6-7
Date of Issue: 04/2008
Revision: 1.0
WEIGHT
(kg)
ARM
(m)
MOMENT
(WEIGHTxARM)
PILOT
55
0,6
33
PASSENGER
BAGGAGE
COMPARTMENT - A
BAGGAGE
COMPARTMENT - B
WING LOCKERS
FUEL TANKS
98
0,2
19,6
TOTAL
W= 153
M= 52,6
Take-Off Weight
:
501 kg
CG= 0,329 m
26
%
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
