Quicksilver Aircraft
Quicksilver MX Sprint
Availability unconfirmedDocumented kit / materials package
Photos of the Quicksilver MX Sprint
Photos will appear here as reuse permissions are verified.Documented as a kit or construction-materials package. Current complete-kit availability is not established.
About the Quicksilver MX Sprint
Documented as a kit or construction-materials package. Current complete-kit availability is not established.
Engine: 1 Rotax Model 447 Twin Cylinder, Two Cycle 436.5 cc, 40 hp @ 6500 rpm
Manufacturer specification sheet. Cruise and range use the 75%-power sea-level row. Ground roll and total distance over a 50 ft obstacle are separate fields. Range reserve is not specified.
Specifications
| Seats | 1Source: Seats: 1 |
|---|---|
| Wingspan | 28 ftSource: Wingspan: 28 ft 0 in |
| Wing area | 156 sq ftSource: Wing area: 156 sq ft |
| Length | 18.08 ftSource: Length: 18 ft 1 in |
| Height | 8.83 ftSource: Height: 8 ft 10 in |
| Cabin width | |
| Cabin height | |
| Empty weight | 250 lbSource: Empty Weight: 250 lbs |
| Gross weight | 525 lbSource: Max takeoff weight: 525 lbs |
| Design gross weight | |
| Useful load | 275 lbSource: Useful load: 275 lbs |
| Useful load, published minimum | |
| Useful load, published maximum | |
| Fuel capacity | 5 US galSource: 5 U.S. gal |
| Optional fuel capacity | |
| Baggage capacity | |
| Engine power | 40 hpSource: PowerPlant: 1 Rotax Model 447 Twin Cylinder, Two Cycle 436.5 cc, 40 hp @ 6500 rpm |
| Suitable power, minimum | |
| Suitable power, maximum | |
| Published average build time | |
| Build time, minimum | |
| Build time, maximum |
Performance
| Top speed | |
|---|---|
| Cruise speed | 43.45 ktSource: At 75% power(5900 rpm): 50 mph/80 mi |
| Economy cruise speed | |
| Stall speed | 20.86 ktSource: Vs (Stall, power off): 24 mph |
| Stall speed, clean | |
| Never exceed speed | 56.48 ktSource: Vne (Never exceed).: 65 mph |
| Rate of climb | 900 ft/minSource: Rate of climb: 900 ft/min |
| Takeoff ground roll | 65 ftSource: Takeoff distance, ground roll: 65 ft |
| Takeoff distance, obstacle basis unspecified | |
| Landing ground roll | 60 ftSource: Landing distance ground roll (with brake): 60 ft |
| Landing distance, obstacle basis unspecified | |
| Ceiling | |
| Range | 69.52 nmiSource: At 75% power(5900 rpm): 50 mph/80 mi |
| Endurance | |
| Takeoff distance over 50 ft obstacle | 200 ftSource: Takeoff distance, 50 ft obstacle: 200 ft |
| Landing distance over 50 ft obstacle | 200 ftSource: Landing distance 50 ft obstacle (with brake): 200 ft |
Source notes & conditions
- Gallon capacities without an explicit US basis remain blank. Maximum operating altitude is not relabeled as service ceiling. Values from cruise and fuel-flow rows are kept distinct.