Weight And Balance Data And Record - Piper Turbo Saratoga PA-32-301T Pilot's Manual

PIPER AIRCRAFT CORPORATION SECTION
6
PA-32-30lT, TURBO
SARATOGA WEIGHT
AND BALANCE
(2)
The basic empty
weight
center
of gravity
(as
weighed
including
optional equipment, full oil and unusable
fuel)
can be determined by
the
following formula:
C.G. Arm
=
N (A)
+
(R
+
L) (B) inches
T
Where: T=N+R+L
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
permanently
installed
equipment
or modification which
affects
weight
or
moment must
be
entered
in the Weight
and Balance Record.
ISSUED: JANUARY 10, 1980
REPORT: VB-1070
REVISED: AUGUST 6, 1982
6-5