
is
actuated
by
the
RUDDER
TRIM
wheel
(Fig
15
‐
2)
on
the
pedestal.
Left
or
right
clicking
n
the
trim
wheel
positions
the
tab
for
yaw
trim.
ELEVATOR
(PITCH)
TRIM
There
are
no
trim
tabs
on
the
elevators;
pitch
trim
is
accomplished
by
moving
the
entire
horizontal
stabilizer.
On
the
real
aircraft,
pitch
trim
is
controlled
by
two
buttons
located
on
both
control
yokes
(not
modelled).
There
is
an
auxiliary
trim
switch
located
on
the
pedestal
marked
AUX
TRIM.
Left
or
right
clicking
on
this
switch
will
provide
UP
or
DOWN
pitch
trim
(Fig
15
‐
1).
Stabilizer
position
is
displayed
on
a
PITCH
TRIM
indicator
on
the
instrument
panel
(Fig
17).
FLAPS
The
aircraft’s
flaps
are
electrically
controlled
and
hydraulically
actuated.
The
right
and
left
wing
flaps
are
interconnected
to
prevent
asymmetrical
operation.
The
FLAP
lever
(Fig.
19)
on
the
pedestal
is
used
to
preselect
any
flap
position
from
full
up
to
full
down.
The
lever
has
detents
at
the
¼
(Takeoff
position)
and
½
flap
positions.
Flap
position
is
shown
on
the
FLAP
POSition
indicator
(Fig.
19).
Fig.
17
Pitch
Trim
Indicator.
