Flight
and
operational
manual
TL
3000
SIRIUS
Page
41
6.1
Introduction
Section
6
includes
the
allowed
centre
of
gravity
positioning
and
weight
ranges
and
centre
of
gravity
position
determination
procedure
allowing
safe
aircraft
operating.
6.2
Centre
of
gravity
positioning
permitted
range
and
maximum
take
‐
off
weight
Aircraft
maximum take
‐
off
weight
(kg)
472,5
Centre
of
gravity
positioning
permitted
range
(%
MAC)
22
–
32,5
6.3
Empty
aircraft
centre
of
gravity
determination
This
paragraph
defines
the
correct
aircraft
weighing
procedure
and
empty
aircraft
centre
of
gravity
position
calculation.
a
=
840
mm
b
=
690
mm
c
=
35
mm
SAT
=
1230
mm
Содержание TL-3000 Sirius
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