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Sport Flight Aviation.

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Talon Magnum

talon_magnum.jpg (37799 bytes)

 

 Category

 Ultralight or Experimental

 Construction Time

100-125 hours

 Field Set-Up Time

20-40 minutes

 Propulsion

 Single Carb Rotax 447

 40 HP

 Dual Carb Rotax 447

 45 HP

  Single Carb Rotax 503

 46 HP

 Dual Carb Rotax 503

 52 HP

 Single Carb Rotax 582

 65 HP

 Dual Carb Rotax 582

 65 HP

 Reduction Ratio

  Single Carb Rotax 447

 2.56:1

 Dual Carb Rotax 447

 2.58:1

 Single Carb Rotax 503

 2.58:1

  Dual Carb Rotax 503

 2.58:1

  Single Carb Rotax 582

 2.58:1

  Dual Carb Rotax 582

 2.58:1

 Propeller Diameter

  Single Carb Rotax 447

 60"

 Dual Carb Rotax 447

 60"

 Single Carb Rotax 503

 62"

  Dual Carb Rotax 503

 62"

  Single Carb Rotax 582

 64"

  Dual Carb Rotax 582

 68"

 Wing Span

 26 Feet 8 Inches

 

 Length

 21 Feet 9 Inches

 

 Height

 6 Feet 0 Inches

 

 Wing Area

 134 Square Feet

 

 Aileron Span

 8 Feet 9 Inches

 

 Flap Span

 4 Feet 7 Inches

 

 Gross Weight

 700 lbs.

 

 Empty Weight

 323 lbs.

 

 Useful Load

 377 lbs.

 

Talon Magnum Performance Specifications

 VNE (Never Exceed Speed)

 90 mph

 Maximum Level Speed

 80 mph

 Cruise Speed

 63-78 mph

 Rate of Climb (W/Rotax 503)

 900 Feet per Minute

 Rate of Climb (W/Rotax 582)

 1450 Feet per Minute

 Take Off Distance

 75-150 Feet

 Stall Speed

 27-30 mph