Piper SENECA III - Page 265

PIPER
AIRCRAFT
CORPORATION
SECTION
9
PA-34-220T,
SENECA
Ill
SUPPLEMENT
4
SECTION 2
-
LIMITATIONS
(a)
During
autopilot operation,
pilot
must
be
seated
at
the
controls
with
seat
belt
fastened.
Operation is
restricted
to
left side
pilot
position.
(b)
Maximum
speed
for
autopilot
operation
is
200
KIAS.
(c)
The
maximum
altitude
for
operation
of
the
autopilot
has
not
been
determined. The
maximum
altitude
flight
tested
was
24,000 feet.
(d)
Do
not
extend
flaps
beyond
25° during
autopilot
operation.
(e)
The
autopilot
must
be
disengaged
during
takeoff
and
landing.
(f)
System
approved
for
Category
I
operation
only
(APPR
or
BC
selected).
(g)
Autopilot
attitude
command
limits:
Pitch
±15°
R011
±25°
NOTE
In
accordance
with
FAA
recommendations,
use
of
"Altitude
Hold"
mode
is
not
recom-
mended
during
operation
in
severe
turbulence.
(h)
Placards:
Location
-
Pilot's
control wheel,
left
horn:
AP
TRIM
DISC
INTERRUPT
-
Pilot's
control wheel,
left
horn:
CWS
-
Pilot's
control
wheel,
left
horn:
TRIM
UP/DN
-
Left throttle lever:
GO AROUND
ISSUED:
APRIL 21,
1981
REPORT:
VB-1110
3
of 16,
9-21