Specifications

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I
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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
#'
-,-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