Land Africa
Specifications |
|
Wing span |
8.63 m |
Fuselage width |
1.05 m |
|
Wing surface |
18.08 m² |
Maximum take-off weigth |
450 kg |
|
Length |
6.45 m |
Wing tank |
76 l |
|
Heigth |
2.40 m |
Maximum luggage |
25 kg |
|
performance - desempenho |
|
Engine |
Rotax
912 uls |
Limit of crossed wind |
35 k/h |
|
Max. Speed (VNE) |
175 k/h
(205 k/h) |
Stall speed |
40 k/h |
|
Approach speed |
60 k/h |
Cruise speed |
175 k/h |
|
Take-off distance |
30 m |
Consumption |
14 l/h |
|
Charge coefficient (*) |
+4g /-2g (at
450 kg) |
| (*)The security
coefficient does not permit, in any case, to exceed the
maximum take-off weight of 450 kg. |
|
|
