Tecnam P2010 2015 - Page 153

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: 9000 ft
Best Economy: -20% to Full Rich F .C.
ISA- 30•c (-33.C) ISA(-3.C)
ISA+ 30•c (21•q
RPM
MAP
PWR TAS
F.C.
PWR
TAS
F.C.
PWR
TAS
F.C.
[lnHg]
[%MCP)
[kn)
[gal/hi
[%MCP) [kn)
[gal/hi
[%MCP)
[kn)
(gal/hi
([L/hll
([ L/h ))
{[L/hll
2700 21.3
85 133 15.4 (58.3) 80 133 14.7 (55.6) 76
133
14.2 (53.8)
2600 21.3
81 130 15 (56.8) 77
131
14.3 (54.1)
73 131
13.8 (52.2)
2600 20
73
124
13.8 (52.2) 69 124 13.3 (50.3)
65
123 12.8 (48.5)
2600 19
67 119 13.1 (49.6) 64
119
12.6(47.7)
60
118 12.1 (45.8)
2600
18
62 114 12.3 (46.6)
58 113
11.9 (45)
55
111 11.5 (43.5)
2450 21.3 77 127 14 .3 (54.1) 72
127
13.7 (51.9)
69
127 13.2 (SO)
2450
20
69
121
13.3 (50.3) 65 121
12.8 (48.5)
62 119
12.3 (46.6)
2450 19
64 116
12.6 (47.7)
60 115
12.l (45.8)
57 114
11.7 (44.3)
2450
18
59
111 11.9 (45)
55 109
11.4 (43.2)
52
106
11.1 (42)
2350 19 66 121 12 .9 (48.8) 62
120
12.4(46.9)
59
117 11.9 (45)
2350 18
60 115
12.2 (46.2) 57
113
11.7 (44.3)
54 110
11.3 (42.8)
Weight: 1160 kg
Corrections
Mixture: FULL RICH Best Power: -10% to Full Rich F.C.
Pressure Altitude: 12000 ft
Best Economy: -20% to Full Rich F .C.
I 1SA - 30•c 1-39•q
ISA (-9•c)
1SA + 30•c 121 ·c1
RPM
MAP PWR TAS F.C.
PWR
TAS
F.C.
PWR
TAS
F.C.
(inHg)
[%MCP) [kn)
[gal/h]
[%MCP J [kn)
[gal/hi
[%MCP) [kn)
[gal/hi
([ L/hll
([L/h))
{[L/hll
2700 19 75 128 14.1 (53.4) 70 128
13.5 (51.1)
67 128
13 (49.2)
2600 19 72 126 13.7 (51.9) 68
126
13.2 (50)
64 125
12.7 (48.1)
2600 18 66 121 13 (49.2) 63 120
12.4 (46.9)
59
118 12 (45.4)
2450 19
68
123 13.2 (SO) 64
122
12.7 (48.1)
61 121
12.2 (46.2)
2450 18
63
118 12.5 (47.3) 59 116
12 (45.4)
56
113 11.6 (43.9)
2350
19
66
121 12.9 (48.8) 62 120
12.4(46.9)
59
117
11.9 (45)
2350
18
60 115
12.2 ( 46 .2) 57
113
11.7 (44.3) 54 110 11.3 (42.8)
Section 5 - Performance
CRUISE PERFORMANCE
Ed. 2, Rev.O