Section VI
Wt and Ba~quip List
BEECH CRAFT Bonanza
V35, V35A & V358 thru D-9947
COMPUTING PROCEDURE
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-TOTAL is 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
take-off. Add the Fuel to Zero Fuel Condition to obtain
the SUB-TOTAL Ramp Condition.
5. Subtract the fuel to be used for 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. 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 al-
lowed, usefu I 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 revised and
the moments rechecked.
6-12
January 1982
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