Piper Arrow PA-28R-201 Pilot Operating Handbook page 155

ARROW
PA-28R-201,
6.3 AIRPLANE
WEIGHING
(2) The basic empty
including optional equipment,
can be detenitined by the following formula:
C.GArm=N(A)+(R+L)(B)
6.5 WEIGHT AND
The Basic Empty
listed in Figure 6-5 are for the airplane as licensed at the factory. These
figures apply only to the specific airplane serial number
number shown.
The basic empty
been entered in the Weight
provided to present tile current statusof the airplane basic empty weight and
a complete
history
installed equipment
permanently
must be entered in the Weight and Balance Record.
moment
12, 1995
ISSUED: JULY
HB-PQY, Page: 6-5-(0)
PROCEDURE
weight
T
T=N+R+L
Where:
BALANCE DATA AND
Weight, Center of Gravity Location and Useful Load
weight of the airplane as licensed at the factory has
and Balance
of previous modifications.
or modification which
Issued: JULY 12, 1995
WEIGHT AND
(continued)
center of gravity (as weighed
full oil and unusable fuel)
inches
RECORD
and registration
Record (Figure 6-7). This form is
Any change
affects weight or
REPORT:
6
SECTION
BALANCE
to the
VB-1612
6-5
6-5