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Tecnam P2010 2015 - Page 160

Tecnam P2010 2015
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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 takeojfweight
and
CG excursion
as
re-
ported
in
Flight Manual Sect10n
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.
Section
6 -
Weight
and
Balance
INTRODUCTION
2"d
Edition, Rev. 0