6-9
Date of Issue: 04/2008
Revision: 1.0
WEIGHT
(kg)
ARM
(m)
MOMENT
(WEIGHTxARM)
PILOT
80
0,6
48
PASSENGER
80
06
48
BAGGAGE
COMPARTMENT - A
0
1.4
0
BAGGAGE
COMPARTMENT - B
14
2,0
28
WING LOCKERS
0
0,65
0
FUEL TANKS
22
0,20
4,4
TOTAL
W = 196
M= 128,4
Take-Off Weight
:
544 kg
CG= 0,443 m
35
%
MAC
Max.Take-off Weight: 544 kg
CG Range: 24
– 35 %
Total Moment 100
Center of Gravity (
CG
) = ------------------- [ in ] x --------- [ % ]
Total Weight
MAC
Serial No: 001/2008
Date: 2008-04-26
By: Milan Bristela
