Atec ATEC 212 SOLO ROTAX 912 UL Description of the Aeroplane, Specification Dimensions, Brakes

1.3.Description of the Aeroplane

ATEC 212 SOLO is an ultralight single-seater cantilever low-wing aircraft of an all carbon composite construction. It is equipped with a tail landing gear with the steerable tail wheel. The power plant is a pull arrangement and consists of a ROTAX 912 UL 80 HP engine and a two-blade or three-blade fix or ground adjustable propeller FITI.

1.4.Specification

Dimensions
Wing span	…………………………………….			7,48 m
Length of fuselage		…………………………….		5,2 m
Total height	…………………………………….			1,4 m
Wing area	…………………………………….			7,27 m2
Depth of mean aerodynamic chord			……………..	1,032 m
Span of horizontal tail surface			……………..	2,18 m
Flap position ……………………………………. I					10°
				II	20°
Airfoil Section				III	35°
Root section	…………………………………….. SM 701
End section	…………………………………….. SM 701
Tail Wheel Landing Gear
Wheel spacing…………………………………….. 1,56 m
Wheel base	…………………………………….. 3,66 m
Tyre dimensions		…………………………….. 350 * 120
Tyre pressure …………………………………….. 0,16 MPa / 1,6 atp
Springing system
Main wheels		…………………………….. composite spring
Tail wheel		…………………………….. composite spring
Brakes	……………………………………. Main wheels hydraulic disc brakes
Rescue System installed / not installed……….				GRS 6/360
Weights
Empty weight ………………………………………………….						kg
Maximum take-off weight ………………………………….						300 kg
Maximum take-off weight including rescue system installed …						315 kg
Maximum weight of luggage in luggage space					…	5 kg

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