S k y F o x F l i g h t T r a i n i n g
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SKYFOX
CA25N

POWERPLANT
Engine Type
No. of Cylinders
Ignitions System
Max. Horsepower
Engine Capacity
Max. RPM
Cruise RPM
Max. Continuous
Fuel Consumption
Fuel Grade
Propeller
   Rotax 912A
   4-liquid cooled/4 stroke
   dual CDI
   80
   1211cc
   5500
   5000
   5500 RPM
   14 litres/hr.
   Mogas (super)
   2 blade/wood
PERFORMANCE @ MAX. WEIGHT (all quoted speeds are in Knots)
Lift-off speed
Best Climb Speed
Approach Speed
Max. Crosswind
Stall Speed
Cruise Speed
Vne-never exceed speed
Useable Fuel
Endurance
Range
Service Ceiling
Glide Ratio
Takeoff roll
Landing Distance
Stuctural limits
Manufacturer
Wing Span
Fuselage length
Gross Weight
Empty Weight 		   45
   55
   60
   14
   43
   70
   93
   48 litres
   3.4 hours
   240 nautical miles
   13,500'
   10:1
   100 meters
   120 meters
   6G positive/3G neg.
   Skyfox Aviation
   9.5 meters
   5.6 meters
   520 kgs
   315 kgs