SECTION 2 / PERFORMANCE
At the MTOW (Maximum Take-Off Weight) of 450 kg
DYNAMIC 450 Wing
Standard Conditions 15°C - 1013,2 hPa
Engine Type
Rotax 503
Rotax 582
Hirth 3701ES
Rotax 912
Rotax 912S
Rated Engine Power
37 kW
48 kW
74 kW
59,6 kW
73,5 kW
Maximum Weight
450 kg
450 kg
450 kg
450 kg
450 kg
Stalling speed (VSO)
62 km/h
62 km/h
62 km/h
62 km/h
62 km/h
Maximum Shown speed
177 km/h
177 km/h
177 km/h
177 km/h
177 km/h
Maximum speed Never exceed (VNE)
160 km/h
160 km/h
160 km/h
160 km/h
160 km/h
Maximum speed of operation (VA)
110 km/h
110 km/h
110 km/h
110 km/h
110 km/h
Maximum speed in turbulent air (VC)
110 km/h
110 km/h
110 km/h
110 km/h
110 km/h
Horizontal maximum speed (VH)
115 km/h
126 km/h
138 km/h
130 km/h
138 km/h
Landing distance
70 m
70 m
70 m
70 m
70 m
Landing distance from 15 m
190 m
190 m
190 m
190 m
190 m
Minimum rate of fall
3 m/s
3 m/s
3 m/s
3 m/s
3 m/s
Speed of minimum rate of fall
70 km/h
70 km/h
70 km/h
70 km/h
70 km/h
Glide ratio
6,5
6,5 6,5 6,5 6,5
Take-off Roll
85 m
80 m
70 m
75 m
70 m
Take-off Distance to 15 m
210 m
190 m
170 m
180 m
170 m
Rate of rise at 75 km/h
2,5 m/s
3,5 m/s
4,5 m/s
4 m/s
4,5 m/s
Roll Rate (45°/45°) at 75 km/h
3,5 s
3,5 s
3,5 s
3,5 s
3,5 s
Roll Rate (45°/45°) at VA
3 s
3 s
3 s
3 s
3 s
Cross-wind Limit
20 km/h
20 km/h
20 km/h
20 km/h
20 km/h
The performance data indicated are average performances. The model of airframe and the
presence of fairing can modify the data slightly.
MAUT – EN DYN 450
Edition : June 2005
Section : 2 - 01
