Cirrus SR22T User Manual

Cirrus Design Section 5
SR22T Performance Data
P/N 13772-005 5-27P/N 13772-005 5-27
Range / Endurance: 55% Power Cruise - Full Power Climb
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
2000 1.0 78.5 143 12.7 6.2 884 11.2
4000 2.1 77.5 145 12.7 6.1 890 11.4
6000 3.2 76.4 147 12.7 6.0 896 11.6
8000 4.3 75.3 150 12.7 5.9 902 11.8
10000 5.4 74.2 152 12.7 5.8 908 12.0
12000 6.5 73.0 155 12.7 5.7 913 12.2
14000 7.7 71.9 157 12.7 5.6 918 12.4
16000 8.9 70.7 160 12.7 5.6 922 12.6
18000 10.1 69.4 162 12.7 5.5 926 12.8
20000 11.3 68.2 165 12.7 5.4 930 13.0
22000 12.6 66.9 168 12.7 5.3 933 13.2
24000 14.2 65.4 170 12.7 5.1 934 13.4
25000 15.1 64.4 171 12.7 5.1 932 13.5
Original Issue

Cirrus SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental TSIO-550-K
Horsepower	315 hp
Max Takeoff Weight	3, 600 lbs
Service Ceiling	25, 000 ft
Cabin Width	49 in
Cabin Height	50 in
Seating Capacity	4
Avionics	Cirrus Perspective+ by Garmin
Category	Single-engine piston aircraft
Propeller	Hartzell 3-blade composite
Wingspan	38 ft 4 in
Length	26 ft
Height	8 ft 11 in
Maximum Cruise Speed	213 KTAS
Fuel Capacity	92 gallons
Stall Speed	64 knots
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cruise Speed	183 knots