Tecnam P2010 - Page 481

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV5 - 14
Section 5 – Performance-
CRUISE PERFORMANCE
Ed. 1, Rev.2
Weight: 1160 kg
Mixture: FULL RICH
Pressure Altitude: 3000 ft
Corrections
Best Power: -10% to Full Rich F.C.
Best Economy: -20% to Full Rich F.C.
ISA – 30°C (-21°C)
ISA (9°C)
ISA + 30°C (39°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
26.8
104
137
17.9 (67.8)
98
138
17.2 (65.1)
93
139
16.5 (62.5)
2600
26.8
100
135
17.4 (65.9)
94
136
16.7 (63.2)
90
137
16.1 (60.9)
2600
26
96
133
16.9 (64)
90
134
16.2 (61.3)
86
135
15.6 (59.1)
2600
24
85
126
15.4 (58.3)
80
127
14.8 (56)
76
128
14.3 (54.1)
2600
22
76
128
14.3 (54.1)
70
120
13.5 (51.1)
67
120
13 (49.2)
2600
20
63
111
12.6 (47.7)
60
111
12.1 (45.8)
57
110
11.7 (44.3)
2600
18
53
101
11.1 (42)
50
99
10.7 (40.5)
47
97
10.4 (39.4)
2450
26.8
94
132
16.6 (62.8)
89
132
15.9 (60.2)
84
133
15.3 (57.9)
2450
26
90
129
16.1 (60.9)
85
129
15.4 (58.3)
81
130
14.8 (56)
2450
24
80
123
14.7 (55.6)
75
123
14.2 (53.8)
72
124
13.7 (51.9)
2450
22
70
116
13.5 (51.1)
66
116
12.9 (48.8)
63
117
12.5 (47.3)
2450
20
60
108
12.1 (45.8)
57
108
11.6 (43.9)
54
107
11.3 (42.8)
2450
18
50
97
10.7 (40.5)
47
97
10.4 (39.4)
45
95
10.1 (38.2)
2350
26.8
90
130
16.1 (60.9)
85
131
15.5 (58.7)
81
131
14.9 (56.4)
2350
26
86
127
15.6 (59.1)
81
128
15 (56.8)
77
129
14.4 (54.5)
2350
24
77
121
14.3 (54.1)
72
122
13.8 (52.2)
69
122
13.3 (50.3)
2350
22
67
114
13.1 (49.6)
64
114
12.6 (47.7)
60
114
12.2 (46.2)
2350
20
57
105
11.7 (44.3)
54
105
11.3 (42.8)
51
103
11 (41.6)
2350
18.5
50
98
10.7 (40.5)
47
95
10.4 (39.4)
45
92
10.1 (38.2)