Initial issue
EASA Approved
Page 5-11
Associated conditions:
Example:
Weight
600 kg / 1323 lb
Cruise pressure altitude
6000 ft
Flaps
FLAPS 0
(0°)
Engine speed
5000 rpm
Winds
Zero
Airspeed
101 KIAS / 99 KCAS / 108 KTAS
MAP
21.3 inHg
Fuel consumption
16.4 l/h
4.33 U. S. gal/h
Pressure
altitude
Engine
speed
Airspeed
MAP
Fuel consumption
ft
rpm
KIAS
KCAS
KTAS
inHg
(l/h)
U. S. gal/h
2000
4 300
89
88
93
21.6
14.5
3.83
4 500
94
93
99
22.4
15.5
4.10
4 800
103
100
106
23.5
17.2
4.54
5 000
108
105
111
24.2
18.5
4.89
5 500
120
116
123
25.8
21.3
5.63
5 800
125
121
128
26.7
23.3
6.16
4000
4 300
86
85.5
91
20.5
13.6
3.59
4 500
92
90
95
22.2
14.5
3.83
4 800
99
97.5
103
22.2
16.3
4.31
5 000
105
102
108
22.8
17.4
4.60
5 500
117
113
120
24.4
20.4
5.39
5 800
122
118
125
25.2
22.0
5.81
6000
4 300
83
82.5
90
19.2
12.6
3.33
4 500
88
87
95
19.8
13.7
3.62
4 800
96
94.5
103
20.7
15.3
4.04
5 000
101
99
108
21.3
16.4
4.33
5 500
114
110
120
22.6
19.0
5.02
5 800
119
115
126
23.3
20.5
5.42
8000
4 300
78
79
85
18.3
11.8
3.12
4 500
84
84
95
18.8
12.8
3.38
4 800
93
91
103
19.6
14.2
3.75
5 000
98
95.5
108
20.1
15.3
4.04
5 500
109
105.5
119
21.4
18.0
4.76
5 720
114
110.5
125
22.0
19.3
5.10
10000
4 300
74
75.5
88
17.3
11.2
2.96
4 500
79
80
93
17.7
12.0
3.17
4 800
88
87
101
18.4
13.4
3.54
5 000
93
91
106
18.8
14.3
3.78
5 500
104
101
118
19.9
16.9
4.46
5 660
109
106
123
20.5
18.4
4.86
Содержание WT9 Dynamic LSA / Club
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