Specifications

CHEROKEE
SD(.300
Obtain
measurement "A"
by
measuring
from a
plumb
bob dropped
from
the
wing leading
edge,
at the intersection of
the straieht
and
tapered
section,
horizontally
and
parallel
to
the airplane centerline,
to
the main
wheel
centerline.
Obtain
measurement
'oB"
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.
d.
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.
:iri;i
fti;1
ISSLJED:
MAY
14,1973
REVISED:
NOVEMBER
6. 1974
REPTORT:
VB-551
PAGE 5-5
MODEL: PA-32.30O
Weight
Arm
Moment
Empty Weight
(as
weighed)
Unusable Fuel
(.4 gallon)
+2.3
103.0
+237
Licensed
Empty Weight