| M106 Specifications |
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Wing span:
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9.32 m (30 ft 6 in)
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Baggage capacity:
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40 kg (90 lbs)
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Wing area:
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11.8 m² (127 ft²)
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Cabin width:
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1.12 m (44 in)
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Aspect ratio:
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7.4
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Fuel capacity std.
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70 l
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Length:
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5.65 m (18 ft 6 in)
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Tailplane span:
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2.40 m (8 ft 0 in)
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Height (taildragger):
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1.80 m (6 ft 0 in)
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Wheeltrack:
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1.75 m (5 ft 10 in)
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Height (nosewheel):
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1.95 m (6 ft 6 in)
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Limit load factors:
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4.0/-2.0
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Max. crosswind comp.
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12 kt (taildragger)
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16 kt (nosewheel)
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Never exceed speed:
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210 km/h (112 kt)
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Engine:
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Engine displacement:
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2.6 litres (160 cu.in)
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Engine output:
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60 kW (82 HP) at 2800 rpm
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Empty weight:
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260 kg
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Max. all up weight:
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450-480 kg1
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Max. level speed at S/L:
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100 kt (185 km/h)
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Max. S/L rate of climb:
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1000 ft/min (5 m/s)
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Cruise speed:
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80-85 kt (150-160 km/h)
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Fuel consumption:
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10-12 litres/h
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Range (20 min res.):
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380 nm (700 km)
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Stall speed, full flaps:
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35 kts (65 km/h)
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T-O ground roll:
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80-110 m
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1
Structure designed and tested to 495 kg. Allowed maximum all up weight may be limited to 450 or 472.5 kg depending on national regulations. |
