Cirrus SR22T User Manual

P/N 13772-149 1 of 10
Cirrus Design Section 9
SR22 / SR22T Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
SR22 / SR22T Airplanes Registered in Mexico and
Operating Under the Direccion General de
Aeronautica Civil (DGAC) Requirements
1. This supplement is required for operation of Cirrus Design SR22 /
SR22T airplanes Registered in Mexico and Operating Under the
Direccion General de Aeronautica Civil (DGAC) Requirements.
2. The supplement is to be attached and used in conjunction with
applicable SR22 / SR22T FAA-Approved Airplane Flight Manual
(AFM). The information contained herein supplements or
supersedes that in the basic AFM and approved supplements only
in those areas indicated.
Original Issue: January 14, 2013

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