Cirrus SR22T User Manual

P/N 13772-146 1 of 4
Cirrus Design Section 9
SR22T Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
SR22T Airplanes Registered in South Africa and
Operating Under the South African Civil Aviation
Authority (SACAA) Requirements
1. This supplement is required for operation of Cirrus Design SR22T
airplanes registered in South Africa and operating under the South
African Civil Aviation Authority (SACAA) Requirements.
2. The supplement is to be attached and used in conjunction with
applicable 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: 11-16-2010

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