Aircraft Operating Instructions (AOI)
Type:
CT
Series:
CTLS
LSA
Page: 6-8
AU 010 11000
Revision No. 6
Date: 05 Feb 2009
0,3
0
0,3
2
0,3
4
0,3
6
0,3
8
0,4
0
0,
42
0,
44
0,
46
0,
48
0,
50
[m
m
]
0,2
8
Cent
er of
Grav
ity
Flight Mas
s
Pe
rm
iss
ible CG R
a
nge
37
5
57
5
55
0
52
5
50
0
47
5
45
0
42
5
40
0
60
0
[kg]
35
0
32
5
30
0
0,2
6
forw
ard
limit
28
2m
m (
11.1 in
)
rear limit
478
mm
(18.8
in)
max.
p
e
rmit
te
d
f
lig
h
t m
a
s
s
600
kg
(
1
32
0 lb
)
62
5
80
0
1.2
0
0
1.1
5
0
1.1
0
0
1.0
5
0
1.0
0
0
95
0
90
0
85
0
1.3
5
0
[l
b]
75
0
70
0
66
0
1.3
0
0
1.2
5
0
11
12
13
14
15
16
1
7
1
8
1
9
[i
n]
0,3
0
0,3
2
0,3
4
0,3
6
0,3
8
0,4
0
0,
42
0,
44
0,
46
0,
48
0,
50
[m
m
]
0,2
8
0,3
0
0,3
2
0,3
4
0,3
6
0,3
8
0,4
0
0,
42
0,
44
0,
46
0,
48
0,
50
[m
m
]
0,2
8
Cent
er of
Grav
ity
Flight Mas
s
Pe
rm
iss
ible CG R
a
nge
37
5
57
5
55
0
52
5
50
0
47
5
45
0
42
5
40
0
60
0
[kg]
35
0
32
5
30
0
0,2
6
forw
ard
limit
28
2m
m (
11.1 in
)
rear limit
478
mm
(18.8
in)
max.
p
e
rmit
te
d
f
lig
h
t m
a
s
s
600
kg
(
1
32
0 lb
)
62
5
80
0
1.2
0
0
1.1
5
0
1.1
0
0
1.0
5
0
1.0
0
0
95
0
90
0
85
0
1.3
5
0
[l
b]
75
0
70
0
66
0
1.3
0
0
1.2
5
0
11
12
13
14
15
16
1
7
1
8
1
9
[i
n]
The example shown in this diagram represents the verification of the mass and cg
position values achieved as by the example shown in the analysis table. The aircraft
with no fuel is represented by the values 415 kg (
916 lb
) and 380 mm (
15,0 in
). The
aircraft takeoff fuel is represented by the values 458 kg (1.011
lb
) and 0,398 m (
15.6
in
). Both values are within the allowed range.
Example 1:
mass moment
wit
h
empt
y f
u
el t
a
nks
Example 2:
mass moment with
ful
l fue
l ta
nk
s
