Weight and Balance N3-2 PUP
LN-YGA
Consult POH for Official Numbers
Datum: Front of propeller hub.
All measurement are performed with the airplane in
"level fiight" position (Top Longeron level).

__________	_________	_______
From Weight	Weight	Arm
Report	Kg	mm
--------------	------------	---------
Empty Weight
Empty CG
__________	_________	_______	_________
Weight and	Weight	Arm	Moment
Balance	Kg	mm	/ 1000
--------------	------------	---------	-----------
	20 Kg 15 Kg 12 Kg 10 Kg 8 Kg 7 Kg 6 Kg 5 Kg 4 Kg 3 Kg 2.5 Kg 2 Kg 1.5 Kg 1 Kg 0.5 Kg 0 Kg
	19 L 15 L 10 L 5 L 0 L
	13.2 L 10 L 8 L 6 L 4 L 2 L 0 L
	13.2 L 10 L 8 L 6 L 4 L 2 L 0 L
	60 L 55 L 50 L 45 L 40 L 35 L 30 L 25 L 20 L 15 L 10 L 5 L 0 L
	120 Kg 110 Kg 100 Kg 95 Kg 90 Kg 85 Kg 80 Kg 75 Kg 70 Kg 65 Kg 60 Kg 55 Kg 50 Kg 45 Kg 40 Kg 35 Kg 30 Kg 25 Kg 20 Kg 15 Kg 12 Kg 10 Kg 8 Kg 6 Kg 4 Kg 2 Kg 0 Kg
	120 Kg 110 Kg 100 Kg 95 Kg 90 Kg 85 Kg 80 Kg 75 Kg 70 Kg 65 Kg 60 Kg 55 Kg 50 Kg 45 Kg 40 Kg 35 Kg 30 Kg 25 Kg 20 Kg 15 Kg 12 Kg 10 Kg 8 Kg 6 Kg 4 Kg 2 Kg 0 Kg
	30 Kg 25 Kg 20 Kg 15 Kg 12 Kg 10 Kg 8 Kg 7 Kg 6 Kg 5 Kg 4 Kg 3 Kg 2.5 Kg 2 Kg 1.5 Kg 1 Kg 0.5 Kg 0 Kg
--------------	------------	---------	-----------
Fuel_Burn:	7 L/t 7.5 L/t 8 L/t 8.5 L/t 9 L/t 9.5 L/t 10 L/t 10.5 L/t 11 L/t 11.5 L/t 12 L/t 12.5 L/t 13 L/t 13.5 L/t 14 L/t 14.5 L/t 15 L/t
__________	_________	_______	_________
Sum:		Kg
CG:

cg_min = 1340 mm
cg_max = 1543 mm
        Fuel =