Flight Manual LS10-s,-st
Issued:
December
2011
TN
LS10-02
6.13
Table of C.G. positions for various items of equipment:
Item mass
C.G.
behind
datum
kg
lbs
m
ft
1 Battery in front of control stick
*)
2,5 5,5 -1,05
-3,44
Battery in baggage compartment
4BR-255/2
2,5 5,5 0,185
0,61
Battery in the fin 3BR-199
2,6
5,7
4,308 14,13
Water in LH (System No.1)-
(forward) fin tank - up to
3,9 8,6 4 13,12
Water in RH (System No. 2)-
(rear) fin tank - up to
4,6 10,1
4,16
13,65
Water in outer wing tank
(System No.1) - up to
30,0 66,1 0,189
0,62
Water in the centre wing tank
(System No. 1)- up to
50,0 110,2
0,189
0,62
Water in the inner wing tank
(System No. 2) - up to
110,0 242,5 0,196 0,64
Powerplant 26,5
58,4
1,05
3,44
Empty fuel tank
1,5
3,3
0,38 1,25
Fuel in main tank max.
7,0
15,4
0,38 1,25
Trim weight rear fuselage 4R8-
109
2,5 5,5 4,383
14,38
Trim weight in front support
4R8-108
2,45 5,4 -1,69 -5,54
Heavy tail wheel (P/N.: S27) **) 3,4
6,6
4,314 14,15
*) usually 2 batteries are installed
**) 3.0kg (6.6 lbs) more than standard tail wheel with plastic hub S23
(mass of plastic hub S23 with tyre= 0,9 kg (1.98 lbs.))
