Cirrus SR22T User Manual

Cirrus Design Section Front Matter
SR22T Foreword
P/N 13772-005 Front Matter-5P/N 13772-005 Front Matter-5
Retention of Data
In the event a new title page is issued, the weight and balance data
changes, equipment list changes, or the “Log of Supplements” is
replaced, the owner must ensure that all information applicable to the
airplane is transferred to the new pages and the aircraft records are
current. It is not a requirement that owners retain information, such as
supplements, that is not applicable to their airplane.
Warnings, Cautions, and Notes
Warnings, Cautions, and Notes are used throughout this Handbook to
focus attention on special conditions or procedures as follows:
• WARNING •
Warnings are used to call attention to operating procedures
which, if not strictly observed, may result in personal injury or
loss of life.
• Caution •
Cautions are used to call attention to operating procedures
which, if not strictly observed, may result in damage to
equipment.
• Note •
Notes are used to highlight specific operating conditions or
steps of a procedure.
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