Piper SENECA III User Manual

PIPER
AIRCRAFT CORPORATION
SECTION
9
PA-34-220T,
SENECA
III SUPPLEMENT 21
PILOT'S
OPERATING
HANDBOOK
AND
FAA
APPROVED
AIRPLANE
FLIGHT
MANUAL
SUPPLEMENT
NO. 21
FOR
CENTURY 31
AUTOPILOT
MODEL AKB95
This
supplement
must
be
attached
to
the
Pilot's
Operating
Handbook
and
FAA
Approved
Airplane Flight
Manualwhenthe
Century3I
Autopilot
System
Model
AKN95
is
installed
in
accordance with
STC
SA3390SW-D.
The
information
contained
herein
supplements
or
supersedes
the
infor-
mation
in
the
basic
Pilot's
Operating
Handbook
and
FAA
Approved
Airplane
Flight
Manual
only
in
those
areas
listed herein.
For
limitations.
procedures
and
performance
information
not
contained
in
this
supplement,
consult
the
basic Pilot's Operating
Handbook
and
FAA
Approved
Airplane
Flight
ManuaL
FAA
APPROVED
WARD
EVANS
D.O.A.
NO.
SO-I
PIPER
AIRCRAFT CORPORATION
VERO BEACH,
FLORIDA
DATE
OF
APPROVAI
Februarv
10,
1984
ISSUED:
FEBRUARY 10,
1984 REPORT:
VB-Ill0
1
of
20,
9-135
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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