Flight and Operations Manual of ATEC 321 Faeta ultralight aircraft with Rotax 912 iS Sport
ATEC v.o.s. Libice nad Cidlinou, Czech Republic Page 6 of 56
1.3. Aircraft Description
ATEC 321 FAETA is an ultralight, two-seater, cantilever, low-wing aircraft of all carbon composite
construction. The landing gear is a fixed tricycle undercarriage with a steerable nose wheel. The
propulsion unit is in pulling configuration and consists of ROTAX 912 iS Sport engine and of two- or
three- blade fix or ground adjustable FITI propeller.
1.4. Modifications and Changes
If the Manufacturer makes any structural or operation changes necessary to be advised to the owner,
the related documentation will be delivered to the owner, who is obliged to record them into this
Manual. Such documents are published in ascending numerical series.
If the aircraft is sold to another person, the Manufacturer shall be announced about the name and
contact information of the new owner.
1.5. Aircraft Technical Data
Dimensions
Wing span 9,6 m
Length of fuselage 6,2 m
Total height 2,0 m
Wing area 10,1 m
2
Depth of mean aerodynamic chord 1,11 m
Span of horizontal tailplane 2,4 m
Flap position I 10 ° 45 mm
II 20 ° 90 mm
III 35 ° 150 mm
Aileron deflection up 20 ° 90 mm
down 12 ° 55 mm
Elevator deflection up 22 ° 80 mm
down 18 ° 65 mm
Rudder deflection L/R +-20° 180 mm
Airfoil Section
Root section SM 701
End section SM 701
Landing Gear (tricycle with nose gear)
Wheel spacing 1,9 m
Wheel base 1,4 m
Tyre dimensions (main wheels) 350 x 120 mm
Tyre dimensions (nose wheel) 300 x 100 mm
Tyre pressure 0,16 MPa / 1,6 atp
Suspension
Main gear composite springs
Nose gear rubber springs
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