ALTO

The ALTO is an all-metal light sport aircraft certified in the UL and LSA categories. At present, over 120 of these aircraft fly in different countries such as USA, Brazil, South Africa, Spain and many more. The ALTO is specially suitable for flying training and recreational flying, due to its robust design and predictable flight characteristics.  

Wing

An extremely thorough test program means the ALTO is safe and predictable across the entire flight envelope. The wing is a semi-monocoque structure and is equipped with built-in tanks with a total capacity of 100 litres of fuel.

Fuselage 

The rear of the fuselage is designed with a rectangular cross section with an oval upper surface. The stiffness of the structure is assured by diagonal webs. The wing-fuselage link is completed by a dual spar and no less than fifteen precision fitted bolts.

Tail Surfaces 

The horizontal stabiliser and vertical tail surfaces are of a traditional arrangement. They are made as a riveted structure with composite fairings

Flight controls 

Flight control is by dual sticks and rudder pedals. The system uses heavy duty ball bearings which are strong and with no play - providing maximum feel while flying. There is easy access for both the aileron push rods and flap connection as well as the cables for elevator and rudder. Directional steering of the front landing gear leg is coupled with the pedals which allow a tight turning radius. The brakes are hydraulically controlled by a lever located on the center panel which simplifies flying, regular maintenance and operating cost.

Landing gear

The landing gear is strong yet light, with easy access for regular maintenance and inspection. The steerable nose wheel is directly connected to the rudder pedals for positive feel both in the air and on the ground. Small turn radius means manoeuvering on a tight apron is made with ease.

Cockpit

Access to the cockpit is secured by means of two foot steps located at the trailing edge of the wing. The spacious, 1.1 metre wide cockpit provides plenty of room for comfortable control of the aircraft. The cockpit canopy slides forward and is mounted on rails which allow the canopy to be removed for ease of maintenance.


​Performance & Dimensions

Vne (never exceed speed)
132 knots
Typical cruise TAS
40-110 knots
Stall TAS (landing configuration)
35 knots
Take-off roll
110 metres
Take-off to 50'
250 metres
Landing roll
91 metres
Landing from 50'
366 metres
Flap limit speed
70 knots
Best climb
 1020 feet per minute at 60 knots
MTOW (land plane)
600 kilos
Typical empty weight
310 kilos
Fuel capacity
92 litres usable
Carry including fuel
290 kg
Usable load after full fuel
219 kg
Cruise endurance (912ULS)
4.2 hours + 45 minutes reserve
Total fuel (2x wing tanks)
100 litres 
Wing span
8.2 metres
Length
6.14 metres
Height
2.26 metres
Main gear track
1.7 metres
Operational load limits
+4 -2 G
Tested at 650 kgs to
+6 -3 G
Luggage area limit
15kg

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    Doug King

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    Newtownards.

    Northern Ireland

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