Sling LSA
Section 6
Pilot Operating Handbook
Weight and Balance
Document Number: DC-POH-002-X-A-6
Page | 6-6
Revision: 3.0
Date: 2021/04/23
6.6
Determination of Empty CG
ITEM
WEIGHT
[kg (lb)]
ARM
[mm (ft)]
MOMENT
(weight x arm)
[kg.mm (lb.ft)]
Ai
rc
ra
ft E
m
pt
y C
G
Right Main
Wheel
W
R
=
L
R
= 1 959 (6.427)
Left Main
Wheel
W
L
=
L
L
= 1 959 (6.427)
Nose Wheel W
N
=
L
N
= 464 (1.522)
Totals
Empty weight:
W
E
= …………………
-
Aircraft moment:
M
0
=………………..
Final CG
CG = …………………. mm (ft)