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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 UL 80 HP or ROTAX 912 SUL
100 HP
FITI three or two blade propeller ground adjustable.
6,2 m
2,0 m
9,6 m
10,1 m2
2
275 kg
175
kg
450 / 472,5 kg
70
l
x |
performance
(Rotax 912 ULS, 450 kg)
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
x
7 m/s
1375 FPM
255
km/h 138 kt
230 km/h 124 kt
x
x |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
275
km/h 148 kt
60
km/h 34 kt
x |
All specifications are based on manufacturer's
calculations
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