Cirrus DESIGN SR22T User Manual

Cirrus Design Section 2
SR22T Limitations
P/N 13772-003 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 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, 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 DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches