Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION
SECTION
9
PA-34-220T,
SENECA IH
SUPPLEMENT
19
PILOT'S
OPERATING HANDBOOK
AND
FAA
APPROVED AIRPLANE FLIGHT MANUAL
SUPPLEMENT NO. 19
FOR
BENDIX
RDR-160XD/IN-232A
WEATHER
RADAR SYSTEM
SECTION I
-
GENERAL
This
supplement
supplies
information
necessary
for
the
operation of
the
airplane
when
the
optional
Bendix
RDR-160XD/IN-232A
Weather Radar
System
is
installed
in
accordance
with
"FAA
Approved"
Piper
data. The
information
contained within this supplement
is
to
be used
in
conjunction
with
the
complete
handbook.
This
supplement
has been "FAA Approved"
and
must
remain
in this
handbook
at
all
times
when
the
optional
Bendix
RDR-160XD
IN-232A
Weather
Radar System
is installed.
FAA
APPROVED
DAC
o
ser
WARD
EVANS
D.O.A. NO,
SO-I
PlPER
AIRCRAFT CORPORATION
VERO BEACH, FLORIDA
ISSUED:
FEBRUARY
25,
1982
REPORT:
VB-1110
1
of
6, 9-125

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