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Beechcraft Beech 95 2017 - Section 6 - Weight and Balance

Beechcraft Beech 95 2017
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Selkirk College IATPL Program Manual
Beech 95 POH Effective September 1, 2005 Appendix 14 - 52
Section 6 – Weight and Balance
Introduction to Section 6
Section 6 describes the procedures for establishing the basic empty weight and moment
of the airplane.
A weight and balance report for each airplane can be found in the Pilot Operating
Handbook in the airplane. The weight and balance report contains the actual weight,
moment and arm for the empty airplane. This data must be used when computing takeoff,
landing and zero fuel weight, moment and arm for the airplane.
Pilots must ensure that the airplane is loaded within the specified weight, arm and
moment limits throughout all flights. It is the responsibility of the pilot to ensure that the
airplane is loaded properly.

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