Piper SENECA III - Page 281

PIPER
AIRCRAFT
CORPORATION
SECTION
9
PA-34-220T,
SENECA
111
SUPPLEMENT
5
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
173
KlAS.
(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
Mode
selected)
(g)
Autopilot
attitude
command
limits:
Pitch
±15°
Roll
+25°
NOTE
In
accordance
with FAA
recommendations,
use
of
"Altitude
Hold"
mode
is
not
recom-
mended
during
operation
in
severe
turbulence.
(h)
Placards:
I..,ocation
-
Pilot's
control
wheel,
left
horn:
AP
TRIM
DISC
lNTERRUPT
-
Pilot's
control wheel,
left
horn:
CWS
-
Pilot's
control
wheel
left horn:
TRIM
UP DN
ISSUED:
APRIL
21,
1981
REPORT:
VB-1110
REVISED:
FEBRUARY 25,
1982
3 of 16,
9-35