sonaca aircraft S201 - Page 148

S201 AFM
5 - PERFORMANCE
5.3 - PERFORMANCE TABLES
AND DIAGRAMS
27/06/2019
SONAIR-S2-D-MAN-006
Page : 5-6
Rev. : A
MAXIMUM TAKE OFF POWER [kW] (Approx. 5800 RPM)
Standard Atmosphere
Delta temperature with standard temperature [°C]
Hp
T (°F)
T (°C)
-45
-40
-35
-30
-25
-20
-15
-10
-5
0
5
10
15
20
25
30
35
-2000
66
19
101
99
97
95
94
92
90
89
87
86
84
83
81
80
79
78
76
0
59
15
100
98
96
94
93
91
89
88
86
85
83
82
80
79
78
77
75
2000
52
11
99
97
95
93
92
90
88
87
85
84
82
81
79
78
77
76
74
4000
45
7
98
96
94
92
91
89
87
86
84
83
81
80
78
77
76
75
73
6000
38
3
97
95
93
91
90
88
86
85
83
81
80
79
77
76
75
74
72
8000
30
-1
96
94
92
90
88
87
85
83
82
80
79
78
76
75
74
73
71
According to the above tables, the correction at all altitudes is approximately :
• -5% for an increase of temperature of 15°C with respect to ISA temperature, and
• -10% for an increase of temperature of 30°C with respect to ISA temperatures.
• +5% for a decrease of temperature of 15°C with respect to ISA temperature, and
• +10% for a decrease of temperature of 30°C with respect to ISA temperatures.
Source : Rotax Operator’s Manual, Ref. OM-914