Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION SECTION
9
PA-34-220T,
SENECA
III
SUPPLEMENT
4
PlLOT'S
OPERATING HANDBOOK
AND
FAA
APPROVED
AIRPLANE FLIGHT
MANUAL
SUPPLEMENT NO. 4
FOR
KFC
200
AUTOMATIC
FLIGHT CONTROL
SYSTEM
(WITH
FLIGHT
DIRECTOR INSTALLATION)
PIPER
DWG.
36840
SECTION I
-
GENERAL
This
supplement
is
to
acquaint the
pilot
with the operation of
the
KFC 200
Automatic
Flight Control System
with optional
Flight Director
as
installed
in
the
PA-34-220T Seneca III
in
accordance
with
"FAA
Approved"
Piper
data.
The
airplane
must
be
operated within the limitations
herein
specified.
This
supplement has
been "FAA
Approved"
based
on
King
STC
SA I
147CE
and
must
remain
in
this
handbook
at
all
times
when the
optional
King
KFC 200
Automatic Flight Control System
is installed.
FAA
APPROVFD
WARD EVANS
D.O.A.
NO.
SO-l
PIPER
AIRCRAFT
CORPORATION
VERO
BEACH,
FLORIDA
ISSUED:
APRIL 21, 1981 REPORT:
VB-1110
1 of 16, 9-19

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