Cirrus Design
Section 5
SR22T
Performance Data
P/N 13772-005
5-23
P/N 13772-005
5-23
Cruise Performance
• Note •
Subtract 10 KTAS if nose wheel pant and fairing removed. Lower KTAS by
10% if nose and main wheel pants & fairings are removed.
Aircraft with optional Air Conditioning System: Cruise performance is reduced
by 2 knots. For maximum performance, turn air-conditioner off.
Aircraft with optional Enhanced Vision System: Cruise performance is
reduced by up to 1 knot.
Conditions:
• Weight ........................................................................................................ 3400 LB
• Winds ............................................................................................................... Zero
CRUISE PERFORMANCE
ISA -30°C
ISA
ISA +30°C
Altitude
(ft MSL)
Power
(% of 315)
FF
(GPH)
TAS
(KTAS)
Econ
(nm/gal)
TAS
(KTAS)
Econ
(nm/gal)
TAS
(KTAS)
Econ
(nm/gal)
2000
85%
18.3
164
9.0
170
9.3
176
9.6
75%
16.4
157
9.6
162
9.9
167
10.2
65%
14.6
148
10.2
154
10.5
158
10.8
55%
12.7
138
10.9
143
11.2
147
11.5
4000
85%
18.3
168
9.1
174
9.5
179
9.8
75%
16.4
160
9.7
165
10.1
170
10.4
65%
14.6
151
10.3
156
10.7
161
11.0
55%
12.7
140
11.0
145
11.4
149
11.8
6000
85%
18.3
171
9.3
177
9.7
183
10.0
75%
16.4
163
9.9
168
10.2
174
10.6
65%
14.6
153
10.5
159
10.9
163
11.2
55%
12.7
143
11.2
147
11.6
152
11.9
8000
85%
18.3
174
9.5
180
9.8
186
10.2
75%
16.4
166
10.1
171
10.4
177
10.8
65%
14.6
156
10.7
161
11.1
166
11.4
55%
12.7
145
11.4
150
11.8
154
12.1
10000
85%
18.3
177
9.7
184
10.0
190
10.4
75%
16.4
169
10.3
175
10.6
180
11.0
65%
14.6
159
10.9
164
11.3
169
11.6
55%
12.7
148
11.6
152
12.0
157
12.3
12000
85%
18.3
181
9.9
187
10.2
193
10.6
75%
16.4
172
10.4
178
10.8
183
11.2
65%
14.6
162
11.1
167
11.5
172
11.8
55%
12.7
150
11.8
155
12.2
159
12.5
Original Issue
