SPECIFICATIONS:
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.....................................254 lb
Useful load.........................................271 lb
Payload w/full fuel..............................241 lb
Max takeoff weight............................525 lb
Fuel capacity...............................5 U.S. gal
PERFORMANCE:
Takeoff distance, ground roll..............75 ft
Takeoff distance, 50 ft obst..............250 ft
Rate of climb...............................850 ft/min
Max level speed, sea level............58 mph
Max operating altitude.................14,000 ft
Landing distance, 50 ft obst.............300 ft
Landing distance, ground roll.............70 ft
CRUISE PERFORMANCE CHART:
(Speed/Range at sea level)
@ 55% power(5000 rpm).......45 mph/90 mi
@ 65% power(5300 rpm).......49 mph/91 mi
@ 75% power(5500 rpm........53 mph/88 mi
@ 100% power(6500 rpm).....59 mph/65 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
SPEEDS:
Vx (Best angle of climb)................34 mph
Vy (Best rate of climb)...................37 mph
Va (Design maneuvering).............54 mph
Vne (Never exceed).......................74 mph
Vs (Stall, power off)........................27 mph
Landing approach speed (1.3 Vs)...........
...........................35 mph
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FEATURES:
- 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
- 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)
PRICES SUBJECT TO CHANGE WITHOUT NOTICE
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 Mfg. 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.
Range is listed in statute miles
with no allowance for wind or fuel reserve.
*All performance figures are based on standard
day, standard atmosphere, at sea level, and
aircraft at 525 pounds take-off weight.
These distances must be increased equal to 20%
for each one thousand feet of pressure altitude
above sea level.
**The empty weight is approximate due to a
4% Mil. Spec. tolerance on materials.
Weight shown is minimum empty weight. |