i
I
I
t,
A-
S=
CHEROKEE SD(.300
3.
WEIGHING. AIRPLANE EMPry WETGHT
a'
lVith the ailplane level and brakes released, record the weight shown on
each scale. Deduct the tare, if any, from each reading.
4.
EMPTY WEIGHT CENTER OF GRAVITY
a.
The following geometry applies to the PA-32-300 airplane when airplane is
level (See Item 2).
24il
i illl
{t
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-,-q6r.
Level Points
(Fuselage Left Side)
Wing Leading Edge
R+ L
The datum is 78.4 inches ahead
of the wing leading edge at the
intersection of the straight and
tapered section.
REFORT: VB-551 PAGE 5,f
MODEL: PA-32-3O0
Scale Position and Symbol
Nose \Yheel
(N)
Right'Main.Wheel
(R)"
Left Main Wheel
(L)
Airplane Empty Weight, as Weighed (T)
ISSUED: II{AY 14, 1973