POWERPLANT:
      PowerPlant.........................1 Rotax Model 447
      .................................Twin Cylinder, Two Cycle
      ...........................436.5 cc, 40 hp @ 6500 rpm
      Recommended TBO...............................250 hr
      Propeller........................................66 in x 34 in
      Length.................................................18 ft 1 in
      Height.................................................8 ft 10 in
      Wingspan............................................28 ft 0 in
      Wing area...........................................156 sq ft
      Wing loading..................................3.36 lb/sq ft
      Power loading.................................13.12 lb.hp
      Seats..............................................................1
      Minimum flight crew........................................1
      Empty weight...........................................250 lb
      Useful load...............................................275 lb
      Payload w/full fuel....................................245 lb
      Max takeoff weight..................................525 lb
      Fuel capacity.....................................5 U.S. gal

   PERFORMANCE:
      Takeoff distance, ground roll......................65 ft
      Takeoff distance, 50 ft obst......................200 ft
      Rate of climb......................................900 ft/min
      Max level speed, sea level......................54 mph
      Max operating altitude.........................14,000 ft
      Landing distance
           50 ft obstacle (with brake)...................200 ft
      Landing distance
          ground roll (with brake)..........................60 ft

   CRUISE PERFORMANCE CHART:
   (Speed/Range at sea level with
          4.8 gal. usable fuel)
  @ 55% power(5000 rpm)...............44 mph/84 mi
  @ 65% power(5300 rpm)...............47 mph/84 mi
  @ 75% power(5500 rpm)...............50 mph/80 mi
  @ 100% power(6500 rpm).............54 mph/52 mi                  

   FUEL FLOW:
      @ 55% power ....................................2.5 gph
      @ 65% power ....................................2.7 gph
      @ 75% power ....................................3.0 gph
      @ 100% power ..................................4.5 gph

   LIMITING AND RECOMMENDED

• Rotax 447 Engine
  
• Conventional 3-Axis Controls
  
• 66" Propeller for More Performance With Less Noise
  
• Flexible Driveshaft Coupler for Reduced Vibration
  
• Tapered Stabilizer
  
• Tubular-Braced Tail
  
• Triangulated Kingpost Assembly
  
• Partial Double Surface Wings
  
• Extra Ribs for Firm Airfoil
  
• Excellent Crosswind Capability
  
• Short Takeoff
  
• Very Fast Control Response
  
• Quicksilver's Famous Quality
  
• Easy-to-Assemble Kit (Average 30 to 40 Hours)
  
• 6-Month Written Warranty (See Dealer for Details)
  

All specifications are based on manufacturer's calculations.
All performance figures are based on standard day,
standard atmosphere, at sea level and 175 lb. pilot
weight, unless otherwise noted.
Operations/equipment category reflects this aircraft's
maximum potential.
The empty weight is approximate due to 6% Mil Spec
tolerance on materials.
NOTE: Specifications and equipment subject to
change without notice.
Only Quicksilver Manufacturing approved
accessories should be installed on this aircraft.
This aircraft is not designed for aerobatics.
Be sure to follow the owners manual recommendations
for flight and maintenance guidelines.
The pilot is responsible for operating this aircraft in
accordance with the applicable Federal and State Regulations.

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