Piper SENECA III User Manual

SECTION
9
PIPER
AIRCRAFT CORPORATION
SUPPLEMENT
14
PA-34-220T,
SENECA III
SECTION 2
-
LIMITATIONS
Do
not
operate
the
radar
during
refueling
operations
or
in
the
vicinity
of
trucks
or
containers
accommodating
flammables
or
explosives.
Do
not
allow
personnel
within
15feet
of
area
being
scanned by
antenna
when
system
is
transmitting.
SECTION
3
-
EMERGENCY
PROCEDURES
No
changes
to
the
basic Emergency
Procedures
provided
by
Section
3
of
this Pilot's
Operating
Handbook
are
necessary
for this
supplement.
SECTION 4
-
NORMAL
PROCEDURES
(a)
SYSTEM
CONTROLS
Table
4-3
lists
and
describes the
system
controls,
all
of
which
are
mounted
on
the panel
of
the
radar
indicator. Figure 4-1
illustrates
the
location
of
these
controls.
Table
4-5
lists
the
alphanumeric
read-
outs
of
range
-
range
marks
and
mode
selection
as a
function
of
switch
position.
ALPHANUMEMC
/
ON-SCHEEN
READOUT
RANGE MARK
SELECTED
HOLD
SELECTED
MODE
BPACING
N.M.
HANGE N.M
RANGE
SELECTOR
PUSHBUTTOW
MODE
SELECTOA
T ST
AND
GAtN
CONTROL
TILT
CONTOOL
o
BR1GHTNESS
comnot
LOCATION
OF
CONTROLS
Figure
4-1
REPORT: VB-1110
ISSUED:
JANUARY
8,
1981
9-92,
2
of
6

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