Atec 321 Faeta

The ATEC 321 FAETA is an aerodynamically refined cantilever low-winged all composite aircraft with a high content of carbon fibre. It can be supplied as an ultralight. Fitted with slotted flaps, it is capable of very low speed and is equipped with a ballistic parachute.

The standard engine option is a ROTAX 912 UL 80 HP or ROTAX 912 SUL 100 HP that drives a FITI three or two blade propeller ground adjustable.

specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range
ROTAX 912 ULS
x
6.2 m
2.0 m
9.6 m
10.1 m2
x
275 kg
175 kg
450 / 472.5 kg
70 litres
x

performance

takeoff distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling
x
1375 fpm
x
124 kt
x
x

limiting and recommended speeds

design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed
x
148 kt
34 kt
x

All specifications are based on manufacturer's calculations