SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Arcus M
FLIGHT MANUAL
NOTE: Always full Liters are to be filled. Where value jumps, either
the higher or the lower amount of ballast may be used.
0
0
Lever arm of water ballast in fin tank (m ):
Fin tank capacity: 11 kg/Liter (2.91 US Gal., 2.42 IMP Gal.)
FT
5292 mm (17.36 ft) aft of datum plane
Max. water ballast in main wing panels
1
0.26
0.22
2
0.53
0.44
3
0.79
0.66
4
1.06
0.88
5
1.32
1.10
6
1.59
1.32
7
1.85
1.54
8
2.11
1.76
9
2.38
1.98
10
2.64
2.20
11
2.91
2.42
Liter
US Gal.
IMP Gal
M
a
x
.
fi
n
ta
n
k
c
a
p
a
c
it
y
W
in
g
w
a
te
r
b
a
ll
a
s
t
m
W
T
4.40 5.28 20
IM
P
.
G
a
l.
U
S
.
G
a
l.
L
it
e
r
8.58 10.30 39
12.76 15.32 58
17.16 20.61 78
21.34 25.62 97
25.52 30.64 116
29.92 35.93 136
34.10 40.95 155
38.06 45.70 173
40.70 48.87 185
M
a
x
.
fi
n
ta
n
k
c
a
p
a
c
it
y
Max. load on rear seat
0
1
0.26
0.22
2
0.53
0.44
3
0.79
0.66
4
1.06
0.88
5
1.32
1.10
6
1.59
1.32
7
1.85
1.54
8
2.11
1.76
9
2.38
1.98
10
2.64
2.20
11
2.91
2.42
Liter
US Gal.
IMP Gal
m
FT
Water ballast in fin tank
m
FT
Water ballast in fin tank
lo
a
d
o
n
r
e
a
r
s
e
a
t
m
(
k
g
)
P2
19.8 9
lb kg
0
37.4 17
57.3 26
75.0 34
92.6 42
112.5 51
130.1 59
147.7 67
167.6 76
185.2 84
205.1 93
1
L
it
e
r
=
1
k
g
(
2
.2
l
b
)
October
2011
Revision --
6.2.8