Cirrus SR22T User Manual

2-14 P/N 13772-005
Section 2 Cirrus Design
Limitations SR22T
Ice & Rain Protection
Alternate Engine Air Induc-
tion System
1111
Alternate Static Air Source 1 1 1 1
Pitot Heater — — 1 1
Landing Gear
Wheel Pants — — — — May be removed.
Lights
PFD Bezel Lighting — — — 1
PFD Backlighting * 1 1 1 *Required if MFD
Backlighting Fails.
Engine Indicators
Must Be Shown in
Backup Mode.
MFD Bezel Lighting — — — 1
MFD Backlighting * 1 1 1 *Required if PFD
Backlighting Fails.
Engine Indicators
Must Be Shown in
Backup Mode.
Anticollision Lights 2 2 2 2
Instrument Lights — 1 — 1
Navigation Lights — 2 — 2
Landing Light — 1 — 1 For hire operations.
Flash Light — 1 — 1
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