sonaca aircraft S201 - Page 166

S201 AFM
6 - WEIGHT AND BALANCE
6.5 - MASS AND BALANCE
REPORT
27/06/2019
SONAIR-S2-D-MAN-006
Page : 6-5
Rev. : A
ITEM
MASS
[kg]
ARM
[mm]
MOMENT
(mass x arm)
[kg.mm]
(1)
Empty
aircraft
WE =
………….
(2)
Pilot &
passenger
1150
(3)
Baggage
(Area 1)
1500
(4)
Baggage
(Area 2)
2296
(5)
Fuel Mass
at TO
706
(6)
TOTAL at
TO (1)
thru (5)
CG position=………….
(% MAC =………………)
(7)
Estimated
mission
Fuel burn
Mass
706
(8)
Total at
Landing =
(6)-(7)
CG position=………….
(% MAC =………………)
INFORMATION
CG position = Moment / Mass
CG position in % MAC = 100*( CG position – 612 mm) / 1318 mm