Piper Cherokee Six 300 Information Manual page 63

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 .A rm = 7 8 .4 + A -B(N)
T
C. G. Arm = 78.4 + (
)-(
inches
5.
LICENSED EMPTY WEIGHT AND EMPTY WEIGHT CENTER OF GRAVITY
b.
:iri
fti;
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
1 0 3 . 0
+237
Licensed Empty Weight