Airplane Factory SLING 4
Pilot Operating Handbook
Page | 6-7
DC-POH-001-X-C-3
Revision : 1.3
6.5
Empty CG determination
ITEM
WEIGHT
[kg (lb)]
ARM
[mm (ft)]
MOMENT
(weight x arm)
[kg.mm (lb.ft)]
Air
cra
ft E
m
p
ty
C
G
Right Main
Wheel
W
R
=
L
R
= 2 236 (7.335)
Left Main
Wheel
W
L
=
L
L
= 2 236 (7.335)
Nose Wheel
W
N
=
L
N
= 548 (1.797)
Computed
empty CG
Empty weight:
W
E
= …………..kg (lb)
CG = ……….. mm (ft)
(…………% MAC)
Aircraft moment :
Maximum take-off weight = 920 kg (2028.25 lb).
Maximum useful load (example):
W
max useful
= W
MAUW
- W
E.
= 920 kg (2028.25 lb) - 490 kg (1080.27 lb)
= 430 kg (947.99 lb)
Содержание SLING 4
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