tecHnicaL data
tyP
CELLS
FLAT SuRFACE AREA [QM]
FLAT WINGSPAN [M]
FLAT ASPECT RATIo
AREA PRoJECTED [QM] .
PRoJECTED WINGSPAN [M]
PRoJECTED ASPECT RATIo
WEIGHT [KG]
LEGAL LAuNCH WEIGHT [KG]
ToW
JET FLAP TECHNoLoGY
MoToR CERTIFICATIoN
tHe SerieS taG iS Printed On tHe inSide Of tHe StabiLO.
tHe certificatiOn taG can be fOund in a POcket On tHe MiddLe PrO-
fiLe rib.date and PiLOt Of tHe firSt fLiGHt MuSt be entered. tHe
certificatiOn taG MuSt be attacHed tO tHe ParaGLider in GerMany.
if tHere iS nO taG attacHed, tHe SkyWaLk SeaL MuSt be viSibLe. tHiS
SeaL cOnfirMS tHat tHiS GLider MOdeL iS identicaL in cOnStructiOn
tO tHe MOdeL teSted at tHe inSPectiOn center. if tHiS SeaL iS MiSS-
inG, it MuSt be aSSuMed tHat tHiS iS an uninSPected PrOtOtyPe.
XXS
XS
51
51
21,85
24,71
10,99
11,68
5,52
5,52
18,57
20,99
8,7
9,25
4,07
4,07
4,6
4,9
55-75
70-90
YES
YES
YES
YES
No
No
S
M
51
51
26,89
28,87
12,19
12,63
5,52
5,52
22,85
24,54
9,65
10
4,07
4,07
5,2
5,6
80-100
90-114
YES
YES
YES
YES
No
No
L
51
31,83
13,26
5,52
27,05
10,49
4,07
6,0
100-130
YES
YES
No
37