Tecnam P2010 2015 - Page 152

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 Altitude: 6000 ft
Best Econornv: -20% to Full Rich F.C.
JSA- 30'C (-27'C) ISA (3'C)
ISA + 30'C (33'C)
RPM
MAP
PWR TAS
[in HI]
[%MCP)
[kn)
2700
23.9
94 135
2600
23.9
90 133
2600 23
85
130
2600 22
80
126
2600 20
68
117
2600 19
63
113
2600
18
57 108
2450 23.9 85
129
2450 23 80 126
2450
22
75 123
2450 20 64 114
2450
19
59 11 0
2450
18
54 104
2350
23.9
81
12 7
2350 23 17 124
2350 22 72 121
2350 20
62
112
2350
19
57 10 7
2350
18.5
54 104
F.C.
PWR
TAS
F.C.
[gal/hi
( %MCP) ( kn)
[gal/hi
([L/h)) ([L/h))
16.6 (62. 8) 89
136
15.9 (60.2)
16.l (60.9) 85
134
15.5 (58. 7)
15.5 (58.7) 80
130
14.8 (56)
14 .8 (56) 75
127
14.2 (53.8)
13.2 (50)
64 117
12.7 (48.1)
12.5 (47.3)
59 112
12 (45.4)
11.7 (44.3) 54
106
11.3 (42.8)
15.4 (58.3) 80 130
14.8 (56)
14.8 (56) 75
127
14.2 (53. 8)
14 .1 (53.4) 71
123
13.6 (51. 5)
12.7 (48.1) 61 114
12.2 (46.2)
12 (45.4)
56 109
11.6 (43.9)
11.3 (42.8) 51
102
10.9 (41.3)
15 (56.8) 17 128
14.4(54 .5)
14 .3 (5 4.1) 73 124
13.8 (52. 2)
13.7 (51.9) 68
121
13.2 (50)
12.3 (46.6)
58 111
11.9 (4 5)
11.7 (44.3)
54
106
11.2 (42.4)
11.3 (42.8) 51
102
10.9 (41.3)
Section 5 - Performance
CRUISE PERFORMANCE
PWR
TAS
F.C.
( %MCP) ( kn )
[gal/hi
([L/h))
84 137 15.3 (57.9)
81
134 14 .9 (56.4)
76 131 14.3 (5 4.1)
72
127 13.6 (51.5)
61 117
12.3 (46.6)
56
111 11.6 (43.9)
51 104 10.9 (41.3)
76 131
14 .2 (53.8)
72
127 13.7 (51.9)
67 123
13.1 (49. 6)
58
113
11.8 (44. 7)
53 107
11.2 (42.4)
49 99
10.6 (40.1)
73
128 13.8 (52.2)
69
124 13.3 (50.3)
65
120
12.7 (48.1)
55
110 11.5 (43.5)
51 103
10.9 (41.3)
49 99
10.6 (40.1)
Ed. 2. Rev.O