Tecnam P2010 - Page 567

AFMS N° D08 FOR ALTERNATIVE AVIONICS CONFIGRATION AND
VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page GV 5-18
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
Ed. 1, Rev. 0