Piper SENECA III User Manual

SECTION
9
PIPER
AIRCRAFT
CORPORATION
SUPPLEMENT 21
PA-34-220T,
SENECA
III
(b)
REMOTE
CONTROI.
SWEICHES
AUTOPILOT
CONTROL
WHEEL
SWITCH CAP
Figure
7-3
(
I)
Control
Wheel
Trim
Switch
-
Dual
action
type
switch
requiring
the
top
bar
to
be
depressed
and
the
rocker
to
be
moved
fore
or
aft
to
cause
the
electric
trim
io
function from
the
control
wheel
switch.
Depressing
the
center
bar
will
disconnect
the
autopilot.
(2)
Control
Wheel
Steeting
(CWS)
Switch
See
explanation
in
Special
Modes
and
Operations
Section,
(3)
Master
Disconnect
Trim
laterrupt
Switch
-
Pressing
this
switch
will
disconnect
autopilot
and
interrupt
manual
electric
trim
while
held
depressed.
Trim
operation will
resume
when
the
switch
is
released.
REPORT:
VB-111.0
ISSUED:
FEBRUARY
1.0,
1984
9-150,
16
of 20

Piper SENECA III Specifications

General

Manufacturer	Piper Aircraft
Model	Seneca III
Engine Type	Piston
Engine Model	Continental TSIO-360-KB
Seating Capacity	6
Cruise Speed	188 knots (216 mph, 348 km/h)
Length	28 ft 7 in (8.71 m)
Max Takeoff Weight	4, 750 lb (2, 155 kg)
Horsepower	220 hp each
Service Ceiling	25, 000 ft (7, 620 m)
Height	9 ft 11 in (3.02 m)
Propellers	2-bladed constant speed