Cirrus System 55X Autopilot User Manual

Cirrus Design Section 5
SR22T Performance Data
P/N 13772-005 5-23P/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

Cirrus System 55X Autopilot Specifications

General

Brand	Cirrus
Model	System 55X Autopilot
Category	Aircrafts
Language	English