MX II Sprint
Specifications:
Model |
Rotax 582 |
No. Cylinders |
2 |
Displacement |
580.7 cc |
Horsepower |
65 hp |
Recommended TBO |
300 hrs |
Propeller |
68" x 36" |
Length |
18 ft - 1/2 in |
Height |
9 ft - 1 in |
Wingspan |
32 ft - 7 in |
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 |
Takeoff distance, ground roll |
79 ft |
Takeoff distance, 50 ft obstacle |
202 ft |
Rate of climb |
1145 fpm |
Max level speed, sea level |
60 mph |
Landing distance, 50 ft obstacle |
240 ft |
Landing distance, ground roll |
75 ft |
Glide Ratio |
4.5:1 |
Minimum sink rate |
630 ft/min |
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At 55% power (rpm/mph) |
5300/42 |
At 65% power (rpm/mph) |
5600/50 |
At 75% power (rpm/mph) |
5900/56 |
At 100% power (rpm/mph) |
6500/60 |
At 55% power (gpm/mi) |
4.1/61 |
At 65% power (gpm/mi) |
4.8/63 |
At 75% power (gmp/mph |
5.6/60 |
At 100% power (gmp/mph) |
7.4/48 |
Vx (Best angle of climb) |
36 mph |
Vy (Best rate of climb) |
39 mph |
Va (Design maneuvering) |
64 mph |
Vne (Never exceed) |
75 mph |
Vs1 (Stall, power o°) |
27 mph |
Vs0 (Stall, flaps down, power o°) |
N/A |
Landing approach speed |
39 mph |
Contact local dealer or Quicksilver for Price |
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Features
- Six Month Limited Warranty (See Dealer For Details)
- 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
- 68" Propeller for More Power With Less Noise
- 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
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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 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 specications 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 specifications.