• Six Month Limited Warranty (See Dealer For Details)
   
• Dual CDI Electronic Ignition, Dual Carburetor Engine
   
• Steerable Nose Wheel Standard
   
• Main Wheel Brakes
   
• Double Surface Wings
   
• Extra Ribs for Firm Airfoil
   
• Conventional 3-Axis Controls
   
• 68" Propeller for More Power With Less Noise Stabilizer
   
• New, Wider Cabin for Greater Pilot Comfort
   
• Inflight Adjustable Trim Control
   
• Tapered Stabilizer
   
• Tubular Braced Tail
   
• Excellent Crosswind Capability
   
• Easy Handling and Responsive Control
   
• Short Takeoff and Landing
   
• Quicksilver’s Famous Quality
   
• Easy-to-Assemble Kit (Average 40 to 60 Hours)
   
• Airspeed Indicator Included
   

NOTE: All specifications are based on manufacturer's calculations.
All performance figures are based on standard day, standard atmosphere, at sea level
and 350 lb. crew weight, unless otherwise noted.
The performance shown reflects this aircraft’s maximum potential.
Flight training required.
Specifications subject to change without notice.
This aircraft is not designed for aerobatics.
Be sure to follow the owners manual recommendation for maintenance guidelines.
The pilot is responsible for operating this aircraft in accordance with the applicable Federal and State Regulations.

   POWERPLANT:
      Model..........................................Rotax 503
      No. Cylinders............................................2
      Displacement...............................496.7 cc
      Horsepower.......................................50 hp
      Recommended TBO......................250 hrs
      Propeller.......................................68" x 32"
      Length...............................................216 in.
      Height................................................109 in.
      Wingspan........................................32.75 ft
      Wing area.....................................180 sq ft
      Wing loading..............................4.0 lb/sq ft
      Power loading............................14.4 lb/hp
      Seats..........................................................2
      Minimum flight crew..................................1
      Empty Weight.................................325 lbs
      Useful load......................................395 lbs
      Payload w/full fuel...........................359 lbs
      Max takeoff weight.........................720 lbs
      Fuel capacity....................................6 gals

   PERFORMANCE:
      Takeoff distance, ground roll...........155 ft
      Takeoff distance, 50 ft obstacle......435 ft
      Rate of climb.................................595 fpm
      Max level speed, sea level............61 mph
      Landing distance, 50 ft obstacle.....300 ft
      Landing distance, ground roll.............75 ft
      Glide Ratio..........................................5.0:1
      Minimum sink rate........................630 fpm

   CRUISE PERFORMANCE CHART:
      At 55% power (rpm/mph)............5000/40
      At 65% power (rpm/mph)............5300/48
      At 75% power (rpm/mph)............5600/54
      At 100% power (rpm/mph)..........6500/61

   FUEL FLOW:
      At 55% power (gpm/mi)..................3.2/73
      At 65% power (gpm/mi)..................3.8/72
      At 75% power (gpm/mi)..................4.4/69
      At 100% power (gpm/mi)................5.8/56

   AIRSPEEDS:
      V_x (Best angle of climb)...............37mph
      V_y (Best rate of climb)..................39 mph
      V_a (Design maneuvering)............64 mph
      V_ne (Never exceed)......................75 mph
      V_s1 (Stall, power off).....................32 mph
      V_s0 (Stall, flaps down, power off).......N/A
      Landing approach speed.............45 mph

      Kit Cost: ...................................Contact dealer for price

   POWERPLANT:
      Model..............................................Rotax 582
      No. Cylinders.................................................2
      Displacement....................................580.7 cc
      Horsepower............................................64 hp
      Recommended TBO..........................250 hrs
      Propeller...........................................68" x 36"
      Length....................................................210 in.
      Height....................................................112 in.
      Wingspan............................................32.75 ft
      Wing area..........................................180 sq ft
      Wing loading...................................4.0 lb/sq ft
      Power loading...............................11.25 lb/hp
      Seats...............................................................2
      Minimum flight crew.......................................1
      Empty Weight......................................330 lbs
      Useful load...........................................390 lbs
      Payload w/full fuel................................354 lbs
      Max takeoff weight..............................720 lbs
      Fuel capacity..........................................6 gals

   PERFORMANCE:
      Takeoff distance, ground roll................121 ft
      Takeoff distance, 50 ft obstacle...........260 ft
      Rate of climb....................................1145 fpm
      Max level speed, sea level.................67 mph
      Landing distance, 50 ft obstacle...........300 ft
      Landing distance, ground roll..................75 ft
      Glide Ratio...................................................5:1
      Minimum sink rate..............................630 fpm

   CRUISE PERFORMANCE CHART:
      At 55% power (rpm/mph).................5000/43
      At 65% power (rpm/mph).................5300/52
      At 75% power (rpm/mph).................5600/59
      At 100% power (rpm/mph)...............6500/67

   FUEL FLOW:
      At 55% power (gpm/mi)......................4.1/63
      At 65% power (gpm/mi)......................4.8/65
      At 75% power (gpm/mi)......................5.6/63
      At 100% power (gpm/mi)....................7.4/54

   AIRSPEEDS:
      V_x (Best angle of climb)....................37 mph
      V_y (Best rate of climb).......................39 mph
      V_a (Design maneuvering).................64 mph
      V_ne (Never exceed)...........................75 mph
      V_s1 (Stall, power off)..........................32 mph
      V_s0 (Stall, flaps down, power off)............N/A
      Landing approach speed..................45 mph

      Kit Cost: ....................................Contact dealer for price

All specifications are based on manufacturers calculations.
SPECIFICATIONS SUBJECT TO CHANGE WITHOUT NOTICE.
This information is for reference only, please consult Quicksilver Mfg.® or one of it’s dealers for exact
and up to date specifications.

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