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Gn =
Gml =
Gmr =
Gtotal =
La =
Lb =
kg
kg
kg
kg
706 mm
1518 mm
Center of Gravity
Lt = Gn x Lb / Gtotal
Xt = La - Lt
X% = Xt x 100 / MAC
Lt = ..... x 1518 / ..... = ....
Xt = 706 – .... = ....
X%
= .... x 100 / 1312 =
....%
Flight Manual Page 10 of 40