Length 21 FT
Wingspan 27 FT
Wing area 114 SF
Height 7.5 FT
Cockpit width 4 FT
Number of seats 2
Fuel tank capacity 26 Gal.
Engine Rotax 912 ULS
Empty weight: 635 LBS
Maximum T/O weight 640 / 1320 LBS
VNE (Never EXCEED) 131 / 134 KTS
Cruising speed 107 KTS
Stall Speed, (UL/LSA) 35 / 41 KTS
Stall speed, C/C. (UL/LSA) 39 / 46 KTS
Load factor +4 / -2
Max climb speed (UL/LSA) 9 / 12 KTS call us specifications
At the moment over 80 of these all-metal aircraft fly in various countries such as USA, Brazil, South Africa, Spain and many more.
ALTO is especially suitable for recreational flying, mostly thanks to its robust design and predictable flight characteristics. For more info:
The principle lies in drilling holes for the connecting material already in the stage of metal cutting – milling process. The parts thus obtained are then passed on to other shaping operations – bending and forming. After the subsequent surface treatment, the parts are passed on to final assembly. The sophisticated Match Hole Technology system ensures that the individual parts fit together with a minimum of finishing operations.
The main advantage of this system lies in its effectiveness. Implementation of MHT drastically reduces production costs and times, eliminates the need to use complex tools/jigs to mount individual parts in assemblies and reduces the need for experienced personnel.
The advantages of this system will be appreciated especially by amateur builders, for whom the aircraft airframe assembly is very simple and comfortable.
The advantages of ALTO 912 TG lie in its simple and comfortable piloting, which is guaranteed by the design of the wing. The rectangular wing plan and profile that features a blunt leading edge that provides predictable stall characteristics and behavior. The wing is a semi-monocoque structure and is equipped with built-in tanks with a capacity of 26 gallons of fuel.
The rear of the fuselage of ALTO 912 TG is designed with a rectangular cross members with an oval upper surface. The stiffness of the structure is secured by diagonal web design. The wing-fuse link is conceived as the interconnection of the wing beams with the center of the airplane fastened by flange bolts.
The horizontal and vertical tail surfaces of ALTO 912 TG are of a traditional arrangement. They are made as a riveted structure with composite end arcs.
Flight control transmission from the "stick" is realized by means of rods and cables. Directional steering of the front landing gear leg is coupled with pedals for changing the aircraft direction. The brakes of ALTO 912 TG are hydraulically controlled by a lever located on the center panel.
The landing gear is designed as three-wheel, with front steering wheel. The main wheels are fixed to the fuselage on flexible laminate legs.
Access to the cockpit is secured by means of footpaths located at the trailing edge of the wing. The spacious, 110 cm wide cockpit of ALTO 912 TG provides plenty of room for comfortable control of the aircraft. The cockpit roof slides forward and it is mounted on rails.
At the customer's request, the dashboard can be made in the GLASS COCKPIT configuration!