Computing Procedure - Beechcraft Debonair 35-33 Pilot Operating Handbook

SectionVI
Wt
and Bal;'Equip List
COMPUTING PROCEDURE
BEECHCRAFT
Debonair33
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. Th e moment must be divided by 100
to cor respond 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 f uel 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 weig ht and moment. The Zero Fuel Condi -
tion, the Take-Off Condition, and the Landing Condi-
6 - 16
April 1982