Welcome to the home of Alto New Zealand, exclusive distributors of ALTO NG aircraft in New Zealand and the South Pacific.
Our mission is to sell ALTO NG, safe, new two-seat single-engine, light sports low wing propelled aircraft with the support of Direct Fly s.r.o.
Single-engine, two seat, self-supporting monoplane. The aircraft was designed as a simple all-metal design suitable for assembly in amateur conditions, yet providing sufficient performance, corresponding to the standards in this category, low maintenance costs and easy and comfortable flight control. The aircraft is equipped with a proven ROTAX 912 ULS engine, providing sufficient power in its category. GALAXY GRS rescue system and glider tow can be installed upon request.
Alto has an elegant appearance with a smooth transition between the fuselage and the cabin. with the related lengthening of the engine deck, the engine has moved forward. With a total luggage locker capacity, which is 15 kg.
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Our Product
Alto has an elegant appearance with a smooth transition between the fuselage and the cabin. with the related lengthening of the engine deck, the engine has moved forward. The luggage locker capacity is 15 Kg.
Motor devices
Tachometer, cylinder head temperature indicator, electric fuel gauges, oil temperature indicator, oil pressure indicator, fuel pressure indicator, carburetor preheat indications.
GLASS COCKPIT
At the customer’s request, the instrument panel can be made in GLASS COCKPIT configuration.
Flight instruments
Speedometer, altimeter, vario, compass, transverse inclinometer
The only place where you’ll get the perfect solution for all your needs.
Engine Installations
The aircraft presents an excellent solution for engine and oil cooling, as well as cabin heating and engine supercooling in the winter months. All this thanks to the shape of the engine cover and its internal structure: carburetor air intake and cylinder deflector. The airbox stabilizes the air between both carburetors, helping the engine run quieter, and the ram air intake provides plenty of air for the otherwise non-supercharged engine. In cooperation with the oil and water thermostat, and the choice between three sizes of oil coolers, the engine does not overheat during ascent or overcool during descent.
Engine
Alto NG has a reinforced front leg fixing on the engine partition with rivets that allows a greater load capacity.
On the fuselage, on top of the skin and below the windows, it has stringers to increase the stability of the skin. The VD speed of 159 Knots., in connection with that, the control stiffness is higher, which contributes to the reduction of the force of the control lever during taxiing, which provides a better response of the force during maneuvering and better adjustability in landing configurations.
Flight Control
With the new Alto NG, control rigidity has been increased by changing the concept of flight control, from the control stick to the control surface. For pitch control it features a system of drawbars, levers and rockers, allowing faster and more precise control of the aircraft with quick response for the pilot. The entire control system is connected by bolts fitted with cotter pins.
Possibilities
Inside, there is also the flap controller and a START button fuel valve, where it is mechanically impossible to start the engine with the fuel valve closed. No need to think about which tank to pump fuel from first when both tanks are full. It is possible to pump from any tank the pilot chooses because unused fuel returns to the tank they are pumping from.
Our Contributions
The only place where you’ll get the perfect solution!
Technical Specification
| Lenght | 6,15 m |
| Wingspan | 8,20 m |
| Height | 2,25 m |
| Cockpit Width | 1,10 m |
| Wing Area | 10,5 m2 |
| Number of seats | 2 |
| Load Factor | +4 / -2 |
| Fuel tank capacity | 100 Lt |
| Take-off distance to 50ft | 410 m |
| Landing distance to 50 ft | 295 m |
| Maximum take-off weight | 600 Kg |
| VNE (never exceeded speed) | 131 Kts |
| Stalling speed, landing configuration | 41 Kts |
| Stalling speed, clean configuration | 46 Kts |
| Maximum rate of climb | 1000 ft /min |
| Crusing Speed | 107 Kts |
