Tecnam P2010 2015 - 12. Balked Landing Performance

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
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12. BALKED LANDING PERFORMANCE
To account for likely in service performance vari at ions apply a
factored lo rate of climb and to angle of climb of0 .90
Throttle and Propeller Lever : Full Forward
Flaps: LAND
Speed: 67 KIAS
Pressure
Steady Gradient of Climb [%)
Weight
[kg]
([lb])
1160
(2557)
1060
(2337)
960
(2116)
Altitude
Temperature ["CJ
[ft] -25
0
25
S.L. 10 .9 8.6 6.6
1000 10.0 7.8 5.7
2000 9.2
6.9
4.9
3000 8.3
6.1
4.1
4000 7.4
5.2
3.2
5000 6.6 4.4 2.4
6000 5.7 3.5 1.6
7000
4.8 2.7
0.7
S.l.
12.9
10.4 8.1
1000 11.9
9.4
7.2
2000 11 .0
8.5
6.3
3000
10.0
7.6
5.4
4000
9.1
6.7
4.5
5000
8.1
5.7
3.6
6000 7.2 4.8
2.7
7000 6.2 3.9 1.8
S.L. 15.2
12.4
10
1000 14 .1
11.4
9.0
2000 13.1 10 .4 7.9
3000 12.0 9.3
6.9
4000
11.0
8.3
5.9
5000 10.0 7.3 4.9
6000 8.9 6.3
3.9
7000 7.9 5.3 2.9
Section 5 - Performance
BALKED LANDING PERFORMANCE
50
4.7
3.9
3.1
2.3
1.4
0.6
-0.2
-1.0
6.1
5.2
4.3
3.4
2.5
1.7
0.8
-0.1
7.7
6.7
5.8
4.8
3.8
2.8
1.8
0.9
ISA
7.4
6.7
6.0
5.3
4.6
3.9
3.3
2.6
9.0
8.3
7.5
6.8
6.0
5.3
4.5
3.8
10.9
10.1
9.3
8.4
7.6
6.8
6.0
5.2
Ed. 2, Rev.O