Aircraft's general specification
| | Wings span | 8.630 [m] | Fuselage width | 1.05 [m] | | Wing surface | 12.08 [m²] | Maximum take-off weight | 450 [Kg] | | Length | 6.450 [m] | Wing tank | 76 [l] | | Heigth | 2.40 [m] | Maximum luggage | 25 [Kg] |
LAND AFRICA
| DUIKER | IMPALA | PALANCA | ENGINE | Rotax 582 | Rotax 912 UL | Rotax 912 ULS | WEIGHT | 255 [Kg] | 270 [Kg] | 274 [Kg] |
MAXIMUM TAKE-OFF WEIGHT
| 450 [Kg] | 450 [Kg] | 450 [Kg] |
MAXIMUM LUGGAGE
| 25 [Kg] | 25 [Kg] | 25 [Kg] | CROSS WIND LIMIT | 22 [MPH] | 22[MPH] | 22 [MPH] | CLIMB RATE@ 60 mph | 800 [ft/min] | 1000 [ft/min] | 1200 [ft/min] | MAX SPEED STRAIGHT AND LEVEL FLIGHT | 94 [MPH] | 100 [MPH] | 109 [MPH] | STALL SPEED | 26 [MPH] | 26 [MPH] | 26 [MPH] | APPROACH SPEED | 38 [MPH] | 38 [MPH] | 38 [MPH] | MANOEUVRING | 90 [MPH] | 90 [MPH] | 90 [MPH] | CRUISE SPEED
(5000 [RPM]): | 86 [MPH] | 92 [MPH] | 100 [MPH] | VNE | 126 [MPH] | 126 [MPH] | 126 [MPH] | TAKE-OFF RUN | 35 [m] | 35 [m] | 30 [m] | CONSUMPTION | 17 [l/h] | 12 [l/h] | 14 [l/h] |
EFFICIENCY
| BEST GLIDE SPEED | 66 [MPH] | 66 [MPH] | 66 [MPH] | TAKE-OFF WITH 450 [Kg] | WITHOUT FLAPS | 55 [m] | 55 [m] | 45 [m] | WITH ONE POINT OF FLAPS | 55 [m] | 55 [m] | 45 [m] | SPEED | 54 [MPH] | 54 [MPH] | 54 [MPH] | WITH TWO POINTS OF FLAPS | 55 [m] | 55 [m] | 45 [m] | | SPEED | 38 [MPH] | 38 [MPH] | 38 [MPH] | LANDING DISTANCE | 85 [m] | 85 [m] | 85 [m] | WITH ONE POINT OF FLAPS | 65 [m] | 65 [m] | 65 [m] | WITH TWO POINTS OF FLAPS | 40 [m] | 40 [m] | 40 [m] | LOAD FACTOR | MAXIMUM WEIGHT 450 KG | +4 [g] | +4 [g] | -2 [g] | THE LOAD FACTOR IS VALID UP TO THE MAXIMUM TAKE-OFF WEIGHT OF 450 KG. |
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Last Updated ( Monday, 12 May 2008 21:14 )
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