Atec 321 FAETA - Page 31

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 31 of 56
5.4. Altitude Loss by Stalling
Flap position (level flight)
Flap deflection
Altitude loss
I
10°
30 m 100 ft
II
20°
30 m 100 ft
III
35°
30 m 100 ft
0
0
30 m 100 ft
5.5. Take-off Distance up to 15m / 50ft
Engine
Rotax 912 iS Sport
Runway surface
Take-off distance
Asphalt
245 m 800 ft
Grass
265 m 870 ft
5.6. Rate of Climb - when speed of 110 km/h (59 kt)
Engine
Rotax 912 iS Sport
Solo flight
7,5 m/s 1476 ft/min 14,6 kt
472,5 kg
6,0 m/s 1182 ft/min 11,6 kt
5.7. Cruising Speeds
ROTAX 912 iS Sport
Air speed
km/h kt
RPM
1/min TP
Fuel consumption
l/h
120 65
3350 52%
5,4
140 76
3700 62%
7,0
160 86
4050 69%
8,0
180 97
4330 73%
9,4
200 108
4700 86%
12,1
220 119
5100 92%
14,7
240 130
5500 98%
18,4