Piper SENECA III - Page 386

SECTION
9
PIPER
AIRCRAFT
CORPORATION
SUPPLEMENT
21
PA-34-220T, SENECA
III
SECTION 1
-
GENERAI
This
supplement
supplies information
necessary
for
the
operation
of the
airplane
when
the
optional
Century 31
Autopilot
Model
AKS95
is
installed
in
accordance
with
"FAA
Approved"
Piper
dant.
SECTION 2
-
LIMITATIONS
(a)
Autopilot
OFF
during
takeofT
and
landing.
(b)
Maximum
airspeed
for
autopilot
operation
is 180 KIAS:
(c)
Autopilot
operation
prohibited
with
more
than
2
notches
(25°)
flaps
extended.
(d)
Autopilot
coupled
single-engine
approaches
to
be
conducted
at
90
KIAS
or
faster.
with
flaps
up.
(e)
Category
1
operations
orily.
(f)
Placard
-
in full
view
of
the
pilot:
CONDUCT
TRlM
CHECK
PRIOR
TO
FIRST
FLIGHT
OF
DAY
(SEE
AFM).
SECTION 3
-
EMERGENCY
PROCEDURES
(a)
AL'TOPlLOT
In
the
event
of
an
autopilot
malfunction,
or
anylime
the
autopilot
is
not
performing
as
commanded,
do
not
attempt to
identify
the
problem
system,
Regain
control
of the
aircraft
by
overpowering
and
immediately
disconnecting
the
autopilot.
Be
prepared for
any
residual
trim
force
and
retrim,
as
necessary,
using the
aircraft's
primary
trim
control.
CAUT/ON
Do
not
overpower
autopilot
in
pitch
for
more
than
approximately
3
seconds
as
the
autotrim
system
will
cause an
increase
in
pitch
over-
power
forces.
REPORT:
VB-Ill0
ISSUED:FEBRUARY 10,
1984
9-136,
2
of
20