Atec 212 SOLO, Flight Manual

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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 582 UL DCDI 2V 65 HP
engine and a two-blade or three-blade 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 m
2
Depth of mean aerodynamic chord …………….. 1,032 m
Span of horizontal tail surface
…………….. 2,18 m
Flap position ……………………………………. I 10°
II 20°
III 35°
Airfoil Section
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 …………………………………….. 0,12 MPa / 1,2 atp
Springing system
Main wheels …………………………….. composite spring
Tail wheel …………………………….. composite spring
Brakes
……………………………………. Main wheels hydraulic disc brakes
Rescue System installed / not installed……….
Weights
Empty weight ……………………………………..
kg
Maximum take-off weight
…………………….. 300 315 kg