Tecnam P-Mentor - Page 155

1
st
Edition - Rev. 0
Section 6 – WEIGHT AND BALANCE
INTRODUCTION
P-Mentor – Aircraft Flight Manual Page 6 - 3
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
concerning the maximum take-off 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. C.G. excursion and Weight limits are reported in Section 2 –
Limitations.