Pilot´s Operating Handbook of ATEC 322 Faeta LSA with otax 912iS engine
ATEC v.o.s. Libice nad Cidlinou, Czech epublic Page 6 of 56
1.3. Aircraft Description
ATEC 322 FAETA is the light sport aircraft, two-seater, cantilever, low-wing aircraft of all carbon
composite construction. The landing gear has a fixed tricycle gear with a steerable front wheel. The
power unit is of pulling configuration and consists of OTAX 912 iS Sport engine and of two-blade or
three-blade fix or ground adjustable FITI propeller.
1.4. Modifications and Changes
If the Manufacturer makes any structural or operational changes, which are 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. These documents will be published in ascending numerical series.
If the aircraft is sold to another person, the Manufacturer shall be announced about the name and
the address of the new owner.
1.5. Aircraft Technical Data
Dimensions
Wing span 31,5 ft
Length of fuselage 20,341 ft
Total height 6,562 ft
Wing area 108,7 sq ft
Depth of mean aerodynamic chord 3,648 ft
Span of horizontal tail surface 7,874 ft
Flap position I 10 ° 1,77 in
II 20 ° 3,54 in
III 35 ° 5,9 in
Aileron deflection up 20 ° 3,54 in
down 12 ° 2,16 in
Elevator deflection up 22 ° 3,15 in
down 18 ° 2,56 in
udder deflection L/ +-20° 7,09 in
Wing profile
oot area SM 701
End area SM 701
Landing Gear (tricycle with front wheel)
Wheel spacing 6,234 ft
Wheel base 4,742 ft
Front tire 4´´x 4´´
Main tire dimensions 6´´x 4´´
Tire pressure 23,2 psi
Suspension
Main gear composite springs
Front wheel rubber springs
