Section
VI
BEECHCRAFT
Debonair
C33
Bonanza
E33
and
F33
Wt
and Bal;'Equip List
4.
To
determine airplane
configuration
at
time
of
weighing, installed
equipment
is checked against the
airplane equipment
list
or
superseding forms.
All
installed equipment
must
be
in
its
proper place
during
weighing.
5.
At
the
time
of
weighing,
the airplane
must
be level
both longitudinally and laterally, and the landing gear
must be
fully
extended. Leveling
screws
are located on
the
left side of
the
fuselage at approximately Fuselage
Station
152.25.
longitudinally
level
attitude
is de-
termined
with
a
plumb
bob.
laterally
level attitude is
obtained
when
the
vertical distance
from
each
wing
tip
to the floor is equal.
6.
Measurement
of
the reaction arms
for
a
wheel
weighing
is made using a steel
measuring
tape.
Measurements are
taken,
with
the
airplane level
on
the
scales, from the reference
(a
plumb
bob dropped
from the center of either
main
jack point) to
the
axle
center
line of the
main
gear
and
then
to
the
nose
wheel
axle center line. The
main
wheel
axle
center
line
is
best located by Stretching
a·
String across
from
one
main
wheel
to
the
other.
All
measurements
are
to
be taken
with
the tape level
with
the hangar
floor
and
parallel to the fuselage center line. The locations
of
the
wheel
reactions
will
be approximately at Fuselage
Station 96.7 for
main
wheels
and Fuselage Station
12.7 for the nose
wheel.
7.
Jack point
weighings
are accomplished by placing
6-4
scales
at
the jack
points
specified in step 1 above.
Since the center of gravity
of
the
airplane is
forward
of
Fuselage Station 83.1. the
tail
reaction
of
the
airplane
..-\
will
be in
an
up direction.
This
can be measured
on
regular scales by pfacing baHast of approximately
200
August
1982
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