l I.C.P.
Sri
l
Savannah
FLIGHT
MANUAL
l Pag.
351
6.2 WEIGHT AND BALANCEREPORT
Procedure
to be used to determine the Centre o f Gravity position:
- The aircraft
MUST be weighed fitted with all equipments, accessories, engine oil, coolant
and
WITHOUT FUEL;
NOTE:
all the fuel MUST be drained accurately.
-
Put the aircraft on three weight measuring equipments ( each under each wheel o f the landing
gear);
- Put the aircraft in the flight level position by using a level fitted o n the aircraft' s fuselage, o n the
horizontal plane where doors will be closed;
-Record
the three weight measuring equipments readings: the nose wheel weight will be called
Pl,
the left wheel weight P2, the right wheel weight P3;
- By using a plumbing wire fix ed to the leading edge, measure the distance D l between the
projection on the floor o f the leading edge and the nose wheel axle, and the distance D2 between the
same projected point and the main landing gear axle;
- By filling out the table below, make the calculations and find out the CG position. The airplane is
in the correct balance
if
the line o f the actual weight and the line o f the actual total moment cross
inside the white area.
TABLE
TO
DETERMINE
THE
AIRCRAFT'S
BASIC
EMPTY
WEIGHT
Aircraft serial number
Weight measuring equipment
Location and date
Certifying staff
N ose landing gear
LH
main landing gear
RH
main landing gear
TOTALS
l Signature
Issue l /Revision l
Apr.
Ol
Weight (kg)
Arm
(m)
Moment
(kg x m)
PI
=
n,{),
t
L/5~s
71..
<,./'
P2=
D2=€J
~
,u
p3 =
D2=fJ
7o,)-
"
/CJIX
ICP
Sri-
Via Torino 12, 14020 PlOV
A'
MASSAIA
(AT)-
Italy
Phone +39-0141-996503 • Fax +39-0141-996506
\
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