Outside Air Temperature [°F]
Outside Air Temperature [°C]
Aircraft Weight [lbs]
-20
0
+20
+40
68
86 104
50
32
15
10.000 ft
pressure alt.
8.000 ft
pressure alt.
6.000 ft
pressure alt.
4.000 ft
pressure alt.
2.000 ft
pressure alt.
0 ft
Aircraft Weight [kg]
1600
1490
1380
725 700 675 650 650
Headwind
Component [kts]
0
5
10
15
0
5
10
15
Obstacle
Height [m]
[m]
[ft]
Obstacle Height [ft]
49
16
33
0
1000
900
800
700
600
500
400
300
200
[m]
[ft]
3200
2200
1200
3000
2000
1000
2800
1800
800
2600
1600
2400
1400
T
ake-Of
f Distance
Example:
- Pressure altitude: 3000 ft
- Outside temperature: 15° C (59° F)
- Weight : 725 kg(1598 lbs)
- Wind: 10 kts
Result:
- Take-Off roll distance: 312 m (1025 ft)
- Take-Off distance to clear a 15 m (50 ft) obstacle: 434 m (1425 ft)
DA20-100 ‘Katana’ 4X Manual
PERFORMANCE
5.3.5 TAKE-OFF DISTANCE
Conditions:
- Maximum take-off power
- Lift-off speed 53 KIAS and speed for climb over obstacle 57 KIAS
- Level runway, paved
- Wing Flaps T/O
Neither the software nor the documentation may
be used for real aviation and training purposes.
05<07
page
Summary of Contents for DA20-100
Page 1: ...MANUAL DA20 100 Katana ...
Page 2: ......
