5-28
P/N 11934-003
Section 5
Cirrus Design
Performance Data
SR20
Figure 5-16
Cruise Performance
8000 Feet Pressure Altitude
ISA - 30° C (-31° C)
ISA (-1° C)
ISA + 30° C (29° C)
RPM
MAP
PWR
KTAS
GPH
PWR
KTAS
GPH
PWR
KTAS
GPH
2700
22.2
82%
157
12.9
77%
157
11.6
73%
154
11.4
2500
22.2
73%
150
11.4
69%
150
11.0
65%
147
10.6
2500
21.2
69%
146
10.9
65%
146
10.5
62%
143
10.2
2500
20.1
64%
142
10.4
60%
142
10.0
57%
139
9.7
2500
18.9
59%
136
9.8
55%
136
9.5
52%
134
9.2
2500
17.7
53%
131
9.2
50%
131
8.9
48%
128
8.7
10,000 Feet Pressure Altitude
ISA - 30° C (-35° C)
ISA (-5° C)
ISA + 30° C (25° C)
RPM
MAP
PWR
KTAS
GPH
PWR
KTAS
GPH
PWR
KTAS
GPH
2700
20.6
76%
155
11.7
72%
155
11.2
68%
152
10.9
2500
20.6
68%
148
10.8
64%
148
10.5
61%
145
10.1
2500
19.6
64%
144
10.4
60%
144
10.0
57%
141
9.7
2500
18.5
59%
139
9.8
55%
139
9.5
53%
136
9.2
2500
17.3
54%
134
9.3
50%
134
9.0
48%
131
8.7
12,000 Feet Pressure Altitude
ISA - 30° C (-39° C)
ISA (-9° C)
ISA + 30° C (21° C)
RPM
MAP
PWR
KTAS
GPH
PWR
KTAS
GPH
PWR
KTAS
GPH
2700
19.0
70%
153
11.1
66%
153
10.7
63%
150
10.3
2500
19.0
63%
146
10.3
59%
146
9.9
56%
143
9.6
2500
18.0
59%
141
9.8
55%
141
9.5
52%
138
9.2
2500
16.8
53%
136
9.2
50%
136
8.9
47%
133
8.6
14,000 Feet Pressure Altitude
ISA - 30° C (-43° C)
ISA (-13° C)
ISA + 30° C (17° C)
RPM
MAP
PWR
KTAS
GPH
PWR
KTAS
GPH
PWR
KTAS
GPH
2700
17.6
66%
151
10.5
62%
151
10.2
58%
148
9.8
2500
17.6
59%
144
9.8
55%
144
9.5
52%
141
9.2
2500
16.5
54%
142
9.3
50%
142
9.0
48%
139
8.7
Sheet 2 of 2
Revision A5
Summary of Contents for SR20
Page 10: ...1 2 P N 11934 003 Section 1 Cirrus Design General SR20 Intentionally Left Blank Revision A3 ...
Page 22: ...2 2 P N 11934 003 Section 2 Cirrus Design Limitations SR20 Placards 2 21 Revision A6 ...
Page 308: ...9 2 P N 11934 003 Section 9 Cirrus Design Supplements SR20 Intentionally Left Blank Reissue A ...