“AERO” Sp. z o.o.
SECTION 6
AT-3 R100
WEIGHT AND BALANCE
JULY, 2010
Page 6-3
AEROPLANE FLIGHT MANUAL
Graphical method
From the table 6.3:” Weight and Balance schedule” the actual weight and
moment of the empty aeroplane should be read off. If on the rear wall of
the cockpit is installed the collapsible tow bar to the weight of empty
aeroplane +1,5 kg should be added and moment +2,6 kgm should be
increased.
WARNING
The empty weight of the aeroplane is the weight of the
aeroplane with the unusable amount of fuel, engine oil, cooling
liquid and with the optional equipment according to 6.4
For known weights of fuel, passenger, pilot and luggage read off the
values of the moments from the chart 1 “values of the moments”.
Weights and moments should be calculated according to the following
table:
Aircraft Loading Example
Your Aircraft loading
Moment [kGm]
Moment [kGm]
Weight
[kg]
(+)
(-)
Weight
[kg]
(+)
(-)
Empty aeroplane
358
91.3
fuel (0.72 kg/l)
43.2
-11,1
pilot + passenger
142
85.2
Luggage
14
15.8
Moment totals
192.3
-11.1
Total weight and
moment
557.2
181.2
9