The MX II Sprint’s simple design and bolt together construction make preflight inspections and routine maintenance a breeze. And as with all other Quicksilvers, its true assembly-style kit will have you flying in days, not weeks or months. MX II Sprint SPECIFICATIONS POWERPLANT Model Rotax 582 No. Cylinders 2 Displacement 580.7 cc. Aeromarine LSA, Merlin PSA Assembly Manual HV105/103, Revision '0', dated 4/25/17. MX II Sprint (PDF) Sept 2012: Quicksilver MX II Sprint Packing Lists: 99315. Tc40d Manual quicksilver mx ii sprint assembly manual new holland tc40d, used new holland tc40d, new 110 tractor owners manual new holland tc35, tc35d, tc40, tc40d, tc45, tc45d oem service manual premium compact new holland tc40d manual service, repair & owners ford f350 super duty repair manual new holland tc40d operators manual service, repair. Two Place Quicksilver Aircraft Performance and Specifications: NOTE: There will be a price increase on the Rotax motors, beginning Soon. Order NOW if you want to beat that increase. Fuel Capacity (gal.) Performance Specifications for MX II Sprint and MXL II Sport are shown for Rotax 582 motor. Rotax 503 powerplant option is available. The MX Sprint has extremely fast roll response and handles crosswinds easily with its conventional three-axis controls. Yet it retains the docile and predictable slow flight characteristics that made the original MX famous.
- Quicksilver Mx Ii Sprint Assembly Manual Free
- Quicksilver Mx Ii Sprint Assembly Manual Pdf
- Quicksilver Mx Assembly Manual
Quicksilver Mx Ii Sprint Assembly Manual Free
| Specification | MX II Sprint | MXL II Sport | Sport 2S | Sprint 2S | GT 500 (582) | GT 500 (912) |
| Horsepower | 64 | 64 | 65 | 65 | 65 | 80 |
| TBO Hours | 250 | 250 | 250 | 250 | 250 | 1000 |
| Propeller | 66 X 36 | 66 X 36 | 68 X 36 | 68 X 36 | 72' Carbon Fiber | 72' Carbon Fiber |
| Length | 18' 1/2' | 18' 1/2' | 18' 3' | 18' 3' | 20' 5' | 20' 5' |
| Height | 9' 1' | 9' 1' | 8' 1/2' | 8' 1/2' | 6' 6' | 6' 6' |
| Wingspan | 32' 7' | 32' 9' | 30' 11' | 30' | 30' | |
| Wing Area | 180 sq. ft. | 180 sq. ft. | 174 sq. ft. | 155 sq. ft. | 155 sq. ft. | |
| Wing Loading | 4.0 lb/sq ft | 4.0 lb/sq ft | 5.74 lb/sq ft | 6.45 lb/sq ft | 7.09 lb/sq ft | |
| Power Loading | 11.25 lb/hp | 11.25 lb/hp | 15.38 lb/hp | 15.38 lb/hp | 13.75 lb/hp | |
| Empty Weight (lbs.) | 330 | 335 | 430 | 575 | 638 | |
| Useful Load (lbs.) | 390 | 385 | 570 | 425 | 462 | |
| Payload w/ Full Fuel | 354 | 349 | 534 | 329 | 366 | |
| Max Takeoff Weight | 720 | 720 | 1000 | 1000 | 1100 | |
| Fuel Capacity (gal.) | 6 | 6 | 6 | 6 | 16 | 16 |
| Takeoff Distance, Ground Roll (ft.) | 79 | 121 | 240 | 220 | 244 | |
| Takeoff Distance, 50' Obstacle | 202 | 260 | 660 | 689 | 621 | |
| Rate of Climb (ft/min) | 1145 | 1145 | 500 | 650 | 655 | |
| Max Level Speed (sea level) (mph) | 60 | 67 | 69 | 81 | 88 | |
| Landing Distance, With Brake (ft) | 75 | 75 | 220 | 260 | 390 | |
| Landing Distance, 50'Obstacle | 240 | 300 | 484 | 580 | 905 | |
| Glide Ratio | 4.5 : 1 | 5.0 : 1 | 5.5 : 1 | 7.0 : 1 | 6.5 : 1 | |
| 55% Power, 5300 RPM (mph) | 42 | 43 | 55 | 68 | 4500 RPM = 70 | |
| 65% Power, 5600 RPM (mph) | 50 | 52 | 58 | 72 | 4800 RPM = 75 | |
| 75% Power, 5900 RPM (mph) | 56 | 59 | 61 | 75 | 5000 RPM = 78 | |
| 100% Power, 6500 RPM (mph) | 60 | 67 | 69 | 83 | 5500 RPM = 86 | |
| 55% Power, (miles) | 61 | 63 | 73 | 240 | 300 | |
| 65% Power, (miles) | 63 | 65 | 69 | 225 | 280 | |
| 75% Power, (miles) | 60 | 63 | 65 | 215 | 255 | |
| 100% Power, (miles) | 48 | 54 | 53 | 175 | 215 | |
| Best Angle of Climb (mph) | 36 | 37 | 38 | 47 | 50 | |
| Best Rate of Climb (mph) | 39 | 39 | 40 | 55 | 58 | |
| Maneuvering Speed (mph) | 64 | 64 | 70 | 90 | 94 | |
| Never Exceed Speed (mph) | 75 | 75 | 87 | 103 | 103 | |
| Stall, Power Off (mph) | 27 | 32 | 35 | 39 | 42 | |
| Landing Approach Speed (mph) | 39 | 45 | 46 | 51 | 55 |
Quicksilver Mx Ii Sprint Assembly Manual Pdf
The Quicksilver design, and manufacturing process were so far ahead of their time, that even today nearly 30 years later they are still the marker that others try to meet. Whether it is the simple bolt together construction, step by step assembly manuals, production methods, dealer network or quality of design, only a select few have been able to follow in the trail that the Quicksilver made.
The Quicksilver MX series was first introduced in the late 70's as a weight shift. The control system featured a sling style seat for pitch control with a set of control cables (actually string) running out to the wings and then going to the rudder for turning.
Power was originally supplied by a single cylinder Yamaha go cart engine, sitting above the wing, with a drive shaft running to the back of the root tube where it came into a belt reduction drive.
Around 1979 the power pack was updated to the 430 Cuyuna, which was mounted below the wing. Then in 1980 the Quicksilver revolutionized the sport of ultralight aviation with the introduction of the Quicksilver MX. It was literally the first ultralight that a pilot could now sit in with a control stick, and rudder pedals.
While not true three axis control, it dihedral in the wings to allow for coordinated turns. It also had spoilerons which could be used to kill lift on a wing which aided in turning or with both spoilerons deployed lift could be lost for loosing altitude quickly.
Quicksilver also came out with a Yoke, or steering wheel style control system. Here the forward and back movement of the stick controlled pitch while turning the wheel or yoke left and right turned the rudder.
The next major change was the introduction of the Quicksilver MX 11. The first real two place ultralight trainer on the market. The MX 11 featured side by side seating, a center control stick, with dual throttles located on the outboard side of each seat. The only problem was POWER - the 430 Cuyuna was just not powerful or reliable enough.
Quicksilver Mx Assembly Manual
Thus the introduction of the Rotax 377 for the single place MX and the Rotax 503 for the two place.