•
.Section VI
Wt & Bal/Equip List
COMPUTING PROCEDURE
BEECHCRAFT
Sierra C24R
1.
Record the Basic Empty Weight and Moment from the
Basic Empty Weight and Balance form (or from the latest
superseding form) under the Basic Empty Condition block.
The moment must
be
divided by 100 to correspond to
Useful Load Weights and Moments tables.
2.
Record the weight and corresponding moment from the
appropriate table
of
each
of
the useful load items (except
fuel) to be carried in the airplane. {
3.
Total the weight column and moment column. The
SUB-TOTALS are the ZERO FUEL CONDITION.
4. Determine the weight and corresponding moment for
the fuel loading to be used. This fuel loading includes fuel
for the flight, plus that required for start, taxi, and takeoff.
Add the Fuel Loading Condition to Zero Fuel Condition to
obtain the SUB-TOTAL Ramp Condition.
5.
Subtract the fuel to
be
used for start, taxi, and takeoff
to arrive at the SUB-TOTAL Take-off Condition.
6.
Subtract the weight and moment
of
fuel to
be
used
from the take-off weight and moment. The SUB-TOT
AL
Condition
of
No. 3
and
No. 5, as welt as the landing
condition
moment,
must
be
within
the
minimum and
maximum moments shown on the Moment Limits vs Weight
graph for that weight. If the total moment is less than the
minimum moment allowed, useful load items
must
be
shifted aft, or forward load items reduced. If the total
moment is greater than the maximum moment allowed,
useful load items must
be shifted forward, or aft load items
reduced. If the quantity or location
of
load items is changed,
the
calculations
must
be
rev
ised and
the
moments
r.echecked.
6-14 November, 1980
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