Piper SENECA III - Weight and Balance Data Form

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