|
Version
|
Q201J
|
O201R582
|
Q201R
|
Q201RS
|
Engine
|
Jabiru
2200
|
Rotax
582
2V
|
Rotax
912UL2
|
Rotax
912ULS2
|
Engine output
|
80HP
|
65HP
|
80HP
|
100HP
|
Two bladed fixed propeller
|
V250
|
V230C
|
V230D
|
V230E
|
|
|
|
|
|
Max. take-off weight
|
450 kg
|
450 kg
|
450 kg
|
450 kg
|
Weight of empty aircraft in
standard specification
|
265 kg
|
265 kg
|
282 kg
|
286 kg
|
|
|
|
|
|
Wingspan
|
9,2 m
|
9,2 m
|
9,2 m
|
9,2 m
|
Length
|
6,1 m
|
6,05 m
|
6,0 m
|
6,0 m
|
Height
|
1,7 m
|
1,7 m
|
1,7 m
|
1,7 m
|
Wing area
|
10,5 m2
|
10,5 m2
|
10,5 m2
|
10,5 m2
|
|
Characteristics respecting max. take-off weight and
condition of the International standard atmosphere on marine level:
|
Max. horizontal speed
|
230
|
180
|
220
|
237
|
Cruise speed
|
140-190
|
120-150
|
140-190
|
140-210
|
Stalling speed
|
|
|
|
|
Cruising
specification
|
71
|
71
|
71
|
71
|
Landing
specification
|
60
|
60
|
60
|
60
|
Max. climbing speed m/sec
|
5
|
3,2
|
5
|
6,6
|
|
|
|
|
|
|
Price with
standard equipment ( without V.A.T. )
|
€ 40 757
|
€ 36 043
|
€ 44 245
|
€ 45 515
|
|
