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Ultralights
and Sport Planes by QuickSilver
7 models
to choose from for the perfect plane for you!
Ultralights
USA
Ultralights
USA is A QuickSilver Dealer & Training Center
staffed
by ASC instructors. Ultralights USA offers assembly
and service.
Contact us for configuration and pricing
MX II Sprint
Features:
- Dual CDI Electronic Ignition, Dual Carburetor Engine
- Steerable Nose Wheel Standard
- Main Wheel Brakes
- High Lift, Partial Double Surface Wings
- Extra Ribs for Firm Airfoil
- Conventional 3-Axis Controls
- Easy Handling and Responsive Control
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- 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
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- Short Takeoff and Landing
- Quicksilver's Famour Quality
- Easy-to-Assemble Kit
(Ultralights USA offers assembly service)
- Airspeed Indicator Included
- Six-Month Written Limited Warranty
(Ask us about it!)
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Standard
Configuration
| Airframe |
R503 |
R582 |
| Length |
216.5 in. |
216.5 in. |
| Height |
109 in. |
109 in. |
| Wingspan |
32 ft - 7 in |
32 ft - 7 in |
| Wing Area |
180 sq.
ft. |
180 sq.
ft. |
| Wing Loading |
4.0 lb/sq
ft |
4.0 lb/sq
ft. |
| Power Loading |
14.4 lb/hp |
11.25 lb/hp |
| Seats |
2 |
2 |
| Minimum
flight crew |
1 |
1 |
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-
Strut Braced Wing
| Weights |
R503 |
R582 |
| Max takeoff
weight |
720 lbs. |
720 lbs. |
| Empty weight |
325 lbs. |
330 lbs. |
| Useful
load |
395 lbs. |
390 lbs. |
| Payload
w/full fuel |
359 lbs. |
354 lbs. |
| Fuel Capacity |
6 U.S. gal. |
6 U.S. gal. |
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Specifications
subject to change without notice.
NOTE: All
specifications are based on manufacturer's calculations.
| PERFORMANCE: |
R503 |
R582 |
| Takeoff
distance, ground roll |
102 ft |
79 ft |
| Takeoff
distance, 50 ft obstacle |
352 ft |
202 ft |
| Rate of
climb |
595 fpm |
1145 fpm |
| Max Level Speed, sea level |
55 mph |
60 mph |
| Landing
distance, 50 ft obstacle |
240 ft |
240 ft |
| Landing
distance, ground roll |
75 ft |
75 ft |
| Glide Ratio |
4.5:1 |
4.5:1 |
| Minimum
sink rate |
630 fpm |
630 fpm |
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| CRUISE
PERFORMANCE CHART: |
R503 |
R582 |
| At 55%
power (rpm/mph) |
5000/39 |
5000/42 |
| At 65%
power (rpm/mph) |
5300/46 |
5300/50 |
| At 75%
power (rpm/mph) |
5600/51 |
5600/56 |
| At 100%
power (rpm/mph) |
6500/55 |
6500/60 |
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| FUEL FLOW: |
R503 |
R582 |
| At 55%
power (gpm/mi) |
3.2/73 |
4.1/61 |
| At 65%
power (gpm/mi) |
3.8/72 |
4.8/63 |
| At 75%
power (gpm/mi) |
4.4/69 |
5.6/60 |
| At 100%
power (gpm/mi) |
5.8/56 |
7.4/48 |
All performance
figures are based on standard day, standard atmosphere, at sea
level and
175 lb. pilot weight, unless otherwise noted. Flight training required.
| AIRSPEEDS: |
R503 |
R582 |
| Vx (Best
angle of climb) |
36 mph |
36 mph |
| Vy (Best
rate of climb) |
39 mph |
39 mph |
| Va (Design
maneuvering) |
64 mph |
64 mph |
| Vne (Never
exceed) |
75 mph |
75 mph |
| Vs1 (Stall, flaps up,
power off) |
27 mph |
27 mph |
| Vs0 (Stall,
flaps down, power off) |
N/A |
N/A |
| Landing
approach speed |
39 mph |
39 mph |
| SPECIFICATIONS: |
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| Powerplant
ROTAX |
503 |
582 |
| No.
Cylinders |
2
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2
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| Displacement |
496.7
cc
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580.7
cc
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| Horsepower |
50
hp
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64
hp
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| Recommended
TBO |
250
hrs
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250
hrs
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| Propeller |
68" x 32"
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68" x 36"
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All specifications
are based on manufacturers calculations.
SPECIFICATIONS
SUBJECT TO CHANGE WITHOUT NOTICE.
This information
is for reference only, please consult
Ultralights
USA for exact and up to date specifications.
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