Cirrus SR22T User Manual

Cirrus Design Section 2
SR22T Limitations
P/N 13772-005 2-3P/N 13772-005 2-3
Introduction
The limitations included in this Section of the Pilot’s Operating
Handbook (POH) are approved by the Federal Aviation Administration.
This section provides operating limitations, instrument markings and
basic placards required by regulation and necessary for the safe
operation of the aircraft and its standard systems and equipment.
Refer to Section 9: Log of Supplements of this handbook for amended
operating limitations for airplanes equipped with optional equipment.
Compliance with the operating limitations in this section and in Section
9 is required by Federal Aviation Regulations.
• Note •
Limitations associated with optional equipment are not
described in this section. For optional equipment limitations,
refer to Section 9: Log of Supplements.
Certification Status
The aircraft is certificated under the requirements of Federal Aviation
Regulations (FAR) Part 23 as documented by FAA Type Certificate TC
A00009CH.
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