Flight
and
operational
manual
TL
3000
SIRIUS
Page
43
1.
Determine
the
weight
of
the
onboard
items
for
the
required
configuration:
G
POS
(crew
weight),
G
PAL
(fuel
weight),
and
G
ZAV
(luggage
weight
in
the
luggage
compartment)
2.
Calculate
the
empty
aircraft
centre
of
gravity
for
the
required
configuration
(by
inserting
the
values
derived
from
the
step
1
a
2
into
the
formula)
WARNING:
The
calculated
x
%CONFIGURATION
value
must
fit
within
the
centre
of
gravity
positioning
permitted
range
from
22
to
32.5
%MAC.
Summary of Contents for TL-3000 Sirius
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