Piper CHEROKEE ARCHER II Pilot Operating Handbook page 101

PIPER AIRCRAFT CORPORATION
PA-28
I8I,
CHEROKEE ARCHER
II
SECTION 6
WEIGHT AND BALANCE
(l)
-I'lte
basic
e
mpty weight centcr of
gravity (as
weighed including optionalequipment, full oil
and unr.rsable
f'uel)
can
be
determined by the following formula:
C.Ci.
Arrn
=
N(A)_+_(R +
L)(B)
inches
1'
Where:
-['= N+R+L
ISSUED:
JUNE 18,
1976
REYISED:
JANUARY 20,
1977
REPORT:
V&790
6-5