F
F
l
l
i
i
g
g
h
h
t
t
M
M
a
a
n
n
u
u
a
a
l
l
S
S
u
u
p
p
p
p
l
l
e
e
m
m
e
e
n
n
t
t
f
f
o
o
r
r
t
t
h
h
e
e
s
s
a
a
i
i
l
l
p
p
l
l
a
a
n
n
e
e
Document No.: G304eS/AFMSupp, R00
Date of Issue: 09/16
6-2
H
P
H
Ltd.
6.6
Founding of CG position in case of battery packs
removed.
For preliminary estimation of CG position following equation can be
used. Permitted CG range is 251-378 mm.
WARNING
Position of sailplane CG in case motor and battery packs removed
must be determined by weighting of sailplane in intended configuration.
Sailplane CG and empty weight must lie in permitted range of Trim
plan (G304S/FM chapter 2.5) Weighting procedure is described in
G304S/MM.
