Cirrus DESIGN SR22T - Cruise Performance

Cirrus Design Section 5
SR22T Performance Data
P/N 13772-003 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........................................................................................................ 3200 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% 18.3 163 8.9 170 9.3 176 9.6
75% 16.4 158 9.6 163 9.9 168 10.2
65% 14.6 149 10.2 154 10.6 159 10.9
55% 12.7 139 11.0 144 11.3 148 11.6
4000 85% 18.3 167 9.1 174 9.5 180 9.8
75% 16.4 161 9.8 166 10.1 172 10.4
65% 14.6 152 10.4 157 10.8 162 11.1
55% 12.7 142 11.1 146 11.5 151 11.8
6000 85% 18.3 171 9.3 178 9.7 184 10.0
75% 16.4 164 9.9 169 10.3 175 10.6
65% 14.6 155 10.6 160 11.0 165 11.3
55% 12.7 144 11.3 149 11.7 153 12.0
8000 85% 18.3 174 9.5 181 9.9 187 10.2
75% 16.4 167 10.1 173 10.5 178 10.8
65% 14.6 157 10.8 163 11.2 168 11.5
55% 12.7 147 11.5 152 11.9 156 12.3
10000 85% 18.3 178 9.7 185 10.1 191 10.4
75% 16.4 170 10.3 176 10.7 181 11.0
65% 14.6 160 11.0 166 11.4 171 11.7
55% 12.7 149 11.7 154 12.1 159 12.5
12000 85% 18.3 181 9.9 188 10.3 195 10.6
75% 16.4 173 10.5 179 10.9 185 11.2
65% 14.6 163 11.2 169 11.6 174 11.9
55% 12.7 152 11.9 157 12.3 161 12.7
Original Issue