Tecnam P2010 2015 - Page 151

AFMS N'D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
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Weight: 1160 kg
Corrections
Mixture: FULL RICH Best Power: -10% to Full Rich F. C.
Pressure Attitude: 3000 ft
Best Economy: -20% to Full Ri ch F.C.
ISA- 30"C (·Zl "C) ISA (9"C)
ISA + 30"C (39"C)
RPM
MAP
PWR TAS
PnHg]
[%MCP] [kn)
2700 26.8 104 137
2600 26.8
100 135
2600 26
96
133
2600 24
85
126
2600
22
76 128
2600 20
63 111
2600 18 53 101
2450 26.8
94
132
2450 26
90
129
2450 24
80
123
2450
22
70 116
2450 20
60
108
2450
18
50
97
2350 26.8
90
130
2350 26 86 127
2350 24
77
121
2350 22 67 114
2350 20
57
105
2350
18.5
50 98
F.C.
PWR TAS
F.C.
[pi/hi
[%MCP]
[kn)
filll/h]
([l/h)) ([l/h))
17.9 (67.8)
98 138
17.2 (65. 1)
17.4 (65.9)
94
136
16 .7 (63. 2)
16.9 (6 4) 90 134 16.2 (61.3)
15.4 (58.3)
80 127
14.8 (56)
14.3 (5 4.1) 70 120
13.5 (51.1)
12.6 (47.7) 60 111 12.1 (45.8)
11.1 (42)
so
99
10.7 (40.S)
16.6 (62.8)
89 132
15.9 (60.2)
16.1 (60.9) 85
129
15.4 (58.3)
14 .7 (55.6) 75
123
14 .2 (53.8)
13.5 (51.1) 66 116
12.9 (48.8)
12 .1 (45.8) 57
108
11.6 (43.9)
10.7 (40.5) 47
97
10.4 (39. 4)
16 .1 (60.9) 85 131 15.S (58.7)
15.6 (59.1)
81
128
15 (56 .8)
14 .3 (54.1) 72
122
13.8 (52. 2)
13.1 (49.6) 64
114
12.6 (47.7)
11.7 (44.3) 54
105
11 .3 (42.8)
10.7 (40.5) 47
95
10.4 (39.4)
Section 5 - Performance
CRUISE PERFORMANCE
PWR TAS
f. C.
[%MCP)
[kn]
[gal/hi
([l/hll
93 139 16.5 (62.5)
90
137 16.1 (60.9)
86
135 15.6 (59.1)
76
128 14.3 (54.1)
67 120 13 (49.2)
57 110
11.7 (44.3)
47 97 10.4 (39.4)
84 133 15.3 (57.9)
81
130 14.8 (56)
72
124 13.7 (51.9)
63
117
12.5 (47.3)
54
107 11.3 (42.8)
45 95
10 .1 (38.2)
81 131 14 .9 (56.4)
77 129
14.4 (54.5)
69
122 13.3 (50.3)
60
114 12.2 (46.2)
51
103 11 (41.6)
45
92 10.1 (38.2)
Ed. 2, Rev.O