Tecnam P2010 2015 - 10. Cruise Performance

AFMS N"D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
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10. CRUISE PERFORMANCE
Weight: 1160 kg
Corrections
Mixture: FULL RICH Best Power: -l!J% to Full Rich F .C.
Pressure Altitude: Oft
Best Economy: -20% to Full Rich F .C.
1SA - 30"C (-lS"C) ISA (lS"C) ISA+ 30"C (45"C)
RPM
MAP
PWR TAS
(lnHR]
[%MCP] [kn]
2700 29.9
113 138
29.9 109 136
28 101 132
26
90
126
2600
24 79 120
22
69
113
20
59
105
29.9 103 133
28
95 129
26
85
123
2450
24 75
117
22
65
110
20
55
102
29.9 100 131
28 91
127
26 81 121
2350
24
72
115
22
62
108
20
53 99
F.C.
PWR
TAS
F.C.
[ial/h ]
[%MCP]
(kn]
(gal/h]
([ L/h]) ([L/h])
19.2 (72 . 7)
107
139
18.4 (69. 7)
18.7 (70.8) 103
138
17.9 (67.8)
17.6 (66. 6)
96 134
16.9 (64)
16.1 (60.9)
85 127
15.4 (58.3)
14.7 (55.6)
75 121
14.1 (53. 4)
13.3 (50.3)
65 113
12.8 (48.5)
11.9 (45)
56 104
11.5 (43.5)
17.9 (67.8)
98 135
17.1 (64.7)
16.8 (63. 6)
90
130
16.1 (60.9)
15.4 (58.3)
80 124
14.8 (56)
14.1 (53. 4)
71 117 13.5 (51.1)
12.8 (48.5)
62 110
12.3 (46.6)
11.5 (43.5)
52 101
11.1 (42)
17 .4 (65.9) 94
133
16.7 (63.2)
16.2 (61.3)
86 128
15.6 (59. 1)
15 (56.8) 77
122
14.4 (54.5)
13.7 (51.9)
68 115
13.1 (49. 6)
12 .4 (46.9)
59 108
12 (45.4)
11.1 (42)
50 98
10.7 (40.5)
Section 5 - Performance
CRUISE PERFORMANCE
PWR TAS
F.C.
(%MCP] [kn]
(gal/h]
([L/h])
102 141 17.7 (67)
98
139
17.2 (65.1)
91
135
16.3 (61.7)
81 128
14.9 (56.4)
71 121 13.6 (51.5)
62
113
12.4(46.9)
53 103 ll .l (42)
93 136
16.5 (62.5)
85 131 15.5 (58.7)
76
125
14 .3 (54.1)
67
118
13.1 (49. 6)
59 110
11.9 (45)
so 100
10.7 (40.5)
90 134 16 .1 (60.9)
82 129 15 (56.8)
73 123 13.9 (52.6)
65 115
12.7 (48.1)
56 107
11.6 (43.9)
48
96
10.4 (39.4)
Ed. 2. Rev.O