6-10
Date of Issue: 04/2008
Revision: 1.0
WEIGHT & BALANCE REPORT
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ITEM
WEIGHT
(kg)
ARM
(m)
MOMENT
(WEIGHTxARM)
AI
R
C
R
A
FT
E
MP
TY
CG
RIGHT MAIN
WHEEL
W
R
=
L
R
=
LEFT MAIN
WHEEL
W
L
=
L
L
=
NOSE WHEEL
W
N
=
L
N
=
-
(negative arm)
-
COMPUTED CG
EMPTY
Empty Weight:
W
E
=
CG
= m
%
MAC
Aircraft moment:
