Cirrus SR22T User Manual

2-26 P/N 13772-005
Section 2 Cirrus Design
Limitations SR22T
Figure 2-5
(Sheet 3 of 6)
CREW SEATS MUST BE LOCKED IN POSITION AND
CONTROL HANDLES FULLY DOWN BEFORE FLIGHT
RICH
OFF
LIFT BUTTON FOR OFF POSITION
P
O
W
E
R
OFF
RIGHT
46 U.S.
GALLONS
USABLE
LEFT
46 U.S.
GALLONS
USABLE
CUTOFF
F
R
I
C
T
I
O
N
IDLE
M
I
X
T
U
R
E
MAX
TURN BOOST PUMP
ON DURING TAKE OFF,
CLIMB, LANDING AND
SWITCHING FUEL TANKS.
PUMP
FUEL
BOOST
HIGH
BOOST/
PRIME
Engine control panel:
SR22_FM02_3559
100%
50%
UP
FLAPS
150 KIAS
110 KIAS
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