l I.C.P.
Sri
l
Savannah
FLIGHT
MANUAL
j Pag.
341
6.1
GENERAL
The aircraft is allowed
to
have its CG (Centre
of
Gravity) within a quite large range thus
easing the aircraft's loading and balancing. By knowing the weights
ofthe
people, fuel and baggage
to be carried on board and using the attached W
&B
report, the pilot would be
ab
le to check for the
proper aircraft's weight and balance configuration. To find out the CG position piease refer to the
attached table. Compute the total weight and the total moment, given by adding all the single
moments. To be acceptable, the found point MUST be located into the WHITE area, between the
two limit lines.
W ARNING: a CG beyond the most foreward limit,
as
well
as
a CG beyond the most rearward limit
may result in a VERY DANGERODS flight condition.
NOTE:
it's
strictly forbidden
to
make any change or modification to the aircraft since those
modifications may affect the balance limits set by the manufacturer.
Issue l/Revision 2
Ott. 02
ICP
Sri-
Via Torino 12, 14020 PlOV
A'
MASSAIA
(AT)-
Italy
Phone +39-0141-996503 • Fax +39-0141-996506
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