Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION
SECTION 9
PA-34-220T,
SENECA
III SUPPLEMENT 14
PILOT'S
OPERATING
HANDBOOK
AND
FAA
APPROVED AIRPLANE FLIGHT MANUAL
SUPPLEMENT NO.
14
FOR
BENDIX
RDR-160
MONOCHROME WEATHER
RADAR
SYSTEM
SECTION I
-
GENERAL
This supplement
supplies
information
necessary
for the operation ofthe
airplane when the
optional
Bendix
RDR-I60
Monochrome
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-160 Monochrome
Weather Radar
System
is installed.
FAA
APPROVED
WARD
EVANS
D.O.A. NO. SO-l
PlPER
AIRCRAFT
CORPORATION
VERO BEACH,
FLORIDA
ISSUED:
JANUARY
8,
1981
REPORT:
VB-1110
1 of 6, 9-91

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