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Doc. No. 6.01.05-E Revision 1 03-Mar-2003 Page 5 - 2
5.3 PERFORMANCE TABLES AND DIAGRAMS
5.3.1 AIRSPEED CALIBRATION
180 170 160 150 140 130 120 110 100 90 80 70 60 50 40
KCAS
40 50 60 70 80 90 100 110 120 130 140 150 160 170 180 KIAS
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Doc. No. 6.01.05-E Revision 1 03-Mar-2003 Page 5 - 3
5.3.2 DIAGRAM FOR SETTING ENGINE PERFORMANCE
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5.3.3 PRESSURE ALTITUDE -DENSITY ALTITUDE
Conversion from pressure altitude to density altitude.
pressure altitude [m]
14000 4000
density alt. [ft]
1500 4000 1000
density alt. [m]
2000 500
0 0
[°C] [°F]
4000
3500
3000
2500
12000
8
000
3500
10000
3000
2000
6000
2500
80001500
4000
2000
6000
1000
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Doc. No. 6.01.05-E Revision 1 03-Mar-2003 Page 5 - 5
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Doc. No. 6.01.05-E Revision 3 26-May-2003 Page 5 - 6
5.3.5 STALLING SPEEDS
Mass: 980 kg (2161 lb) Airspeeds in KIAS
Mass: 1150 kg (2535 lb) Airspeeds in KIAS
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Doc. No. 6.01.05-E Revision 3 26-May-2003 Page 5 - 7
5.3.6 WIND COMPONENTS
Example: Flight direction : 360°
Wind : 32°/30 kts
Result: Crosswind component : 16 kts
Max. demonstrated crosswind component : 20 kts
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Doc. No. 6.01.05-E Revision 3 26-May-2003 Page 5 - 8
5.3.7 TAKE-OFF DISTANCE
Conditions: -Power lever ............... MAX
-Flaps .................... T/O
-Nose wheel lift-off .......... at vR = 59 KIAS (1150 kg, 2535 lb)
at vR = 55 KIAS (1000 kg, 2205 lb)
at vR = 49 KIAS (850 kg, 1874 lb)
- Airspeed for initial climb ...... 66 KIAS (1150 kg, 2535 lb)
60 KIAS (1000 kg, 2205 lb)
54 KIAS (850 kg, 1874 lb)
-Runway .................. level, asphalt surface
WARNING
On grass strips, depending on the characteristics of the surface (length of the grass, softness of the ground) allowance must be made for a take-off roll which is at least 20 % longer. The take-off distance values given do not include any kind of safety margin. A poorly maintained airplane, deviation from the prescribed procedures and unfavorable external factors (rain, cross-wind, wind shear, uneven terrain and in particular tufts of grass) can all lead to a considerable increase in the take-off distance.
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