Cirrus SR22T User Manual

2-16 P/N 13772-005
Section 2 Cirrus Design
Limitations SR22T
Icing
Flight into known icing conditions is prohibited.
Runway Surface
This airplane may be operated on any smooth runway surface.
Vertical Speed Indicator — — — —
Engine Indicating
Cylinder Head
Tem pe ra tur e I nd ic at io n
————
Exhaust Gas Temperature
Indication
————
Fuel Flow Indication 1 1 1 1
Manifold Pressure Indica-
tion
1111
Oil Pressure Indication 1 1 1 1
Oil Quantity Indicator (Dip-
stick)
1111
Oil Temperature Indication 1 1 1 1
Tur bin e In le t Te mp era tu re
Indication
1111
Engine Speed 1 1 1 1
Special Equipment
Cirrus Airframe Parachute
(CAPS)
1111
System, Instrument, and/
or Equipment
Kinds of Operation
(Continued)
Remarks, Notes,
and/or
Exceptions
VFR
Day
VFR
Nt.
IFR
Day
IFR
Nt.
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