Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION
SECTION
9
PA-34-220T,
SENECA III
SUPPLEMENT
I
PILOT'S
OPERATING
HANDBOOK
AND
FAA
APPROVED
AIRPLANE
FLIGHT
MANUAL
SUPPLEMENT
NO. I
FOR
PORTABLE
OXYGEN
SYSTEM
INSTALLATION-
SCOTT
AVIATION PRODUCTS
EXECUTIVE
MARK
III
PART
NUMBER 802180-00 OR
802180-01
SECTION 1
-
GENERAL
This
supplement
supplies
information
necessary
for
the
operation of
the
airplane
when
the
optional
portable
oxygen
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
portable
oxygen
system
is installed.
FAA
APPROVFD
WARD
EVANS
D.O.A.
NO.
SO-1
PIPER
AlRCRAFT CORPORATION
VERO
BEACH,
FLORIDA
ISSUED:
JANUARY 8,
1981
REPORT:
VB-IllO
1 of 6, 9-3

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