Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION
SECTION
9
PA-34-220T,
SENECA
III
SUPPLEMENT
3
PILOT'S
OPERATING
HANDBOOK
AND
FAA
APPROVED
AIRPLANE FLIGHT
MANUAL
SUPPLEMENT NO. 3
FOR
AIR
CONDITIONING
INSTALLATION
PIPER
DWG. 36809
SECTION
I
-
GENERAL
This supplement
supplies
information
necessary
for
the
operation
of
the
airplane
when
the
optional
air
conditioning
system
is installed in
accor-
dance
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
air conditioning
system
is
installed.
FAA
APPROVFD
WARD
EVANS
D.O.A.
NO.
SO-!
PIPER
AIRCRAFT
CORPORATlON
VERO
BEACH,
FLORIDA
ISSUED:
JANUARY 8,
1981
REPORT:
VB-1110
I
of 6,
9-13

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