Tecnam P2010 - Page 485

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV5 - 18
Section 5 – Performance-
BALKED LANDING PERFORMANCE
Ed. 1, Rev.0
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