Cirrus SR22T User Manual

P/N 13772-148 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 Chile and
Operating Under the Dirección General de
Aeronáutica Civil de Chile (DGAC) Requirements
1. This supplement is required for operation of Cirrus Design SR22 /
SR22T Airplanes Registered in Chile and Operating Under the
Dirección General de Aeronáutica Civil de Chile (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: Oct 04, 2012

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