Cirrus SR22T User Manual

5-30 P/N 13772-005
Section 5 Cirrus Design
Performance Data SR22T
Range / Endurance: 55% Power Cruise - Cruise 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 0.7 78.9 143 12.7 6.2 889 11.2
4000 1.3 78.2 145 12.7 6.1 900 11.4
6000 2.0 77.5 147 12.7 6.1 912 11.6
8000 2.7 76.8 150 12.7 6.0 924 11.8
10000 3.5 76.1 152 12.7 6.0 936 12.0
12000 4.2 75.3 155 12.7 5.9 948 12.2
14000 5.0 74.6 157 12.7 5.9 959 12.4
16000 5.8 73.8 160 12.7 5.8 971 12.6
18000 6.6 73.0 162 12.7 5.7 982 12.8
20000 7.4 72.2 165 12.7 5.7 994 13.0
22000 8.1 71.4 168 12.7 5.6 1005 13.2
24000 9.1 70.5 170 12.7 5.5 1016 13.4
25000 9.6 69.9 171 12.7 5.5 1021 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