Piper SENECA III - Page 392

SECTION
9
PIPER
AIRCRAFT
CORPORATION
SUPPLEMENT
21
PA-34-220T,
SENECA
III
(3) Instrument
Approach
Go-Around
Maneuver
a.
Disconnect
the autopilot
and
manually
control the
aircraft.
b.
Add
takeoff
power,
or
power
as
desired.
c.
Check
that
correct
attitude and
a
positive
rate
of
climb
is
indicated,
then
raise
gear
and
flaps.
d. Set
the
heading bug
to
the
desired
missed
approach
heading,
e.
Re-engage
the
autopilot.
SECTION
5
-
PERFORMANCE
No
change.
SECTION
6
-
WEIGHT
AND
BALANCE
Factory
installed
optional
equipment
is included
in
the
licensed
weight
and
balance
data
in
Section 6
of
the
basic
Pilot's
Operating Handbook.
SECTION
7
-
DESCRIPTION
AND
OPERATION
The
Century
31
Autopilot
is
a
light
weight
electronic
autopilot
system
utilizing
vertical
and
directional
gyro
signals
and
D.C.
electric
servos
to
provide
three
axis
sensing
and
two
surface
control.
The
system
includes
lateral
and
vertical
radio
coupling.
command
and
automatic
elevator
trim:
and
navigation
and
autopilot
failure
monitor
and
warning
systems.
REPORTi
VB-1HO
ISSUED:
FEBRUARY
10,
1984
| 9-142,
8
of
20