Section 6 – Weight and Balance
INTRODUCTION
1. INTRODUCTION
This section describes the procedure for establishing the basic empty weight and
the moment of the aircraft. Loading procedure information is also provided.
Aircraft must be operated in accordance with the limits con-
cerning the maximum takeoff weight and CG excursion as re-
ported in Flight Manual Section 2.
Pilot is responsible for checking the weight and CG excursion are compliant with
the related limits. CG excursion and weight limits are reported in Section 2 – Lim-
itations.
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