M106 aircraft, UL260i engine hyperflite
M106 aircraft, UL260i engine
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M106 aircraft, UL260i engine
M106 Specifications
Mission M 106





Wing span:
9.32 m (30 ft 6 in)
Baggage capacity:
40 kg (90 lbs)
Wing area:
11.8 m² (127 ft²)
Cabin width:
1.12 m (44 in)
Aspect ratio:
7.4
Fuel capacity std.
70 l
Length:
5.65 m (18 ft 6 in)
Tailplane span:
2.40 m (8 ft 0 in)
Height (taildragger):
1.80 m (6 ft 0 in)
Wheeltrack:
1.75 m (5 ft 10 in)
Height (nosewheel):
1.95 m (6 ft 6 in)
Limit load factors:
4.0/-2.0
Max. crosswind comp.
12 kt (taildragger)
 
 
 
16 kt (nosewheel)
 
 
Never exceed speed:
210 km/h (112 kt)
 
 

 

Engine:
 
Engine displacement:
2.6 litres (160 cu.in)
 
Engine output:
60 kW (82 HP) at 2800 rpm
 
Empty weight:
260 kg
 
Max. all up weight:
450-480 kg1
 
Max. level speed at S/L:
100 kt (185 km/h)
 
Max. S/L rate of climb:
1000 ft/min (5 m/s)
 
Cruise speed:
80-85 kt (150-160 km/h)
 
Fuel consumption:
10-12 litres/h
 
Range (20 min res.):
380 nm (700 km)
 
Stall speed, full flaps:
35 kts (65 km/h)
 
T-O ground roll:
80-110 m
 


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.
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