CHEROKEE
WARRIOR
Obtain measurement
"A"
by measuring
from a
plumb
bob
dropped from
one wing leading edge, at
the intersection
of the straight
and inboard
tapered section, horizontally and
parallel
to the
airplane centerline,
to
the
main wheel centerline.
Obtain measurement
"B"
by measuring
the distance from the main
wheel
centerline,
horizontally
and
parallel
to the airplane centerline,
to each side
of the nose
wheel
axle.
Then average the
measurements.
The empty weight
center
of
gravity
(as
weighed including optional
equipment
and
undrainable
oil) can
be
determined
by
the following
formula:
C.G.Arm
=
78.4+A-B(N)
T
C.
G. Arm
=
78.4
+
(
)-(
)( )-
()
inches
5. LICENSED
EMPTY WEIGHT AND
EMPTY WEIGHT CENTER
OF GRAVITY
b.
d.
Weight Arm Moment
Empty Weight
(as
weighed)
Unusable
Fuel
(2.0
gal.)
t2 tb
103.0
1236
Licensed
Empty Weight
ISSUED:
MAY 14, 1973
REVISED:
JLjNE
14,1974
REPORT:
VB-535
PAGE
5-5
MODEL:
PA-2&lSl
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