SectionVI
Wt
and Bal,11:quip List
BEECHCRAFT
Debonair
C33
Bonanza
E33
and
F33
2.
Record the
weight
and corresponding
moment
from
the
appropriate table
of
each
of
the
useful
load
items
(except fuei) to be carried
in
the airplane.
3.
Total the
weight
column
and
moment
column.
The
SUB-TOTAL
is
the Zero Fuel Condition.
4. Determine the
weight
and corresponding
moment
for
the
fuei
loading to
be
used. This
fuel
loading includes
fuel
for
the
flight.
plus
that
required
for
start, taxi, and
take-off.
Add
the Fuel
to
Zero Fuel Condition
to
obtain
the
SUB-TOTAL Ramp Condition.
5.
Subtract the tue! tobe usedfor start, taxi,
and
take-off
to arrive at the SUB-TOTAL Take-off Condition.
6.
Subtract the
weight
and
moment
of
the
fuel
in
the
incremental sequence in
which
it
is
to be used
from
the take-off
weight
and
moment.
The Zero Fuel Condi-
tion,
the
Take-Off Condition, and the Landing Condi-
tion
moment
must
be
within
the
minimum
and
maxi-
mum
moments
shown
on the
Moment
Limit
vs
Weight
table for that weight.
lf
the total
moment
is less
than
the
minimum
moment
allowed,
useful
load items
must
be shifted aft
or
forward
load
items
reduced.
lf
the
total
moment
is greater
than
the
maximum
moment
al-
lowed, useful load
items
must
be shifted
forward
or
aft
load
items reduced. lf
the
quantity
or
location
of
load
items is changed, the calculations
must
be revised and
the
moments
rechecked.
* The Empty
Weight
for
the airplane
may
be converted to
Basic Empty
Weight
by adding the
weight
and
moment
for
full
oil. (19 lbs. and
494
lb. in.)
6-16
August
1982
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