Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION
SECTION 6
PA-34-220T,
SENECA
III
WEIGHT
AND
BALANCE
6.5
WEIGHT
AND
BALANCE
DATA
AND RECORD
The
Basic
Empty
Weight, Center
of
Gravity
Location
and
Useful
Load
listed
in
Figure
6-5
are
for
the
airplane
as
licensed
at
the
factory. These
figures
apply
only
to
the
specific
airplane
serial number and
registration
number
shown.
The
basic
empty
weight
of the
airplane
as
licensed
at
the
factory
has
been
entered
in
the
Weight and Balance
Record
(Figure
6-7).
This form is
provided
to
present
the
current
status
of
the
airplane
basic
empty
weight
and
a
complete
history
of
previous
modifications.
Any
change
to
the
perma-
nently
installed
equipment
or
modification which
affects
weight
or
moment
must
be
entered
in
the
Weight and Balance
Record.
ISSUED:
JANUARY
8,
1981
REPORT: VB-1110
REVISED:
AUGUST
9,
1982
6-5

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