Sport 2S Specifications - R582:  POWERPLANT PowerPlant Rotax 582 No. Cylinders 2 Displacement 580.7 cc Horsepower 65 hp Recommended TBO 300 hrs Propeller 68" in x 36" in Length 18ft 3in Height 8ft 1/2 in Wingspan 30 ft 11 in Wing area 174.1 sq ft Wing loading 5.74 lb/sq ft Power loading 15.38 lb/hp Seats 2 Minimum weight crew 1 Empty Weight 444 lb Useful load 556 lb Payload w/full fuel. 520 lb Max takeoff weight 1000 lb Fuel capacity 6 U.S. gal  AIRSPEEDS Vx (Best angle of climb) 43 mph Vy (Best rate of climb) 45mph Va (Design maneuvering) 70 mph Vne (Never exceed). 80 mph Vs1 (Stall, power off) 38 mph Vs0 (Lading, approach speed) 49 mph    PERFORMANCE Takeoff distance, ground roll 250 ft Takeoff distance, 50 ft obstacle 660 ft Rate of climb 500 ft/min Max level speed, sea level 68 mph Landing distance, 50 ft obstacle 580 ft Landing distance, ground roll 280 ft Glide Ratio 5.5:1 Minimum sink rate 660 ft/min  CRUISE PERFORMANCE CHART At 55% power (5300 rpm/mph) 51 mph At 65% power (5600 rpm/mph) 55 mph At 75% power (5900 rpm/mph) 59 mph At 100% power (6500 rpm/mph) 68 mph  FUEL FLOW  At 55% power (gpm/mi) 4.5/68 At 65% power (gpm/mi) 5.0/66 At 75% power (gpm/mi) 5.6/63 At 100% power (gpm/mi) 7.5/54  KIT COST Contact local dealer or Quicksilver for Price

Features Dual CDI Electronic Ignition Dual Carburetor Engine Rugged Aluminum Steerable Nose Wheel Main Wheel Brakes Double Surface Wings with Streamlined Struts Extra ribs with Mylar Leading Edge Insert for Extra Firm Airfoil Increased Max Takeo Weight of 1000 lbs. Conventional 3-Axis Controls 68" Propeller Wider Tail Boom Accommodates up to 72" Prope Even Wider Cockpit for Greater Pilot Comfortller

Inflight Adjustable Trim Control Tapered Stabilizer Tubular-Braced Tail Excellent Crosswind Capability Easy Handling and Responsive Control Short Take-o and Landing Quick Breakdown for Transport Quicksilvers Famous Quality Easy-to-Assemble Kit (Average 40 to 60 Hours) Airspeed Indicator Included Six-Month Written Warranty (See Dealer for Details)

NOTE: All specifications are based on manufacturer's calculations.
All performance figures are based on standard day, standard atmosphere, at sea level and 465 lb. crew weight,
unless otherwise noted.
The performance shown reects 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

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