Tecnam P2010 - Page 307

AFMS N°D02 FOR VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page V5-18
12. BALKED LANDING PERFORMANCE
To account for likely in service performance variations apply a
factored to rate of climb and to angle of climb of 0.90
Throttle and Propeller Lever: Full Forward
Flaps: LAND
Speed:
67 KIAS
Weight
Pressure
Altitude
Steady Gradient of Climb [%]
Temperature [°C]
ISA
[kg]
([lb])
[ft] -25 0 25 50
1160
(2557)
S.L. 10.9 8.6 6.6 4.7 7.4
1000 10.0 7.8 5.7 3.9 6.7
2000 9.2 6.9 4.9 3.1 6.0
3000 8.3 6.1 4.1 2.3 5.3
4000 7.4 5.2 3.2 1.4 4.6
5000 6.6 4.4 2.4 0.6 3.9
6000 5.7 3.5 1.6 -0.2 3.3
7000
4.8
2.7
0.7
-1.0
2.6
1060
(2337)
S.L. 12.9 10.4 8.1 6.1 9.0
1000 11.9 9.4 7.2 5.2 8.3
2000 11.0 8.5 6.3 4.3 7.5
3000 10.0 7.6 5.4 3.4 6.8
4000 9.1 6.7 4.5 2.5 6.0
5000 8.1 5.7 3.6 1.7 5.3
6000 7.2 4.8 2.7 0.8 4.5
7000
6.2
3.9
1.8
-0.1
3.8
960
(2116)
S.L. 15.2 12.4 10 7.7 10.9
1000 14.1 11.4 9.0 6.7 10.1
2000 13.1 10.4 7.9 5.8 9.3
3000 12.0 9.3 6.9 4.8 8.4
4000 11.0 8.3 5.9 3.8 7.6
5000 10.0 7.3 4.9 2.8 6.8
6000
8.9
6.3
3.9
1.8
6.0
7000
7.9
5.3
2.9
0.9
5.2
NOTE
Section 5 - Performances
BALKED LANDING PERFORMANCE
2
nd
Edition, Rev. 0