Tecnam P2010 - Page 482

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV5 - 15
Section 5 – Performance-
CRUISE PERFORMANCE
Ed. 1, Rev.2
Weight: 1160 kg
Mixture: FULL RICH
Pressure Altitude: 6000 ft
Corrections
Best Power: -10% to Full Rich F.C.
Best Economy: -20% to Full Rich F.C.
ISA – 30°C (-27°C)
ISA (3°C)
ISA + 30°C (33°C)
RPM
MAP
[inHg]
PWR
[%MCP]
TAS
[kn]
F.C.
[gal/h]
([L/h])
PWR
[%MCP]
TAS
[kn]
F.C.
[gal/h]
([L/h])
PWR
[%MCP]
TAS
[kn]
F.C.
[gal/h]
([L/h])
2700
23.9
94
135
16.6 (62.8)
89
136
15.9 (60.2)
84
137
15.3 (57.9)
2600
23.9
90
133
16.1 (60.9)
85
134
15.5 (58.7)
81
134
14.9 (56.4)
2600
23
85
130
15.5 (58.7)
80
130
14.8 (56)
76
131
14.3 (54.1)
2600
22
80
126
14.8 (56)
75
127
14.2 (53.8)
72
127
13.6 (51.5)
2600
20
68
117
13.2 (50)
64
117
12.7 (48.1)
61
117
12.3 (46.6)
2600
19
63
113
12.5 (47.3)
59
112
12 (45.4)
56
111
11.6 (43.9)
2600
18
57
108
11.7 (44.3)
54
106
11.3 (42.8)
51
104
10.9 (41.3)
2450
23.9
85
129
15.4 (58.3)
80
130
14.8 (56)
76
131
14.2 (53.8)
2450
23
80
126
14.8 (56)
75
127
14.2 (53.8)
72
127
13.7 (51.9)
2450
22
75
123
14.1 (53.4)
71
123
13.6 (51.5)
67
123
13.1 (49.6)
2450
20
64
114
12.7 (48.1)
61
114
12.2 (46.2)
58
113
11.8 (44.7)
2450
19
59
110
12 (45.4)
56
109
11.6 (43.9)
53
107
11.2 (42.4)
2450
18
54
104
11.3 (42.8)
51
102
10.9 (41.3)
49
99
10.6 (40.1)
2350
23.9
81
127
15 (56.8)
77
128
14.4 (54.5)
73
128
13.8 (52.2)
2350
23
77
124
14.3 (54.1)
73
124
13.8 (52.2)
69
124
13.3 (50.3)
2350
22
72
121
13.7 (51.9)
68
121
13.2 (50)
65
120
12.7 (48.1)
2350
20
62
112
12.3 (46.6)
58
111
11.9 (45)
55
110
11.5 (43.5)
2350
19
57
107
11.7 (44.3)
54
106
11.2 (42.4)
51
103
10.9 (41.3)
2350
18.5
54
104
11.3 (42.8)
51
102
10.9 (41.3)
49
99
10.6 (40.1)