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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
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