Sling 4 TSi - Determination of Empty CG

Sling 4 TSi Section 6
Pilot Operating Handbook
Weight and Balance
Document Number: DC-POH-001-X-F-3.0 Page | 6-6
Revision: 3.0 Date: 2021/07/14
6.6 Determination of Empty CG
ITEM
WEIGHT
[kg (lb)]
ARM
[mm (ft)]
MOMENT
(weight x arm)
[kg.mm (lb.ft)]
Aircraft Empty CG
Right Main Wheel W
R
= L
R
= 2 236 (7.336)
Left Main Wheel
W
L
=
L
L
= 2 236 (7.336)
Nose Wheel
W
N
=
L
N
= 464 (1.522)
Totals
Empty weight:
W
E
= ………………..
-
Aircraft moment:
M
0
=…………………..
Empty CG
CG = …………………. mm (ft)