Tecnam P2010 2015 - Page 166

A /C empty mas s moment
A/C empty mas s
Occ. front seats
Occ. rear seats
Fuel
Baggage
T.O. weight
Plotted example Ired line)
188 kg•m ( 1360 lb* ft)
765 kg(l687lb)
160 kg(353lb)
140 kg (309 lb)
75 kg(l65lb)
20 kg (44 lb)
1160 kg (2557 lb)
3.1. C.G. CALCULATION SAMPLE
(leg] Arm [mm)
Empty weight
7M(1887) b)
245 (0 ,80 ft )
CoG pos.
17,8%
USEFUL LOAD
Piiot
~.(1781b) .
280 (0 .92 ft)
P ii ot
·" · •'( - -
. 80 . ~~ J ~ b
280 (0, 92ft )
PAX
70 (164) b)
1057 (3.47 ft)
PAX
70 (154 lb)
1057 (3.47 ft)
Baggages
20( ~ 1b) .-
1 59 9 (5,25 ft)
Fuel volume•p,. ..
104-0,12 •1s (' i651b)
6 12 (2 ,00 ft)
Useful load
395 (871 lb)
685 (2,24 ft)
W ro
1160 (2557 lb)
395 (1 , 29 ft )
CoG pos .
28,7%
Moment [kg*mm)
187642(13501b*ft)
22400 (1 62 l b* ft)
22400 (162 lb*ft)
73990 (534 lb*ft)
73990 (534 lb*ft)
31980 (2 31 lb*ft)
45900 (330 lb*ft)
270660 (1953 lb*ft)
458302 (3303 lb*ft)
Ptuel = Density of fuel, it generally varies between 0. 71 and 0.77 depending on
fuel grade and ambient temperature.
Section 6 - Weight and Balance
C.G. CALCULATION SAMPLES
2"J Edition, Rev. 7