Piper SENECA III User Manual

SECTION
6
PIPER
AIRCRAFT CORPORATION
WEIGHT
AND
BALANCE
PA-34-220T, SENECA III
MODEL
PA-34-220T
SENECA
III
Airplane
Serial Number
Registration
Number
Date
AlRPLANE BASIC
EMPTY
WEIGHT
C.G.
Arm
Weight
x
(Inches Aft
=
Moment
ltem
(Lbs.)
of
Datum) (In-Lbs.)
Actual
Standard
Empty
Weight*
Computed
Optional
Equipment
Basic Empty
Weight
*The
standard
empty
weight
includes
full
oil
capacity
and
5.0
gallons
of
unusable
fuel.
AlRPLANE USEFUL
LOAD
-
NORMAL
CATEGORY OPERATlON
(Ramp
Weight)**
-
(Basic Empty
Weight)
=
Useful
Load
(4773
lbs.)
-
(
lbs.)
=
lbs.
THIS
BASIC
EMPTY WEIGHT,
C.G. AND
USEFUL
LOAD
ARE
FOR
THE
AIRPLANE AS
LlCENSED AT
THE FACTORY.
REFER
TO
THE
APPROPRIATE
AIRCRAFT
RECORD WHEN
ALTER-
ATIONS
HAVE
BEEN MADE.
**Includes
fuel allowances
for
start-up,
taxi and
run-up
(23
lbs.)
WEIGHT
AND
BALANCE
DATA
FORM
Figure 6-5
REPORT:
VB-IH0
ISSUED: JANUARY 8, 1981
6-6
REVISED: FEBRUARY 25, 1982

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